U.S. patent application number 09/848886 was filed with the patent office on 2001-08-30 for reusable, separable, structural connector assembly.
This patent application is currently assigned to Planetary Systems Corporation. Invention is credited to Holemans, Walter.
Application Number | 20010017337 09/848886 |
Document ID | / |
Family ID | 23101213 |
Filed Date | 2001-08-30 |
United States Patent
Application |
20010017337 |
Kind Code |
A1 |
Holemans, Walter |
August 30, 2001 |
Reusable, separable, structural connector assembly
Abstract
An easy to use, and reuse, separation connector is disclosed
that comprises a first component having a plurality of leaf
elements with protrusions, and a second component having a recess
for receiving the leaf element protrusions. The protrusions of the
leaf elements are secured within the recess by a tensioned band, or
in an alternative embodiment, by an expansion band; the protrusions
and recess are formed so as to provide an efficient and effective
load and torque bearing surface that requires minimal tension on
the tensioned band, or minimal compression on the expansion band. A
shearing structure is also presented that minimizes translation of
the leaf elements with respect to the receiving surface. When the
band is released, springs or other means urge the leaves away from
the mating surface, thereby allowing for the separation of the
connected items. Preferably, the leaves are hinged, allowing for
ease of coupling and decoupling to the mating surface. