U.S. patent application number 15/179661 was filed with the patent office on 2017-01-26 for multiple beam additive manufacturing.
The applicant listed for this patent is IPG Photonics Corporation. Invention is credited to Joseph DALLAROSA, William O'NEILL, Andrew PAYNE, Martin SPARKES, David SQUIRES.
Application Number | 20170021455 15/179661 |
Document ID | / |
Family ID | 57504395 |
Filed Date | 2017-01-26 |
United States Patent
Application |
20170021455 |
Kind Code |
A1 |
DALLAROSA; Joseph ; et
al. |
January 26, 2017 |
MULTIPLE BEAM ADDITIVE MANUFACTURING
Abstract
Systems and methods for multiple beam additive manufacturing use
multiple beams of light (e.g., laser light) to expose layers of
powder material in selected regions until the powder material fuses
to form voxels, which form build layers of a three-dimensional
structure. The light may be generated from selected light sources
and coupled into an array of optical fibers having output ends
arranged in an optical head in at least one line such that multiple
beams are sequentially directed by the optical head to the same
powder region providing multiple beam sequential exposures (e.g.,
with pre-heating, melting and controlled cool down) to fuse the
powder region. The multiple sequential beams may be moved using
various techniques (e.g., by moving the optical head) and according
to various scan patterns such that a plurality of fused regions
form each build layer.
Inventors: |
DALLAROSA; Joseph;
(Uxbridge, MA) ; O'NEILL; William; (Cambridge,
GB) ; SQUIRES; David; (Lebanon, CT) ; SPARKES;
Martin; (Shingay Cum Wendy, GB) ; PAYNE; Andrew;
(Trumpington, GB) |
|
Applicant: |
Name |
City |
State |
Country |
Type |
IPG Photonics Corporation |
Oxford |
MA |
US |
|
|
Family ID: |
57504395 |
Appl. No.: |
15/179661 |
Filed: |
June 10, 2016 |
Related U.S. Patent Documents
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Application
Number |
Filing Date |
Patent Number |
|
|
62173541 |
Jun 10, 2015 |
|
|
|
Current U.S.
Class: |
1/1 |
Current CPC
Class: |
Y02P 10/25 20151101;
B29C 64/268 20170801; B33Y 30/00 20141201; B23K 26/342 20151001;
B33Y 50/02 20141201; B23K 26/0604 20130101; B23K 26/082 20151001;
B22F 3/1055 20130101; B23K 2103/08 20180801; Y02P 10/295 20151101;
B23K 26/073 20130101; B22F 2003/1056 20130101; B29C 64/277
20170801; B23K 26/0626 20130101; B33Y 10/00 20141201; B23K 26/0869
20130101; B29C 64/153 20170801 |
International
Class: |
B23K 26/342 20060101
B23K026/342; B33Y 30/00 20060101 B33Y030/00; B23K 26/073 20060101
B23K026/073; B23K 26/06 20060101 B23K026/06; B23K 26/082 20060101
B23K026/082; B33Y 10/00 20060101 B33Y010/00; B33Y 50/02 20060101
B33Y050/02 |
Claims
1. A method for multiple beam additive manufacturing of a
three-dimensional structure formed by a plurality of build layers,
the method comprising: providing an array of light sources and an
array of optical fibers coupled to the array of light sources,
respectively, and an optical head including output ends of the
optical fibers, wherein the optical fiber output ends are arranged
in at least one line; delivering powder layers of powder material
on a powder bed support system that moves vertically and
incrementally to accommodate each of the powder layers; and forming
build layers of the three-dimensional structure in each of the
powder layers of powder material by fusing powder regions to
produce fused regions corresponding to voxels of the
three-dimensional structure, wherein the fused regions of the
powder material in each of the powder layers collectively form each
of the respective build layers of the three-dimensional structure,
wherein forming each of the build layers includes performing
multiple beam sequential exposures with a varying intensity of
light on a powder region to be fused in each powder layer, wherein
performing each of the multiple beam sequential exposures includes
generating light from light sources in the array of light sources
and moving the line of the optical fiber output ends across the
powder region such that beams of light are emitted from the optical
fiber output ends and sequentially directed to the powder region to
fuse the powder region.
2. The method for multiple beam additive manufacturing of claim 1
wherein the multiple beam sequential exposures with varying
intensity of light are formed by at least one pre-heating beam
emitted from at least one of the optical fiber output ends at a
beginning of the line to provide pre-heating, at least one melting
beam emitted from at least one of the optical fiber output ends at
a middle of the line to provide melting, and at least one cool down
beam emitted from at least one of the optical fiber output ends at
an end of the line to provide controlled cool down.
3. The method for multiple beam additive manufacturing of claim 1
wherein the light sources include laser diodes.
4. The method for multiple beam additive manufacturing of claim 3
wherein the output power of the laser diodes ranges from 10 W to 60
W to provide the varying intensity of light.
5. The method for multiple beam additive manufacturing of claim 1
wherein the light sources include fiber lasers.
6. The method for multiple beam additive manufacturing of claim 1
wherein the output ends of the optical fibers are arranged in a
one-dimensional array in the optical head.
7. The method for multiple beam additive manufacturing of claim 1
wherein the output ends of the optical fibers are arranged in a
two-dimensional array in the optical head.
8. The method for multiple beam additive manufacturing of claim 1
wherein the output ends of the optical fibers are arranged in a
two-dimensional staggered array in the optical head.
9. The method for multiple beam additive manufacturing of claim 1
wherein performing the multiple beam sequential exposures on each
power region to be fused includes raster scanning the beams.
10. The method for multiple beam additive manufacturing of claim 1
wherein the powder material includes a metal powder.
11. The method for multiple beam additive manufacturing of claim 10
wherein the metal powder includes a Nickel-based superalloy
powder.
12. The method for multiple beam additive manufacturing of claim 10
wherein the metal powder includes an austenite
nickel-chromium-based superalloy powder.
13. The method for multiple beam additive manufacturing of claim 10
wherein the porosity of the three-dimensional structure is below
0.05 vol %.
14. The method for multiple beam additive manufacturing of claim 1
wherein the optical head is configured to produce beam spots having
a size in a range of 10 to 500 .mu.m and a spacing in a range of 0
to 600 .mu.m.
15. A method for multiple beam additive manufacturing of a
three-dimensional structure formed by a plurality of build layers,
the method comprising: delivering a powder layer of powder material
to a powder bed support system; forming a build layer of the
three-dimensional structure in the powder layer of powder material
by fusing powder regions to produce fused regions that collectively
form the build layer, wherein forming the build layer includes
performing multiple beam sequential exposures on powder regions to
be fused in each powder layer, wherein performing each of the
multiple beam sequential exposures includes sequentially directing
beams of light with varying intensity to the powder region to fuse
the powder region; and repeating the delivering a powder layer and
the forming a build layer in the powder layer to form each of the
build layers of the three-dimensional structure and wherein each of
the fused regions corresponds to a voxel of the three-dimensional
structure.
16. The method for multiple beam additive manufacturing of claim 15
wherein performing each of the multiple beam sequential exposures
includes generating light from laser diodes to provide the beams of
light.
17. The method for multiple beam additive manufacturing of claim 15
wherein the beams of light form a one dimensional array of beam
spots.
18. The method for multiple beam additive manufacturing of claim 15
wherein the beams of light form a two-dimensional array of beam
spots.
19. The method for multiple beam additive manufacturing of claim 15
wherein the light beams produce beam spots having a size in a range
of 10 to 500 .mu.m and a spacing in a range of 0 to 600 .mu.m.
20. A method for multiple beam additive manufacturing of a
three-dimensional structure, the method comprising: providing an
array of light sources and an array of optical fibers coupled to
the array of light sources, respectively, and an optical head
including output ends of the optical fibers, wherein the optical
fiber output ends are arranged in at least one line; receiving
build instructions for each build layer of the three-dimensional
structure, the build instructions including at least optical head
positioning data defining a position of the optical head and light
source data identifying selected light sources and a power and
exposure time for the selected light sources; and forming each
build layer of the three-dimensional structure by moving the
optical head relative to powder layers of powder material in
accordance with the optical head positioning data while activating
selected light sources in accordance with the light source data to
provide multiple beam sequential exposures with a varying intensity
of light on a selected powder region in each of the powder layers
to fuse the powder material in the selected powder region, wherein
the fused regions of the powder material in each of the layers form
the build layers of the three-dimensional structure.
21. The method for multiple beam additive manufacturing of claim 20
wherein the light source data includes data defining the power of
the selected light sources to produce the varying intensity of
light.
22. A multiple beam additive manufacturing system comprising: a
powder bed support system for supporting a powder bed and a
three-dimensional structure formed therein and for moving the
powder bed vertically and incrementally to accommodate multiple
powder layers of powder material; a powder delivery system for
delivering each of the powder layers to form the powder bed; an
array of light sources for generating light; an array of optical
fibers coupled to the light sources, respectively; a multiple beam
optical head including output ends of the optical fibers; and a
control system for controlling the array of light sources, the
powder bed support system, and the powder delivery system in
coordination to form build layers of the three-dimensional
structure in each of the powder layers delivered to the powder bed,
the control system being configured to selectively control each of
the light sources to generate light from selected light sources in
the array of light sources and to move the line of the optical
fiber output ends sequentially across a powder region to be fused
to provide multiple beam sequential exposures with varying
intensity on the powder region such that beams of light are emitted
from the optical fiber output ends and sequentially directed to the
powder region to fuse the powder region to provide fused regions
that form voxels of the three-dimensional structure.
