U.S. patent application number 11/271098 was filed with the patent office on 2007-05-10 for lightweight nacelle for turbines and methods for making same.
This patent application is currently assigned to General Electric Company. Invention is credited to Ronald Ralph Cairo.
Application Number | 20070104934 11/271098 |
Document ID | / |
Family ID | 38004098 |
Filed Date | 2007-05-10 |
United States Patent
Application |
20070104934 |
Kind Code |
A1 |
Cairo; Ronald Ralph |
May 10, 2007 |
Lightweight nacelle for turbines and methods for making same
Abstract
A lightweight nacelle includes a plurality of wound carbon
fibers embedded in an epoxy matrix around a hollow region. The
nacelle is made by a process that includes winding the plurality of
carbon fibers around a mandrel.
Inventors: |
Cairo; Ronald Ralph; (Greer,
SC) |
Correspondence
Address: |
PATRICK W. RASCHE (22402)
ARMSTRONG TEASDALE LLP
ONE METROPOLITAN SQUARE, SUITE 2600
ST. LOUIS
MO
63102-2740
US
|
Assignee: |
General Electric Company
|
Family ID: |
38004098 |
Appl. No.: |
11/271098 |
Filed: |
November 10, 2005 |
Current U.S.
Class: |
428/292.1 |
Current CPC
Class: |
Y10T 428/249924
20150401; D04H 3/07 20130101; Y02P 70/50 20151101; F03D 80/00
20160501; Y02E 10/72 20130101; F05B 2230/20 20130101; F05B 2240/14
20130101 |
Class at
Publication: |
428/292.1 |
International
Class: |
D04H 13/00 20060101
D04H013/00 |
Claims
1. A lightweight nacelle comprising a plurality of wound carbon
fibers embedded in an epoxy matrix around a hollow region, and
having rounded corners.
2. A nacelle in accordance with claim 1 wherein said wound carbon
fibers are pre-impregnated, pitch-based carbon fibers.
3. A nacelle in accordance with claim 2 wherein said fibers are
selected for predetermined strength requirements, stiffness
requirements, or both.
4. A nacelle in accordance with claim 2 wherein said fibers include
fibers oriented to provide axial strength and stiffness.
5. A nacelle in accordance with claim 4 wherein said fibers include
fibers wound in a +/-10 degree orientation.
6. A nacelle in accordance with claim 2 wherein said fibers include
fibers oriented to provide torsional stiffness and strength.
7. A nacelle in accordance with claim 6 wherein said fibers include
fibers wound in +/-45 degree orientation.
8. A nacelle in accordance with claim 2 wherein said fibers include
fibers oriented to provide lateral strength and stiffness.
9. A nacelle in accordance with claim 6 wherein said fibers include
fibers wound at a 90 degree orientation.
10. A nacelle in accordance with claim 1 having a thickened dome
region and rounded corners.
11. A wind turbine having a nacelle in accordance with claim 1, a
rotor having a least one blade, and a generator.
12. A method for making a nacelle comprising winding a plurality of
carbon fibers embedded in an epoxy matrix around a mandrel.
13. A method in accordance with claim 12 wherein said winding a
plurality of carbon fibers comprises winding a plurality of
pre-impregnated, pitch-based carbon fibers.
14. A method in accordance with claim 13 further comprising
preselecting said fibers in accordance with predetermined strength
requirements, stiffness requirements, or both.
15. A method in accordance with claim 13 wherein said winding a
plurality of carbon fibers comprises orienting and winding fibers
to provide axial strength and stiffness.
16. A method in accordance with claim 15 wherein said orienting and
winding said fibers to provide axial strength and stiffness
comprises winding said fibers in a +/-10 degree orientation.
17. A method in accordance with claim 13 wherein said winding a
plurality of fibers comprises orienting and winding fibers to
provide torsional stiffness and strength.
18. A method in accordance with claim 17 wherein said orienting and
winding fibers to provide torsional stiffness and strength
comprises winding said fibers in a +/-45 degree orientation.
19. A method in accordance with claim 13 wherein said winding a
plurality of fibers comprises orienting and winding fibers to
provide lateral strength and stiffness.
20. A method in accordance with claim 19 wherein said orienting and
winding fibers to provide lateral strength and stiffness include
winding said fibers in a 90 degree orientation.
Description
BACKGROUND OF THE INVENTION
[0001] This invention relates generally to methods for
manufacturing of nacelles for turbines and for nacelles made by
such methods. Configurations of the present invention are
applicable to many different types of turbines, and are
particularly advantageous for wind turbines.
[0002] At least one known nacelle configuration introduces
substantial weight at the top of each wind turbine tower. The high
weight at the top of the wind tower tends to increase cost and
decrease reliability and life of wind turbines. In addition, this
nacelle configuration includes a large cutout to accommodate a
power shaft. This cutout introduces flexibility to the structure
and requires local reinforcing and/or stiffening members.
BRIEF DESCRIPTION OF THE INVENTION
[0003] One aspect of the present invention therefore provides a
lightweight nacelle that includes a plurality of wound carbon
fibers embedded in an epoxy matrix around a hollow region, and
having rounded corners.
[0004] Another aspect of the present invention provides a method
for making a nacelle that includes winding a plurality of carbon
fibers embedded in an epoxy matrix around a mandrel.