23. The multiple beam additive manufacturing system of claim 22
further comprising an optical head motion stage for moving the
optical head relative to the powder layers on the powder bed
support system to scan the beams of light across the powder
layers.
24. The multiple beam additive manufacturing system of claim 22
wherein the output ends of the optical fibers are arranged in a
one-dimensional array.
25. The multiple beam additive manufacturing system of claim 22
wherein the output ends of the optical fibers are arranged in a
two-dimensional array.
26. The multiple beam additive manufacturing system of claim 22
wherein the control system is configured to control power and
exposure time of selected light sources in the array of light
sources.
27. The multiple beam additive manufacturing system of claim 22
wherein the control system is responsive to a build instruction
file defining instructions to form each build layer of the
three-dimensional structure from the powder layers.
28. The multiple beam additive manufacturing system of claim 27
wherein the build instruction file includes at least optical head
positioning data defining a position of the optical head and light
source data identifying the selected light sources and a power and
exposure time for the selected light sources.
29. The multiple beam additive manufacturing system of claim 28
wherein the build instruction file further includes powder layer
control data for controlling deposition of each powder layer.
30. The multiple beam additive manufacturing system of claim 22
wherein each of the light sources is a diode laser.
Description
CROSS-REFERENCE TO RELATED APPLICATIONS
[0001] The present application claims the benefit of U.S. Patent
Application Ser. No. 62/173,541 filed Jun. 10, 2015, which is fully
incorporated herein by reference.
BACKGROUND OF THE DISCLOSURE
[0002] Field of the Disclosure
[0003] The present disclosure relates to additive manufacturing and
more particularly, to multiple beam additive manufacturing.
[0004] Background Art Discussion
[0005] Additive manufacturing (also known as three-dimensional
printing) techniques have been used to manufacture
three-dimensional structures of almost any shape. Using an additive
process, successive layers of material are deposited to form the
structure based on data defining a 3D model of the structure. In
some methods, referred to as powder bed fusion (PBF), the
successive layers forming the structure are produced by depositing
successive layers of powder material and using a light beam (e.g.,
laser light) to bind or fuse the powder material in selected
regions of each layer. Examples of these methods include selective
laser sintering (SLS) wherein the laser sinters the powder
particles in the selected regions to form each build layer of the
structure and selective laser melting (SLM) wherein the laser melts
the powder in the selected regions such that the melted material
hardens to form each build layer of the structure.
[0006] Although such laser additive manufacturing (LAM) techniques
have been successful, the movement of the laser to the selected
regions often slows the build rate and the speed of manufacturing.
Multiple beams have been used in an effort to increase speeds, but
scanning multiple beams across the powder layers may result in
stresses being created in the fused material of each build layer.
The thermal energy, for example, may cause thermal part stress,
which may deform the three-dimensional structure as the build
layers are formed. As such, LAM techniques have not been as
successful when used with certain materials such as superalloys
because thermal stresses may result in cracking. Also, LAM
techniques have not been as successful when used with powder
material having larger particle sizes because the power of the
laser may not be sufficient to melt and fuse larger particles sizes
without causing excessive thermal stress.
[0007] Moreover, faster build rates generally require energy to be
introduced into the powder bed faster (i.e., at higher power).
Increasing the power of a LAM system is challenging because optical
elements must be larger and cooling must be increased to withstand
the higher power. The scanning mirror in such systems becomes less
responsive with the increased size, which decreases the scanning
speed and reduces build speed. Attempts at using multiple beams in
SLM systems have been unsuccessful because of the challenges
involved with scanning the same area with multiple beams.
[0008] Accordingly, there is a need for an additive manufacturing
system and method that allows faster build rates while reducing
thermal stresses in the fused material.
SUMMARY OF THE DISCLOSURE
[0009] Consistent with an embodiment, a method is provided for
multiple beam additive manufacturing of a three-dimensional
structure formed by a plurality of build layers. The method
includes: providing an array of light sources and an array of
optical fibers coupled to the array of light sources, respectively,
and an optical head including output ends of the optical fibers,
wherein the optical fiber output ends are arranged in at least one
line; delivering powder layers of powder material on a powder bed
support system that moves vertically and incrementally to
accommodate each of the powder layers; and forming build layers of
the three-dimensional structure in each of the powder layers of
powder material by fusing powder regions to produce fused regions
corresponding to voxels of the three-dimensional structure, wherein
the fused regions of the powder material in each of the powder
layers collectively form each of the respective build layers of the
three-dimensional structure, wherein forming each of the build
layers includes performing multiple beam sequential exposures with
a varying intensity of light on a powder region to be fused in each
powder layer, wherein performing each of the multiple beam
sequential exposures includes generating light from light sources
in the array of light sources and moving the line of the optical
fiber output ends across the powder region such that beams of light
are emitted from the optical fiber output ends and sequentially
directed to the powder region to fuse the powder region.
[0010] Consistent with another embodiment, a method is provided for
multiple beam additive manufacturing of a three-dimensional
structure formed by a plurality of build layers. The method
includes: delivering a powder layer of powder material to a powder
bed support system; forming a build layer of the three-dimensional
structure in the powder layer of powder material by fusing powder
regions to produce fused regions that collectively form the build
layer, wherein forming the build layer includes performing multiple
beam sequential exposures on powder regions to be fused in each
powder layer, wherein performing each of the multiple beam
sequential exposures includes sequentially directing beams of light
with varying intensity to the powder region to fuse the powder
region; and repeating the delivering a powder layer and the forming
a build layer in the powder layer to form each of the build layers
of the three-dimensional structure and wherein each of the fused
regions corresponds to a voxel of the three-dimensional
structure.
[0011] Consistent with a further embodiment, a method is provided
for multiple beam additive manufacturing of a three-dimensional
structure. The method includes: providing an array of light sources
and an array of optical fibers coupled to the array of light
sources, respectively, and an optical head including output ends of
the optical fibers, wherein the optical fiber output ends are
arranged in at least one line; receiving build instructions for
each build layer of the three-dimensional structure, the build
instructions including at least optical head positioning data
defining a position of the optical head and light source data
identifying selected light sources and a power and exposure time
for the selected light sources; and forming each build layer of the
three-dimensional structure by moving the optical head relative to
powder layers of powder material in accordance with the optical
head positioning data while activating selected light sources in
accordance with the light source data to provide multiple beam
sequential exposures with a varying intensity of light on a
selected powder region in each of the powder layers to fuse the
powder material in the selected powder region, wherein the fused
regions of the powder material in each of the layers form the build
layers of the three-dimensional structure.
[0012] Consistent with yet another embodiment, a multiple beam
additive manufacturing system includes a powder bed support system
for supporting a powder bed and a three-dimensional structure
formed therein and for moving the powder bed vertically and
incrementally to accommodate multiple powder layers of powder
material and a powder delivery system for delivering each of the
powder layers to form the powder bed. The multiple beam additive
manufacturing system also includes an array of light sources for
generating light, an array of optical fibers coupled to the light
sources, respectively, and a multiple beam optical head including
output ends of the optical fibers. The multiple beam additive
manufacturing system further includes a control system for
controlling the array of light sources, the powder bed support
system, and the powder delivery system in coordination to form
build layers of the three-dimensional structure in each of the
powder layers delivered to the powder bed. The control system is
configured to selectively control each of the light sources to
generate light from selected light sources in the array of light
sources and to move the line of the optical fiber output ends
sequentially across a powder region to be fused to provide multiple
beam sequential exposures with varying intensity on the powder
region such that beams of light are emitted from the optical fiber
output ends and sequentially directed to the powder region to fuse
the powder region to provide fused regions that form voxels of the
three-dimensional structure.
BRIEF DESCRIPTION OF THE DRAWINGS
[0013] These and other features and advantages will be better
understood by reading the following detailed description, taken
together with the drawings wherein:
[0014] FIG. 1 is a schematic diagram of a multiple beam additive
manufacturing system used to form a three-dimensional structure
from layers of powdered material, consistent with an embodiment of
the present disclosure.
[0015] FIG. 2 is a schematic diagram of a one-dimensional multiple
beam optical head for use in the multiple beam additive
manufacturing system, consistent with an embodiment of the present
disclosure.
[0016] FIG. 2A is a schematic diagram of the one-dimensional
multiple beam optical head shown in FIG. 2 with the imaging optics
in different positions to provide different beam spot sizes and
spacings, consistent with another embodiment of the present
disclosure.
[0017] FIG. 3 is a schematic diagram of a two-dimensional multiple
beam optical head for use in the multiple beam additive
manufacturing system, consistent with an embodiment of the present
disclosure.
[0018] FIGS. 4A-4D illustrate the formation of build layers of an
example three-dimensional structure in a powder bed by scanning
with a multiple beam optical head, consistent with embodiments of
the present disclosure.
[0019] FIG. 5A is a schematic diagram of beam spots and melt balls
resulting from a multiple beam distributed exposure, consistent
with embodiments of the present disclosure.
[0020] FIG. 5B is a schematic diagram of beam spots and melt balls
resulting from overlapping multiple beam distributed exposures,
consistent with embodiments of the present disclosure.
[0021] FIG. 6 is a graph of melt ball diameter as a function of
exposure time for a laser beam exposing powder layers of stainless
steel and cobalt chrome, respectively, using a multiple beam
additive manufacturing method, consistent with embodiments of the
present disclosure.
[0022] FIGS. 7A-7E illustrate different scan patterns for
one-dimensional multiple beam distributed exposures, consistent
with embodiments of the present disclosure.
[0023] FIG. 7F illustrates a scan pattern formed by interleaving
scan lines, consistent with another embodiment of the present
disclosure.
[0024] FIGS. 8A and 8B illustrate scan patterns for two-dimensional
multiple beam distributed exposures, consistent with embodiments of
the present disclosure.
[0025] FIG. 9 illustrates a scan pattern for an angled
one-dimensional multiple beam distributed exposure, consistent with
embodiments of the present disclosure.
[0026] FIG. 10 illustrates a scan pattern for a staggered
two-dimensional multiple beam distributed exposure, consistent with
embodiments of the present disclosure.
[0027] FIG. 11 is a photograph of a single layer solid structure
formed using multiple beam additive manufacturing, consistent with
an embodiment of the present disclosure.
[0028] FIG. 12 is a photograph of a single layer shaped structure
formed using multiple beam additive manufacturing, consistent with
an embodiment of the present disclosure.
[0029] FIG. 13 is a photograph of a multiple layer shaped structure
formed using multiple beam additive manufacturing, consistent with
an embodiment of the present disclosure.
[0030] FIG. 14 is a top view of a build layer illustrating
different resolutions in different regions of the build layer,
consistent with an embodiment of the present disclosure.
[0031] FIGS. 15A-15C are top schematic views of a multiple beam
optical head coupled to a powder delivery system for exposing a
powder layer as the powder layer is delivered, consistent with a
further embodiment of the present disclosure.
[0032] FIG. 16 is a top schematic view of a one-dimensional angled
multiple beam optical head coupled to a powder delivery system for
exposing a powder layer as the powder layer is delivered,
consistent with another embodiment of the present disclosure.
[0033] FIG. 17 is a top schematic view of a two-dimensional
staggered multiple beam optical head coupled to a powder delivery
system for exposing a powder layer as the powder layer is
delivered, consistent with another embodiment of the present
disclosure.
[0034] FIG. 18 is a side schematic view of a multiple beam optical
head coupled between hoppers of a powder delivery system for
exposing a powder layer as the powder layer is delivered,
consistent with yet another embodiment of the present
disclosure.
[0035] FIG. 19 is a schematic diagram of a multiple beam laser
additive manufacturing system including a polygon mirror for
scanning multiple beams, consistent with another embodiment of the
present disclosure.
[0036] FIG. 20 is a schematic diagram of multiple beam laser
additive manufacturing system including a galvo scanner for
scanning multiple beams, consistent with another embodiment of the
present disclosure.
[0037] FIG. 21 is a schematic diagram of a line of optical fiber
output ends being moved across a powder region to irradiate the
powder region and provide pre-heating, melting and controlled cool
down, consistent with yet another embodiment of the present
disclosure.
[0038] FIG. 22 is a schematic diagram of a two-dimensional array
including multiple lines of optical fiber output ends being moved
across multiple powder regions to irradiate the powder regions
simultaneously and provide pre-heating, melting and controlled cool
down, consistent with yet another embodiment of the present
disclosure.
[0039] FIG. 23 is a schematic diagram of a further embodiment of a
two-dimensional array including multiple lines of optical fiber
output ends being moved across multiple powder regions to irradiate
the powder regions simultaneously and provide pre-heating, melting
and controlled cool down.
DETAILED DESCRIPTION
[0040] Systems and methods for multiple beam additive
manufacturing, consistent with the present disclosure, use multiple
beams of light (e.g., laser light) to expose layers of powder
material in selected regions until the powder material fuses to
form voxels, which form build layers of a three-dimensional
structure. The light may be generated from selected light sources
and coupled into an array of optical fibers having output ends
arranged in an optical head in at least one line such that multiple
beams are sequentially directed by the optical head to the same
powder region providing multiple beam sequential exposures (e.g.,
with pre-heating, melting and controlled cool down) to fuse the
powder region. The multiple sequential beams may be moved using
various techniques (e.g., by moving the optical head) and according
to various scan patterns such that a plurality of fused regions
form each build layer.
[0041] By providing multiple beam sequential exposures with varying
intensity over a powder region to be fused, the solidification rate
may be controlled resulting in lower porosity and diminished
residual stresses. In another embodiment, a two-dimensional array
of optical fiber output ends may be moved such that multiple lines
of optical fiber output ends provide multiple beam sequential
exposures on multiple powder regions at different locations. The
beams may thus provide distributed multiple beam sequential
exposures forming a distributed exposure pattern with the multiple
beam sequential exposures spaced sufficiently to separate the fused
regions formed by each multiple beam exposure. By using distributed
multiple beam sequential exposures and by using certain scan
strategies, the multiple beam additive manufacturing system and
method may increase build speeds while reducing stresses caused in
the build layers.
[0042] The multiple beam additive manufacturing system, consistent
with embodiments described herein, may be used to form
three-dimensional structures for a wide range of three-dimensional
printing or rapid prototyping applications and from a variety of
materials depending upon the application. The powder material may
include, without limitation, metals, alloys and superalloys. More
specifically, the powder materials may include, without limitation,
powdered Ti-6Al-4V, nickel titanium or nitinol, nickel based
superalloys (e.g., austenite nickel-chromium-based superalloys
known as Inconel) aluminum, stainless steel and cobalt chrome.
Stainless steel 316L and cobalt chrome, for example, both provide
good corrosion resistance and high strength. Stainless steel may be
used, for example, for food processing or medical applications due
to its sterilisability and resistance to fatigue and shock. Cobalt
chrome may be used, for example, for medical implants due to its
high wear resistance and ability to form small features with high
strength. The powder material may also include any other powder
material known for use in powder bed fusion additive
manufacturing.
[0043] Because of the higher powers available when using multiple
lasers, particularly fiber lasers, the particle size of the powders
may not be an issue when using the multiple beam additive
manufacturing systems and methods described herein. The multiple
beam additive manufacturing systems and methods may be used with
powders having asymmetric particle sizes, including particle sizes
smaller than 5 .mu.m and particle sizes greater than 30 .mu.m. The
multiple beam additive manufacturing systems and methods may also
be used with powders having larger particle sizes, for example,
greater than 50 .mu.m.
[0044] As used herein, "exposure" refers to an exposure of light
for a defined period of time, "multiple beam distributed exposure"
refers to an exposure using multiple beams such that the beams
provide spaced exposures in different locations at substantially
the same time, and "multiple beam sequential exposure" refers to a
series of exposures using multiple beams on the same location. As
used herein, "powder material" refers to a material in the form of
particles suitable for use in powder bed fusion additive
manufacturing. As used herein, "fuse" refers to combining particles
of powder material together as a single structure as a result of
melting and/or sintering. As used herein, the terms "melt pool" and
"melt ball" are used interchangeably to refer to a
three-dimensional region of melted powder material formed by an
exposure to a light beam. A "melt pool" or "melt ball" may have a
generally spherical or spheroid shape but is not necessarily
limited to any particular shape. As used herein, a "fused region"
is a region of powder material that has been fused as a result of
an exposure of a light beam forming a "melt pool" or "melt ball"
and "distributed fused regions" refers to "fused regions" that are
separated and formed generally simultaneously by a multiple beam
distributed exposure. As used herein, a "voxel" is a unit of
three-dimensional space in a three-dimensional structure. A "voxel"
may correspond to a "melt pool" or "melt ball" or "fused region"
but is not necessarily the same size and shape as the melt pool or
melt ball or fused region.
[0045] Although the example embodiments described herein are used
primarily for powder additive manufacturing using metal powders,
the concepts described herein may be used with other materials and
other types of additive manufacturing using lasers or light. Other
materials may include, for example, resins, plastics, polymers and
ceramics.
[0046] Referring to FIG. 1, a multiple beam additive manufacturing
system 100, consistent with embodiments of the present disclosure,
is shown and described in greater detail. The multiple beam
additive manufacturing system 100 includes a powder bed support
system 110 for supporting a powder bed 102 formed by successive
layers of powder material 104 and a powder delivery system 120 for
delivering layers of the powder material 104 onto the powder bed
102. The build layers of the three-dimensional structure are formed
in the respective powder layers of the powder bed 102.
[0047] The multiple beam additive manufacturing system 100 also
includes an array of light sources 130 coupled to an array of
optical fibers 132 and an optical head 140 that arranges output
ends of the optical fibers 132 to direct multiple light beams 131
to a processing surface 106 including the exposed layer of the
powder bed 102. When forming a build layer in the exposed powder
layer on the powder bed 102, an exposure by one or more of the
light beams 131 melts the exposed powder material, which causes the
powder material to fuse in a fused region corresponding to a voxel
of the build layer. A multiple beam exposure with multiple beams at
different locations may thus form multiple voxels of a build layer
simultaneously. The light beams 131 may also be used to perform
other operations to facilitate melting and fusion of the powder
material, such as pre-heating and/or annealing.
[0048] In the illustrated embodiment, an optical head motion system
142 moves the optical head 140 relative to the powder bed 102 such
that the light beams 131 may be directed to different locations on
the powder bed 102 to form the voxels that make up the build layer.
The optical head motion system 142 may be capable of moving the
optical head 140 at speeds in a range of about 1-2 m/s, although
slower and faster speeds are possible. A control system 150
controls the powder bed support system 110, the powder delivery
system 120, the light sources 130, and the optical head motion
system 142 in coordination to form each of the build layers of the
three-dimensional structure. In particular, the control system 150
may cause the optical head 140 to be scanned across a powder layer
according to a scan pattern 10 (e.g., similar to a dot matrix
printer) while selectively activating light sources 130 such that
exposures by the light beams 131 selectively create melt pools and
fused regions that result in the individual voxels that form the
build layers of the three-dimensional structure. The optical head
140 may also be rotated with respect to the optical head motion
system 142.