[0005] It will thus become apparent that configurations of the
present invention provide a low-cost, structurally efficient
nacelle.
BRIEF DESCRIPTION OF THE DRAWINGS
[0006] FIG. 1 is a pictorial schematic drawing representing the
winding of carbon fibers embedded in an epoxy matrix as in some
configurations of the present invention.
[0007] FIG. 2 is a pictorial drawing of a nacelle representative of
some configurations of the present invention.
[0008] FIG. 3 is a partial planar cross-section of the nacelle of
FIG. 2 taken in plane 3 of FIG. 2.
[0009] FIG. 4 is a configuration of wind turbine using the nacelle
of FIGS. 2 and 3.
DETAILED DESCRIPTION OF THE INVENTION
[0010] Some configurations of the present invention utilize an
automated process in which a composite pre-impregnated tape/tow
winding is used to fabricate a pitch-based carbon fiber epoxy
nacelle for turbine engines. Pitch-based carbon fibers are
inexpensive and readily available in a wide variety of strengths
and stiffness, thereby allowing the structural response of the
nacelle to be tuned to any of various preselected design
criteria.
[0011] In some configurations of the present invention and
referring to FIG. 1, carbon fibers embedded in a low-cost epoxy
matrix in either tape or tow format are wound around a mandrel.
Suitable carbon fibers include, but are not necessarily limited to,
pre-impregnated pitch-based carbon fibers. Fiber architecture can
be tuned for predetermined strength and stiffness requirements. For
example, the fibers can be wound +/-10-degree orientation for axial
strength and stiffness (0-degrees is not possible with the winding
process due to the winding poles), .+-./-45-degree orientation for
torsional stiffness and strength, and 90-degree orientation for
lateral strength and stiffness. A thicker, dome (i.e., pole) region
is a byproduct of some configurations of the present invention and
provides natural reinforcement for the shaft cutout. Also, in some
configurations of the present invention, rounded corners result
from limitations in composite material winding. These rounded
corners are also advantageous because they result in aerodynamic
surfaces that are less likely to produce flow separation or vortex
trails, which are vibration drivers, in high wind gusts. The
winding can be performed using an automated process to produce a
lighter weight, higher quality, nacelle structure due to
well-controlled manufacturing conditions.
[0012] Thus, and referring to FIG. 1, some configurations of the
present invention comprise a lightweight nacelle 10. Nacelle 10
itself comprise a plurality of carbon fibers 12 embedded in an
epoxy matrix 14 and wound around a mandrel 16, which is
subsequently removed to leave behind a hollow region 60 (best seen
in FIGS. 2 and 3). Mandrel 16 may comprise an inflatable
elastomeric to facilitate removal. Wound carbon fibers 12 in some
configurations are pre-impregnated, pitch-based carbon fibers,
which may be selected to satisfy predetermined strength
requirements, stiffness requirements, or both.
[0013] Carbon fibers 12 in some configurations include fibers
oriented to provide axial strength and stiffness. For example, in
some configurations, fibers 12 include fibers 50 that are wound in
a .theta.=.+-.10 degree orientation. In some configurations, carbon
fibers 12 include fibers oriented to provide torsional stiffness
and strength, which may, for example, include fibers 52 wound in a
.theta.=.+-.45 degree orientation. And in some configurations,
fibers 12 include fibers 54 oriented to provide lateral strength
and stiffness. For example, nacelle 10 may include fibers 12 wound
at a 90 degree orientation.
[0014] In many configurations and referring to FIGS. 2 and 3,
nacelle 10 has a thickened dome region 18 and rounded corners
20.
[0015] Referring to FIG. 4, nacelle 10 configurations of the
present invention are particularly suitable for use in wind
turbines 22 which have a rotor 24 having a least one blade 26, and
a generator (not shown, but inside nacelle 10). In many
configurations, three blades 26 are provided for aerodynamic
efficiency.
[0016] In some configurations, a method for making a nacelle 10 is
provided that comprises winding a plurality of carbon fibers 12
embedded in an epoxy matrix 14 around a mandrel 16. The plurality
of carbon fibers 12 can comprise pre-impregnated, pitch-based
carbon fibers. In some configurations, the method further includes
preselecting the fibers in accordance with predetermined strength
requirements, stiffness requirements, or both.
[0017] The winding a plurality of carbon fibers 12 in some
configurations further comprises orienting and winding fibers to
provide axial strength and stiffness. For example, orienting and
winding the fibers to provide axial strength and stiffness can
comprise winding the fibers in a .+-.10 degree orientation.
[0018] Winding a plurality of fibers 12 in some configurations
comprises orienting and winding fibers to provide torsional
stiffness and strength. For example, orienting and winding fibers
to provide torsional stiffness and strength can comprise winding
the fibers in a .+-.45 degree orientation.
[0019] Winding a plurality of fibers 12 ins some configurations
comprises orienting and winding fibers to provide lateral strength
and stiffness. For example, orienting and winding fibers to provide
lateral strength and stiffness can include winding fibers in a 90
degree orientation.
[0020] While the invention has been described in terms of various
specific embodiments, those skilled in the art will recognize that
the invention can be practiced with modification within the spirit
and scope of the claims.
* * * * *