[0049] The powder bed support system 110 lowers the powder bed 102
(e.g., in the direction of arrow 2) to accommodate each new layer
of powder material 104, thereby defining a build envelope 112 that
encompasses the powder bed 102 and the three-dimensional structure
formed therein. The powder bed support system 110 may include, for
example, a piston driven support platform (not shown). The powder
bed support system 110 lowers the powder bed 102 incrementally by
an amount corresponding to the desired thickness of each new powder
layer. The build envelope 112 is shown with a cuboid shape but may
also have a cylindrical shape. In one example, the powder bed
support system 110 defines a cylindrical build envelope with a
maximum build diameter of 100 mm and height of 70 mm and with a 25
.mu.m resolution for each powder layer.
[0050] The powder delivery system 120 includes a powder spreader
122, such as a roller or a wiper, for spreading each of the layers
of powder material 104 onto the powder bed 102. The powder delivery
system 120 may include, for example, a powder delivery piston (not
shown) that moves powder material upward to be engaged by the
powder spreader 122. In other embodiments, the powder delivery
system 120 may include one or more hoppers or similar devices that
deliver powder material from above the powder bed 102.
[0051] The powder bed 102 and processing surface 106 may be
enclosed in a processing chamber 160. The processing chamber 160
may be an air-tight chamber with a processing window (not shown) to
allow the light beams 131 to pass into the chamber 160 to the
powder bed 102. The processing chamber 160 may also be
atmospherically controlled to reduce oxidation effects when
performing the melting and fusion of the powder material. A vacuum
system 162 may be used to remove oxygen from the processing chamber
160. A gas supply 164 may supply an inert gas, such as argon, to
the processing chamber 160 to replace the oxygen.
[0052] The multiple beam additive manufacturing system 100 may
further include an optical coherence tomography (OCT) system 166 to
provide in-process metrology for each build layer. The OCT system
166 may use known OCT techniques to image the processing plane 106
at the location of one or more of the exposures to obtain size and
shape information about any melt pool. OCT may be an on-line single
point interferometric depth determination.
[0053] The array of light sources 130 may include an array of diode
lasers, such as high power multi-mode fiber-coupled diode lasers.
One example of such a diode laser is the PLD-33 series available
from IPG Photonics Corp., which is capable of up to 30 W of output
power in the 974 nm wavelength range (i.e., 958-980 nm) with a
coupled optical fiber having an aperture of 105-110 .mu.m, a fiber
cladding diameter of 125 .mu.m and a fiber buffer diameter of 250
.mu.m. Other diode lasers with other power outputs (e.g., 10, 60,
or 100 W) and/or other wavelengths may also be used. Diode lasers
of different power outputs and/or wavelengths may also be used in
the same array.
[0054] The output power of the diode lasers may be changed, for
example, by changing the drive current of the diode laser. This may
be done before each exposure to affect variable power delivery or
during exposure to affect pulse shaping. The energy delivered by
each exposure may be changed, for example, by changing the output
power, the pulse duration, pulse shape, and the focus or beam spot
size. The multiple beam additive manufacturing system 100 may thus
be scalable in power density.
[0055] In other embodiments, the array of light sources 130 may
include fiber lasers, such as a green fiber laser with a wavelength
of about 532 nm. Green fiber lasers may include pulsed (e.g.,
nanosecond) green fiber lasers with peak powers greater than 150 kW
and up to 400 kW, continuous wave fiber lasers with output powers
up to 50 W, and quasi-continuous wave (QCW) fiber lasers with
output powers up to 100 W or up to 500 W. Examples of such fiber
lasers include the GLR series single-mode, single-frequency
continuous wave green fiber lasers and the GLPN series high power,
single mode, quasi-continuous wave green fiber lasers available
from IPG Photonics Corp. Other fiber lasers at other wavelengths,
such as IR wavelengths (e.g., 1 micron, 1.5 micron, and 2 micron),
may also be used as light sources 130 in the multiple beam additive
manufacturing system 100. The fiber lasers are capable of providing
higher powers, for example, to fuse powder material with larger
particle sizes and/or higher melting temperatures.
[0056] These are only some examples of the light sources that may
be used in the multiple beam additive machining system 100. The
array of light sources 130 may include any type of light sources
capable of delivering light of sufficient power to melt and fuse
the powder material being used. In some instances, for example, a
higher power white light source may be sufficient.
[0057] In other embodiments, the light sources 130 may include one
or more light sources capable of performing other operations or
processes, for example, to facilitate melting and fusion of the
powder material and/or to form a finish surface on the
three-dimensional structure. Different light sources may be used,
for example, depending on the power and/or the beam characteristics
(e.g., beam quality and spot size) desired for a particular
processing operation. One or more multi-mode lasers producing lower
intensity beams and larger focused spot sizes may be used, for
example, to perform processes that do not require higher power
density and higher resolution, such as pre-heating the powder
and/or annealing the fused regions. Single mode lasers producing
higher intensity beams and smaller focused spot sizes may be used
for processes that do require higher power densities and higher
resolution, such as the melting that creates the voxels in the
powder material. One or more ultrafast lasers, such as picosecond
or femtosecond lasers, producing high peak power may be used, for
example, to form a laser induced periodic surface structure (LIPSS)
on a surface of the three-dimensional structure.
[0058] Although the multiple beam additive manufacturing system 100
is described as including the array of light sources 130 coupled,
respectively, to the array of fibers 132, additionally or
alternatively, the system 100 may include a single light source
coupled to multiple fibers. A single laser, for example, may be
split and coupled to multiple fibers to deliver multiple beams of
light for purposes of pre-heating, annealing, or other processes
that do not require higher power and higher resolution. In other
embodiments, the multiple beam additive manufacturing system 100
may include more than one optical head 140 coupled to other arrays
of light sources or to other single light sources.
[0059] Although the example embodiment uses the optical head 140 to
arrange output ends of optical fibers 132 to direct multiple beams
to the processing surface 106, other techniques and systems may be
used to direct multiple beams toward the processing surface 106 to
form an array of beam spots on the processing surface 106 for use
in the methods described herein. Multiple beams of light may be
directed toward the processing surface 106, for example, by
directing light sources (e.g., laser diodes) toward the processing
surface 106, using other types of laser processing heads (e.g.,
similar to laser welding heads) directed toward the processing
surface 106, and/or using mirrors or other optical components to
direct light beams toward the processing surface 106.
[0060] The optical head motion system 142 may include an X-Y motion
stage configured to move the optical head in at least X and Y
directions as indicated by arrows 6, 8. One example of the optical
head motion system 142 includes a CNC gantry system such as an
Aerotech.RTM. gantry system with an XYZ stage. Another example of
the optical head motion system 142 may include a printer-style
carriage for moving the optical head 140 above the processing
chamber 160. A printer-style carriage may be coupled, for example,
to the powder delivery system 120 such that the optical head 140
scans and exposes the powder layer as the layer is delivered, as
will be described in greater detail below. In other embodiments,
the beams 131 may be moved relative to the powder bed 102 by
scanning the beams using scanning optics such as a polygon mirror
or a galvo scanner, as will be described in greater detail
below.
[0061] The control system 150 controls the powder bed support
system 110, the powder delivery system 120, the light sources 130
and the optical head motion system 142 in coordination to form the
build layers of the three-dimensional structure. The control system
150 may control the powder bed support system 110, for example, by
controlling a stepper motor driving the piston in the powder bed
support system 110 to lower the powder bed 102 according to a
defined increment after forming each new build layer. The control
system 150 may thus control the thickness of each of the powder
layers and thus each of the build layers. The control system 150
may control the powder delivery system 120, for example, by
controlling a drive motor driving the powder spreader 122 to spread
each new layer of power material 104 over the powder bed 102 after
lowering the powder bed 102. The control system 150 may
automatically cause a re-layering of the powder after each build
layer by lowering the powder bed 102 by the defined layer thickness
and driving the powder spreader 122 to spread a new layer of powder
104 on the powder bed 102.
[0062] The control system 150 may also control the array of light
sources 130, for example, by controlling which light source is
activated or turned on, by controlling an output power, and by
controlling the duration of the emitted light (and thus the
exposure time). The control system 150 may further control the
movement and orientation of the optical head 140, for example, by
controlling the X-Y motors driving the optical head motion system
142 to position the optical head 140 according to a scanning
pattern or strategy. The control system 150 may thus cause light to
be generated selectively from the light sources 130 and selectively
directed to different locations on the powder bed 102 from the
optical head 140 with each exposure.
[0063] The control system 150 may receive build instructions 152
defining each of the build layers of a three-dimensional structure
and the operation of the bed support system 110, the powder
delivery system 120, the light sources 130 and the optical head
motion system 142 to form those build layers. The build
instructions 152 may include, for example, image slice data,
scanning data, layer thickness data, scan strip overlap data, and
energy distribution data. This data may be variable and may be
defined when the build instructions are generated. The image slice
data defines a series of binary images corresponding to planar
slices through a model of the three-dimensional structure and
corresponding to each of the build layers forming the
three-dimensional structure. The scanning data defines a scan
pattern or strategy such as a pattern of movement of the optical
head 140 relative to the powder bed 102 such that the multiple
beams are capable of selectively exposing any location on the
exposed layer of the powder bed 102. The strip overlap data defines
an amount of overlap between adjacent scan strips on the powder bed
102. The layer thickness data defines a thickness of each layer of
powder material and thus each build layer. The energy distribution
data defines the energy distribution of the light on the powder
including power and exposure time for each of the selected light
sources.
[0064] The build instructions 152 may be in the form of a file or
other data structure. The build instructions 152 may be produced
from a model of an object, for example, as represented by a CAD
file. Each line of the build instructions 152 may include a
position of the optical head 140, an identification of the light
source(s) to be activated at that position, and the exposure time
and power for each of the identified light source(s) to be
activated at that position. The build instructions 152 may thus
provide the data to form multiple voxels at each position of the
optical head 140 such that multiple positions of the optical head
140 produce all of the voxels in each build layer. The build
instructions 152 may also include re-layer instructions to initiate
a re-layering after each build layer is formed.
[0065] The control system 150 may include a CNC computer (e.g., a
PC) and/or microcontroller circuitry. In one example, the CNC
computer may read a build instruction file line by line to obtain
the position data and control the position of the optical head 140.
The CNC computer may send instructions to a microcontroller for
controlling the light sources 130 while the optical head 140 is in
each position. The CNC computer may also send instructions to the
powder bed support system 110 and the powder delivery system 120
for controlling the positions of the piston stepper motors and
powder spreader motor in the processing chamber to re-layer the
power. In one example of operation, the microcontroller may send a
busy signal to the CNC computer to halt reading instructions while
re-layering and may send a ready signal after re-layering is
complete. In another example, the microcontroller may receive build
instructions directly and may have sufficient processing power to
allow for autonomous operation without the CNC computer.
[0066] Referring to FIG. 2, one embodiment of a multiple beam
optical head 240 includes a one-dimensional array (i.e., a single
line) of n optical fiber output ends 234-1 to 234-n at the end of
an array of optical fibers 232-1 to 232-n coupled to respective
light sources 230-1 to 230-n (e.g., lasers). The one-dimensional
multiple beam optical head 240 is thus capable of producing up to n
light beams 231-1 to 231-n in a one-dimensional array. The number
and the pattern of the light beams 231-1 to 231-n produced in the
one-dimensional array may be changed by selectively activating the
light sources 230-1- to 230-n.
[0067] The one-dimensional multiple beam optical head 240 may
include a fiber positioning block 242 that positions and spaces the
optical fiber output ends 234-1 to 234-n. The optical head 240 may
also include optics such as one or more imaging optics 244 that
focus and direct focused beams 231-1 to 231-n to the processing
surface 206 such that adjacent focused beams 231-1 to 231-n are
spaced at the processing surface 206. The imaging optics 244 may
include a single lens focusing all of the beams or multiple lenses
(e.g., a microlens array) focusing the respective beams. Thus, the
beam spots produced by the beams 231-1 to 231-n on the powder layer
at the processing surface have a spacing that results in melt pools
and fused regions that are spaced accordingly. Although the output
ends are shown with a substantially equal spacing, the optical head
240 may also provide an unequal spacing.
[0068] The optical fiber output ends 234-1 to 234-n may be tight
packed in the block 242, for example, 10 fibers having a diameter
of 100 .mu.m may be tight packed within 1 mm. The beam spot size
and spacing is generally a function of the fiber core diameter, the
fiber spacing, and the focus of the beam. In some embodiments, the
imaging optics 244 may focus the beams 231-1 to 231-n such that the
focused adjacent beams 231-1 to 231-n have a beam spot size in a
range of 50 .mu.m to 300 .mu.m and a spacing in a range of about
150 .mu.m to 600 .mu.m at the processing surface 206. In another
example, single mode lasers may be used to obtain spot sizes as low
as 20 microns. In a further example, multimode fibers with a core
in the range of 100 to 110 microns may produce an imaged spot size
of 100 to 110 microns. When the fibers are tight packed, the center
to center spacing of the beams may correspond generally to the
fiber diameter, for example, 10 micron fibers tight packed may
provide a 10 micron spacing center to center and 100-110 micron
multimode fibers tight packed may provide roughly 100 to 110 micron
spacing. As will be discussed in greater detail below, the beam
spot size and spacing may be adjusted by adjusting the focus
relative to the processing surface.
[0069] When used in a multiple beam additive manufacturing system
and method, as described herein, the one-dimensional multiple beam
optical head 240 may be moved to different positions (e.g., in a
linear or non-linear scan pattern) while selectively activating one
or more of the light sources 230-1 to 230-n. At each position of
the optical head 240, for example, one or more of the light sources
230-1 to 230-n is turned on for a defined time and power (e.g., as
defined by the build instructions) to produce one or more beams
231-1 to 231-n and an exposure pattern including one or more beam
spots on the processing surface 206. When used to form a build
layer in a powder bed, for example, one or more of the light
sources 230-1 to 230-n are selectively activated (i.e., modulated)
to produce a pattern of light beams 231-1 to 231-n that will melt
and fuse regions of a powder layer corresponding to the voxels of
the build layer.
[0070] As shown in FIG. 2A, the multiple beam optical head 240
and/or the imaging optics 244 may be moved to different positions
to change the focus of the beams 231 relative to the processing
surface 206a-c. Changing the focus of the beams 231 changes the
mark-to-space ratio and thus changes the spot size, the spacing,
and the power density of the beam spots. FIG. 2A illustrates three
different degrees of focus and the beam spots 233a-c produced at
the respective processing surfaces 206a-c. When the beams are in
focus on the processing surface 206a (i.e., the processing surface
206a is in the focal plane), the beam spots 233a may have a
minimized spot size and maximized power density but the spacing is
larger. When the beams are defocused relative to the processing
surface 206b, 206c (i.e., the processing surface is out of the
focal plane), the beam spots 233b, 233c may have a larger spot size
and lower power density and a smaller spacing. Thus, the multiple
beam optical head 240 may adjust the focus to provide overlapping
beam spots for certain applications that do not require the higher
power density and resolution. The beam spot size may be varied, for
example, for different materials and/or for different regions of a
build layer as described in greater detail below.
[0071] Thus, a spacing between beams spots in a distributed
exposure pattern may be provided by focusing the beams on the
processing surface and the spacing may be adjusted by changing the
focus. A spacing between beams spots in a distributed exposure
pattern may also be provided by using non-adjacent beams in the
multiple beam distributed exposure. If the beams are defocused, for
example, such that adjacent beam spots are not spaced (e.g., the
beam spots 233c in FIG. 2A), the light sources may be selectively
activated such that the exposures do not use adjacent beams.
[0072] Referring to FIG. 3, another embodiment of a multiple beam
optical head 340 includes a two-dimensional array of n.times.m
optical fiber output ends 334-1 to 334-n, 334-m. The
two-dimensional array generally includes two or more columns n of
optical fiber output ends 334-1 to 334-n and two or more rows m of
optical fiber output ends 334-1 to 334-m. The optical fiber output
ends 334 in each row and column may be aligned as shown or may be
staggered to create an exposure pattern with staggered beam spots.
Although the two-dimensional array is shown as a rectangular array,
the two-dimensional array may have other shapes and
configurations.
[0073] Similar to the one-dimensional multiple beam optical head
240, the optical fiber output ends 334-1 to 334-n, 334-m are
located at the ends of optical fibers coupled to respective light
sources (not shown in FIG. 3). The two-dimensional multiple beam
optical head 340 is thus capable of producing up to n.times.m light
beams 331-1 to 331-n, 331-m in a two-dimensional array. The number
and the pattern of the light beams 331-1 to 331-n, 331-m produced
in the two-dimensional array may be changed by selectively
activating the light sources.
[0074] The two-dimensional multiple beam optical head 340 includes
a fiber positioning block 342 that positions and spaces the optical
fiber output ends 334-1 to 334-n, 334-m. The two-dimensional
multiple beam optical head 340 also includes optics such as imaging
optics 344 for focusing the multiple beams 331 toward the
processing surface 306 to form an array of spaced beam spots. The
spacing of the adjacent focused beams 331-1 to 331-n, 331-m
produced by the two-dimensional multiple beam optical head 340 may
be within the same range of the one-dimensional multiple beam
optical head 240 described above. The two-dimensional multiple beam
optical head 340 and/or imaging optics 344 may also be adjusted to
adjust the focus and the beam spot size and spacing as described
above.
[0075] When used in a multiple beam additive machining system and
method, as described herein, the two-dimensional multiple beam
optical head 340 may be moved to different positions (e.g., in a
linear or non-linear scan pattern) while selectively activating one
or more of the light sources. At each position of the optical head
340, for example, one or more of the light sources may be turned on
for a defined time and power (e.g., as defined by the build
instructions) to produce one or more beams 331-1 to 331-n, 331-m
and an exposure pattern including beam spots on the processing
surface 306. When used to form a build layer in a powder bed, for
example, one or more of the light sources are selectively activated
to produce a pattern of light beams 331 that will melt and fuse
regions of a powder layer corresponding to voxels of the build
layer.
[0076] In an embodiment, the two-dimensional multiple beam optical
head 340 provides a two-dimensional array of beams that is smaller
than the surface area of a powder layer on the powder bed. In this
embodiment, the two-dimensional multiple beam optical head 340 is
thus moved or scanned across the powder layer to provide exposures
across the entire powder layer. In another embodiment, the
two-dimensional multiple beam optical head 340 may provide a
two-dimensional array large enough to cover substantially the
entire surface area of a powder layer on the powder bed. In this
embodiment, the two-dimensional multiple beam optical head 340 is
capable of exposing an entire surface area of the powder layer with
only a small number of local movements depending on the spacing of
the beam spots.
[0077] In another embodiment, a multiple beam optical head may be
modular and configurable to create the different arrays (e.g., one
or two dimensional) of different dimensions. The fiber positioning
blocks that hold and position the optical fiber output ends, for
example, may be configured to be connected together. Thus, multiple
one-dimensional arrays of optical fiber output ends may be
connected together to form a larger one-dimensional array or a
two-dimensional array, or multiple two-dimensional arrays of
optical fiber output ends may be connected together to form a
larger two-dimensional array.
[0078] Although embodiments described herein refer to optical
fibers with circular cross sections producing circular beam spots,
a multiple beam additive manufacturing system and method may also
use optical fibers with other cross sections such as square.
Additional optics may also be used to modify the shape of the beam
spot. Although the illustrated embodiments show the optical heads
directing the beams orthogonally toward the processing surface, the
optical head may also be tilted to direct the beams at an angle
relative to the processing surface.
[0079] FIGS. 4A-4D illustrate an example of the formation of build
layers of a three-dimensional structure 401 using a multiple beam
optical head 440, consistent with embodiments of the present
disclosure. Although this example shows a one-dimensional multiple
beam optical head 440, a two-dimensional multiple beam optical head
may also be used in the same manner. In this example, the three
dimensional structure 401 has side sections 403a, 403b and a top
section 405 and is formed by a series of build layers 408-1 to
408-7 that together form the side sections 403a, 403b and the top
section 405. Each of the build layers 408-1 to 408-7 is made up of
voxels and each of the voxels is formed when powder fuses as a
result of an exposure by one or more of the beams 431 emitted from
the multiple beam optical head 440.
[0080] As shown, successive powder layers 402-1 to 402-7 are
deposited on the powder bed 402 and the multiple beam optical head
440 is moved to different locations relative to the powder layers
402-1 to 402-7 to expose each of the powder layers in selected
regions with one or more of the beams 431 to form the voxels that
make up each of the build layers. In particular, the exposures from
the beams 231 melt at least a portion of the powder within the
exposed region (i.e., the beam spot) and through the powder layer
to form respective fused regions 406 that correspond to respective
voxels in the build layer 408. The energy from each of the
exposures by the beams 431 penetrates the powder layer sufficiently
for the fused regions 406 to extend to and join with any fused
region or voxel at the same location in a previous build layer. For
example, the voxel or fused region 406a shown in FIG. 4A is joined
with a corresponding voxel in the previous build layer 408-1. The
thickness of the powder layer thus determines the depth of each
voxel and the build resolution. For some structures or for some
portions of a structure, a thicker layer of powder material may be
used with a higher output power of the light.
[0081] As shown, the optical head 440 may perform multiple beam
distributed exposures using the beams 431 to form corresponding
distributed melt pools and distributed fused regions 406. By moving
the optical head 440 according to a scan pattern and providing the
multiple beam distributed exposures at a plurality of different
positions of the optical head 440, the distributed fused regions
406 may be joined together to form the build layer. In other words,
subsequent multiple beam distributed exposures fill in the spaces
between the distributed fused regions 406. Forming distributed melt
pools and fused regions allows multiple beams to be used to
increase build speeds while also de-localizing the thermal energy
to reduce the thermal part stress. Joining the fused regions or
voxels at a later time allows the thermal stresses to disperse.
Various scan patterns and strategies may be used to join the
distributed fused regions 406 in a build layer, as will be
described in greater detail below. The fused regions 406 are shown
as rectangular shaped for illustrative purposes only and may have
other shapes such as a cylindrical or spheroid shape.
[0082] FIGS. 4A and 4B show the formation of the side sections
403a, 403b of the structure 401 in the build layer 408-2 by using
multiple beams 431 to perform distributed exposures on the powder
layer 402-2 along relatively narrow strips corresponding to the
side sections 403a, 403b. FIGS. 4C and 4D show the formation of the
top section 405 of the structure 401 in the build layers 408-5,
408-7 by using multiple beams 431 to perform distributed exposures
across the respective powder layers 402-5, 402-7 over a larger area
corresponding to the top section 405.
[0083] As shown in FIG. 5A, a multiple beam distributed exposure
531 provides a distributed exposure pattern including a plurality
of spaced beam spots 533a, 533b having a beam spot size D and a
spacing S. Each of the beam spots 533a, 533b produces a
corresponding melt ball 506a, 506b (and fused region). When the
beam has a Gaussian intensity profile, the lower energy at the
outside regions of the beam may result in the melt ball 506a, 506b
having a smaller size than the beam spots (e.g., a smaller diameter
d). To join the fused regions, therefore, a plurality of multiple
beam distributed exposures are overlayed such that the melt balls
overlap to fill the spaces between the melt balls 506a, 506b formed
by the distributed exposure 531.
[0084] As shown in FIG. 5B, the spaces between the melt balls 506a,
506b may be filled by using a plurality of multiple beam
distributed exposures overlayed on a grid having a grid pitch P.
This allows distributed fused regions to be joined together by
subsequent distributed exposures. In this example, the grid pitch P
and spacing S is such that two melt balls are placed within the
space between the melt balls 506a, 506b formed by the multiple beam
distributed exposure 531 using two beam spots from two subsequent
exposures. This is not a limitation of the present disclosure,
however, because the pitch P, spacing S, beam size D, melt ball
size d, and number of melt balls filling the space may vary. FIG.
5B shows an overlap that is sufficient to minimize any interstitial
air between the melt balls; however, the overlap may be greater or
less than the overlap shown in FIG. 5B.
[0085] The size of the melt pool or melt ball 506a, 506b may depend
on the type of powder material, the power of the light beam, the
size of the beam spot, and the exposure time. FIG. 6 illustrates
melt ball diameter as a function of exposure time for stainless
steel 316L and cobalt chrome. In this example, the light source is
a diode laser with a power of 30 W and a wavelength of 974 nm and
the beam is focused to a spot size of about 300 microns. As shown,
stainless steel 316L, despite having a higher melt temperature,
forms larger melt balls than cobalt chrome for a given exposure
time. Thus, absorption and specific heat should be taken into
consideration when characterizing the melt ball creation process
for a particular powder material.
[0086] Various scan patterns may be used to overlay the multiple
beam distributed exposures on a grid as described above. FIGS.
7A-7E illustrate several interleaved scan patterns (or scan
strategies) using a distributed exposure pattern 733 including a
one-dimensional array of three spaced beam spots. This distributed
exposure pattern 733 may be produced, for example, by
one-dimensional array of at least three optical fibers. Distributed
exposure patterns with other numbers of beam spots may be produced
with other numbers of optical fibers.
[0087] This distributed exposure pattern 733 produces a
corresponding melt pattern of three spaced melt balls, which
results in a corresponding pattern of three spaced fused regions or
voxels. Subsequent multiple beam distributed exposures may be made
using this same distributed exposure pattern 733 to join together
the corresponding distributed fused regions within a scan region
735. Because the size of the melt ball may be smaller than the size
of the corresponding beam spot that produces the melt pool, as
discussed above, the beam spots in the subsequent multiple beam
distributed exposures may overlap accordingly. It may also be
possible to produce a melt pool or melt ball that is larger than
the beam spot, for example, by increasing the power and/or exposure
time.
[0088] As illustrated in FIGS. 7A-7E, each scan pattern includes a
series of local movements by the optical head in different axes,
thereby interleaving the exposure pattern 733 to fill the spaces
between the beam spots and cover a scan region 735, which
corresponds to a section of a build layer. The grid size of the
scan region 735 may be a function of the number of beam spots in
the exposure pattern 733, the spacing between the beam spots, and
the movements in the scan pattern. In this example with three beam
spots and three exposures to fill the spaces, the scan regions 735
are formed with nine (9) overlapping beam spots along the length.
In particular, FIGS. 7A-7D show scan regions 735 with a 3.times.9
grid size and FIG. 7E shows a scan region 735 with a 5.times.9 grid
size.
[0089] The arrows in FIGS. 7A-7E indicate the direction of each
local movement of the optical head in the X and Y axes to each
local position for producing each subsequent multiple beam
distributed exposure until the scan region is covered. If all of
the beams are exposed at each of these positions, a solid build
layer section is formed within the scan region 735 by the melt
balls corresponding to the beam spots. By selectively activating
the light sources and selectively producing the beam spots in each
of the different positions, a build layer section with a different
pattern or shape may be formed in the scan regions 735. These local
movements may be repeated at a series of locations such that
multiple scan regions 735 form a scan strip across a powder bed.
Multiple scan strips may be overlapped (e.g., with a defined scan
strip overlap) as needed to cover an entire powder layer and form a
complete build layer.
[0090] FIG. 7F illustrates a further example of interleaving in a 5
beam system. In this example, each letter represents a different
beam and each column represents a successive scan. The powder
material may be fused and filled in one scan line at a time without
neighboring scan lines being imaged together at the same time. In
other words, the interleaving technique is used with multiple beams
that are not adjacent or contiguous to fill in between the scan
lines.
[0091] Interleaving may provide several benefits in additive
manufacturing. In particular, interleaving allows the imaging
process to proceed as a smooth motion in the slow scan direction.
If a contiguous array of beam spots is used, they would be imaged
in a block and the slow scan direction would step forward by the
size of the array. By interleaving single beam spots in a
non-contiguous array, the array may be stepped in the slow scan
direction in smaller steps.
[0092] Interleaving non-contiguous scan lines also allows each scan
line to be imaged with consistent characteristics. Because adjacent
scan lines are not be imaged at the same time, the base material in
the adjacent areas is not being fused and thus is cold. Laser
additive manufacturing with a metal powder is a thermal process on
a thermally conductive material. If a contiguous array is used, the
center of the array is much hotter than the edge of the array
resulting in different imaging characteristics in the center than
at the edges. The fused material at the edges will thus have
different properties, for example, resulting in visible stripes.
The structure of the fused material is improved when adjacent beams
are not affecting the temperature. When interleaving the scan
lines, therefore, the temperature is more consistent across the
beam spot array and across the scan lines formed by the array.
[0093] FIGS. 8A and 8B illustrate interleaved scan patterns (or
scan strategies) using a two-dimensional distributed exposure
pattern 833 to cover a scan region 835. The two-dimensional
distributed exposure pattern 833 may be scanned according to any of
the interleaved scan patterns shown in FIGS. 7A-7E.
[0094] FIG. 9 illustrates a linear scan pattern using an angled
one-dimensional distributed exposure pattern 933. In this example,
the angled one-dimensional distributed exposure pattern 933 is
angled relative to the linear scan direction such that a beam spot
will be overlapped by an adjacent beam spot in a subsequent
exposure. As such, the angled one-dimensional distributed exposure
pattern 933 may be scanned along one axis and does not require
movement in the other axis to fill the spaces between the beam
spots.
[0095] FIG. 10 illustrates a linear scan pattern using a staggered
two-dimensional distributed exposure pattern 1033. In this example,
the beam spots are staggered such that a beam spot will be
overlapped by an adjacent beam spot in a subsequent exposure. As
such, the staggered two-dimensional distributed exposure pattern
1033 may be scanned along one axis and does not require movement in
the other axis to fill the spaces between the beam spots.
[0096] FIGS. 11-13 show structures that were built using one
embodiment of a multiple beam additive manufacturing system and
method. Each of these objects were built from stainless steel 316L
powder having a particle size of greater than 5 .mu.m and smaller
than 53 .mu.m. The system included seven diode lasers having a
wavelength of about 974 nm and a power of about 30 W coupled to
seven optical fibers arranged in a one-dimensional array and
closely packed in the optical head.
[0097] FIG. 11 shows a single layer solid rectangular structure
including 50 by 21 melt balls (or voxels). This single layer solid
rectangular structure was built using the scanning strategy shown
in FIG. 7A and exposure times of about 5 ms for each diode laser.
FIG. 12 shows a single layer 261.times.64 voxel structure forming
the lettering of the "IPG" logo. This structure was built on a grid
of pitch 0.15 mm with a two pixel overlap between scan strips and
an exposure time of 5 ms for each voxel. FIG. 13 shows a multiple
layer structure forming the lettering of the "IPG" logo. This
multiple layer structure was built using ten build layers on a grid
pitch of 0.15 mm with a two pixel overlap between scan strips and
an exposure time of 10 ms per voxel. An anchor pillar (not shown)
was used at each corner of the multiple layer structure to affix
the build to a substrate to prevent cumulative stress from
distorting the structure. The use of a vacuum system to remove
residual oxygen and back fill with an inert gas may reduce
oxidization and improve inter-layer consolidation in a multiple
layer build. Oxidization may also be reduced where re-melting
occurs, for example, at the stitching overlap.
[0098] Another embodiment of a multiple beam additive manufacturing
system and method may be used to provide different resolutions, for
example, by using different beam spot sizes. Smaller beam spot
sizes generally produce smaller melt balls/fused regions/voxels and
thus higher resolutions. Larger beam spot sizes generally produce
larger melt balls/fused regions/voxels and thus lower resolutions.
The beam spot size may be controlled, for example, by adjusting the
focus as described above. Different light sources or lasers may
also be used to provide different beam spot sizes and resolutions.
This embodiment may use a single larger beam and a single smaller
beam and/or may use multiple larger beams and multiple smaller
beams.
[0099] In one example, a larger beam spot size may be in a range of
400-500 .mu.m and a smaller beam spot size may be in a range of
50-70 .mu.m. The larger spot may be used to fuse the bulk of the
material and the smaller spot may then be used to perform fine
details and/or edge finishing. In this embodiment, a large multi kW
laser may be used at a higher output power (e.g., 500 W-5 kW) for
the larger spots and at a lower output power (e.g., 100-400 W) for
the smaller spots.
[0100] As shown in FIG. 14, for example, the larger sized beam
spots 1433 may be used in the interior regions 1403 of the
structure 1401 and the smaller sized beam spots 1435 may be used on
the outer regions 1405 of the structure 1401 where higher
resolutions are desired. Using larger beam spot sizes and lower
resolutions on a substantial portion of the structure 1401 enables
faster build rates. Using smaller beam spots 1435 and higher energy
density proximate the edges provides a smother surface finish on
the outer surface of the structure 1401 when built.
[0101] In a further embodiment, as shown in FIGS. 15A-15C, a
multiple beam additive manufacturing system includes a multiple
beam optical head 1540 that follows the delivery of each layer of
powder such that the multiple beams scan the powder bed 1502 as
each powder layer is delivered. The multiple beam optical head 1540
may be coupled, for example, to the powder spreader apparatus 1520
that moves across the powder bed. As the powder spreader apparatus
1520 moves in a linear direction across the powder bed 1502, as
indicated by arrow 4, to spread the powder layer, for example, the
multiple beam optical head 1540 scans back and forth in an
orthogonal direction, as indicated by arrows 8, similar to a
printer carriage.
[0102] At each position, the optical head 1540 may provide a
multiple beam distributed exposure to form a pattern of distributed
fused regions 1506 (FIG. 15B). The distributed fused regions 1506
are joined to form the build layer of the structure 1501 by
performing subsequent distributed exposures as the spreader
apparatus 1520 continues to move across the powder bed (FIG. 15C).
Scanning and exposing the powder layer as the layer is delivered
avoids having to wait for the entire powder layer to be delivered
before starting the scanning and exposure process and thus may
further increase build rates.
[0103] In another variation of this embodiment, shown in FIG. 16, a
multiple beam optical head 1640 includes an angled one-dimensional
array. This multiple beam optical head 1640 provides an angled
distributed exposure pattern that may be scanned, for example, as
shown in FIG. 9, as a powder spreader apparatus 1620 moves across a
powder bed 1602. In yet another variation, shown in FIG. 17, a
multiple beam optical head 1740 includes a staggered
two-dimensional array. This multiple beam optical head 1740
provides a staggered, two-dimensional distributed exposure pattern
that may be scanned, for example, as shown in FIG. 10, as a powder
spreader apparatus 1720 moves across a powder bed 1702. The angle
of the exposure pattern may also be variable and controlled during
the build process to control the spacing of the melt pools.
[0104] In a further embodiment, shown in FIG. 18, a multiple beam
optical head 1840 is coupled directly to a powder delivery system.
In this embodiment, the multiple beam optical head 1840 is mounted
between powder delivery hoppers 1820a, 1820b and spreaders 1822a,
1822b. As the hoppers 1820a, 1820b move across the powder bed 1802
(e.g., in the direction of arrow 4), powder 1804 is released from
the leading hopper 1820b and spread using the leading spreader
1822b. The multiple beam optical head 1840 scans back and forth
across the powder bed in an orthogonal direction as described above
and shown in FIGS. 15-17. A powder bed support platform 1810 lowers
the powder bed 1802 after each build layer of the structure 1801 is
formed.
[0105] In another embodiment, shown in FIG. 19, a multiple beam
additive manufacturing system 1900 may include a polygon mirror
1942 for scanning multiple beams 1931 according to any of the
patterns described herein. An array of light sources 1930
selectively generates light that is directed by a multiple beam
optical head 1940 to the polygon mirror 1942, which scans the beams
1931 across the powder bed 1902, for example, while performing
distributed exposures. The polygon mirror may be capable of
scanning the beams at speeds of 50 m/s. In this embodiment, the
light beams 1931 may be scanned over the powder bed 1902 as the
powder layer is being delivered (e.g., following the motion of a
powder spreader). The powder bed 1902 may be moved in a direction
orthogonal to the scanning direction to allow the multiple beams
1931 to be scanned across different regions of the powder bed
1902.
[0106] In a further embodiment, shown in FIG. 20, a multiple beam
additive manufacturing system 2000 may include a galvanometer
scanner 2042 for scanning multiple beams 2031 according to any of
the patterns described herein. The galvo scanner 2042 may include
one or more scan mirrors for scanning in at least one direction.
For larger parts, a second galvo scanner may be provided to scan in
the perpendicular direction. For smaller parts, the galvo scanner
2042 may include a piezo mirror or a scan mirror driven by a voice
coil to scan in the perpendicular direction.
[0107] An array of light sources 2030 selectively generates light
that is directed by a multiple beam optical head 2040 to the galvo
scanner 2042, which scans the beams 2031 across the powder bed
2002, for example, while performing distributed exposures. The
optical head 2040 may provide substantially collimated beams to the
galvo scanner and may include one or more zoom lenses (not shown)
to vary the beam spot sizes. An F-theta scan lens 2045 to focus the
beams 2031 on the powder bed 2002 when scanning.
[0108] In this embodiment, the light beams 2031 may be scanned over
the powder bed 2002 as the powder layer is being delivered (e.g.,
following the motion of a powder spreader). The powder bed 2002 may
also be moved to allow the multiple beams 2031 to be scanned across
different regions of the powder bed 2002.
[0109] In an optical system that is radially symmetric, a multiple
beam scanning system may be designed to scan an array of beams, as
described above, with the array being arranged in different ways
(e.g., different numbers of beams in different patterns or
orientations). If a radially symmetric system is designed to
accommodate an array of .+-.4 mm from the central axis, for
example, it does not matter how many beams are generated within
that 8 mm range or the orientation of those beams. In such a
system, therefore, the array may be changed or reconfigured without
changing the optics. For example, the array may be customized to
the application (e.g., the material, the size of the part,
etc.).
[0110] Multiple beam additive manufacturing systems and methods may
reconfigure the beams in a two-dimensional array to allow different
and more efficient scanning patterns. Multiple beam additive
manufacturing systems and methods are not required to scan back and
forth or up and down to form each build layer of a part. A multiple
beam additive manufacturing system and method may scan a build
layer by following the outline of the part (referred to as random
access systems), which may be more efficient and allow faster build
speeds. In such random access systems, the interleaving may be set
up so that a two-dimensional array is used but only some of the
beams are imaging, depending upon the orientation of the scan line.
For a circular part, for example, instead of going back and forth
and turning the beams on only when they cross the boundaries of a
wall of the part (as shown, for example, in FIGS. 15A-15C), the
array may be scanned around the circular shape. As the array moves
around the circular shape, the array is oriented differently with
respect to the direction of travel, so different sets of beams in
the array would be turned on at different times accordingly. When
interleaving as shown in FIG. 7F, for example, different sets of
beams in the array may correspond to each of the interleaving beams
A-E at different times.
[0111] Multiple beam additive manufacturing systems and methods
with two-dimensional arrays may also use leading beams and trailing
beams to pre-heat and post heat, respectively. Pre-heating and
post-heating the material regulates the temperature profile to
prevent the material from heating up and cooling down too fast.
[0112] When a single high energy beam is focused on the powder
region at a fixed laser power, the metal powder turns from solid to
liquid in a short period of time. When the single beam moves,
however, the liquid metal solidifies at a rate that is not
controlled. The solidification process of a metal or metal alloy
may affect the engineering properties of a product formed by
melting and solidifying that metal or metal alloy. In some powder
bed fusion LAM experiments, a continuous wave (CW) laser diode was
used with a power of about 65 W, a spot size of about 150 .mu.m,
and scanning speeds between 10-80 mm/s to melt various metal
powders (i.e., stainless steel 316L, Ni-based superalloy Inc625,
and Co--Cr alloy) with average powder particle sizes between 20-53
.mu.m. In these experiments, the goal was to form up to
approximately 120 layers of a layer thickness between 30-200 .mu.m
(e.g., layers of 30, 50, 75, 100, 150 and 200 .mu.m). These
experiments resulted in samples having a near 100% density for 316L
and Inc625 powders with porosity ranges between 0.2-1.2 vol %. Some
samples produced from Inc625, however, were observed to have severe
cracks, which could be primarily attributed to the high and
non-controlled solidification rate. The surface roughness was also
higher than desired.
[0113] Instead of using one focused beam scanning over a powder
region to be fused, multiple beams may be scanned sequentially over
the same powder region to provide more heat sources (e.g., from
multiple laser diodes). When laser diodes are used as the heat
sources, for example, the laser characteristics of each diode
(e.g., the power) can be controlled to control pre-heating and/or
post-heating or cool down, thereby controlling the solidification
rate. The control of the solidification rate of an alloy may lead
to the manufacturing of single crystal alloys (i.e., alloys having
no grain boundaries) having improved mechanical properties, such as
higher creep resistance and corrosion resistance, which can be
maintained at higher temperatures. Such a process would be
suitable, for example, to manufacture turbine blades.
[0114] In one example experiment using multiple beams to expose the
same powder region to provide controlled solidification, an array
of 12 diodes were used at different powers up to about 40 W to
provide pre-heating, melting and controlled cool down of an Inc625
alloy powder. The powder particle size, spot size and scan speeds
were the same as the experiment described above with the single
beam. The preliminary results of this experiment produced samples
with a porosity below 0.05% and a smoother surface finish than
those produced by the single beam method. Controlling the
solidification rate may thus diminish the residual stresses, which
may allow production of substantially crack free Ni-based
superalloys (e.g., austenite nickel-chromium-based superalloy) from
LAM processes. Using multiple beams also resulted in an accumulated
effect of the power from each of the diodes, which enabled the
lower maximum power of 40 W (as compared to 65 W) as well as an
increased layer thickness of 200 .mu.m (as compared to 50 .mu.m).
By enabling increased layer thicknesses, the build rate may thus be
increased when multiple beam exposures are used on the same powder
region being fused.
[0115] Referring to FIG. 21, an example of a multiple beam
sequential exposure for providing controlled solidification is
shown and described in greater detail. In this example, a plurality
of output ends 2134 of optical fibers are arranged in a line
forming a one-dimensional array. These optical fiber output ends
2134 may be fixed in an optical head with the optical fibers
coupled to light sources (e.g., laser diodes), for example, as
described in embodiments discussed above. The optical fiber output
ends 2134 may also have the sizes and spacings discussed above and
may be configured to produce beam spots having a size in a range of
10 to 500 .mu.m and a spacing in a range of 0 to 600 .mu.m.
Although the illustrated embodiment shows 12 optical fiber output
ends 2134 (e.g., coupled to 12 laser diodes), other numbers of
fibers and diodes may be used depending upon the desired material,
speeds and metallurgical results.
[0116] Each of the optical fiber output ends 2134 emits a beam of
light generated from a coupled light source. By moving the line of
optical fiber output ends 2134 in the direction of the line as
indicated by the arrow while generating the light from the light
sources, the beams of light are sequentially directed to the same
powder region 2106 providing a multiple beam sequential exposure to
fuse the powder region. The line of optical fiber output ends 2134
may be scanned across the powder region 2106 in the direction of
the line, for example, using a motion stage as described above. The
line of optical fiber output ends 2134 may then be moved to other
locations to fuse other powder regions on a powder layer with
multiple beam sequential exposures, for example, by raster
scanning, thereby forming a build layer of a three-dimensional
structure.
[0117] To provide controlled solidification, the multiple beam
sequential exposure provides a varying intensity of light, for
example, by using different laser diode powers. One example of the
varying intensity of light, as shown in FIG. 21, provides lower
intensities for pre-heating, higher intensity for melting and lower
intensities for cool down (or post-heating). The varying intensity
of light may thus provide a temperature profile 2140 that prevents
the material from heating up and cooling down too fast. In this
example, the intensity profile 2142 represents the intensity of
light of the beams emitted from the respective optical fiber output
ends 2134, which may be produced by providing different power
levels from laser diodes coupled to the respective optical fiber
output ends 2134. The temperature profile 2140 and intensity
profile 2142 are for illustrative purposes only and may not
represent actual profiles.
[0118] In one embodiment, pre-heating may be produced by one or
more optical fiber output ends 2134a at a beginning of the line,
melting may be provided by one or more optical fiber output ends
2134b at a middle of the line, and cool down may be provided by one
or more optical fiber output ends 2134c at an end of the line. In
the illustrated example, the pre-heating may be produced by a
stepped increase in power (e.g., 10 W, 20 W, 30 W, 40 W) across the
optical fiber output ends 2134a at the beginning, a highest power
(e.g., 50 W) across the optical fiber output ends 2134b at the
middle, and a stepped decrease in power (e.g., 40 W, 30 W, 20 W, 10
W) across the optical fiber output ends 2134c at the end. In the
illustrated example, this intensity profile provides a longer cool
down than pre-heating to control the solidification rate, although
this is not necessarily a requirement or limitation.
[0119] Although one example is illustrated, other varying
intensities or intensity profiles producing other temperature
profiles are possible and within the scope of the present
disclosure. The multiple beam exposure, for example, may provide
longer or shorter pre-heating, melting and cool down periods, only
pre-heating and melting, only melting and cool down, or alternating
periods of higher and lower intensities (and temperatures). The
desired temperature profile may depend on the scanning speed, the
type of material, the particle sizes, the feature sizes, and/or the
desired metallurgical results.
[0120] FIGS. 22 and 23 show embodiments of a two-dimensional array
of optical fiber output ends used to provide a plurality of
multiple beam sequential exposures. As shown in FIG. 22, the
optical fiber output ends 2234 may be arranged in a series of lines
to provide multiple beam sequential exposures simultaneously on a
plurality of different powder regions 2206. The lines may be spaced
such that the multiple beam sequential exposures are distributed to
form distributed fused regions simultaneously. As shown in FIG. 23,
the optical fiber output ends 2334 may also be arranged in a
staggered two-dimensional array with staggered lines to provide
multiple beam sequential exposures simultaneously on different
powder regions 2206. The optical fiber output ends 2234, 2334 are
scanned in the direction of the lines to provide the multiple beam
sequential exposures forming the distributed fused regions and may
be moved to other locations and/or scanned using scan patterns
and/or strategies (e.g., interleaved scan patterns) discussed above
for distributed fused regions.
[0121] In further embodiments, an array of beam spots for use in
any of the methods described herein may be created using techniques
other than an array of output ends of optical fibers coupled to an
array of light sources. In one example, an array of light sources
may be arranged over a processing surface to direct or focus light
beams on the processing surface to form a one or two dimensional
array of beam spots. In another example, a plurality of laser
processing heads (e.g., such as the type used for laser welding)
may be arranged over a processing surface to direct or focus light
beams on the processing surface to form a one or two dimensional
array of beam spots. In a further example, mirrors and/or other
optical components may be used to direct light beams on a
processing surface to form a one or two dimensional array of beam
spots.
[0122] Accordingly, multiple beam additive manufacturing systems
and methods, consistent with the present disclosure, may be used to
reduce thermal part stresses, reducing cracking, improving surface
finish and/or improve build speeds.
[0123] While the principles of the invention have been described
herein, it is to be understood by those skilled in the art that
this description is made only by way of example and not as a
limitation as to the scope of the invention. Other embodiments are
contemplated within the scope of the present invention in addition
to the exemplary embodiments shown and described herein.
Modifications and substitutions by one of ordinary skill in the art
are considered to be within the scope of the present invention,
which is not to be limited except by the following claims.
* * * * *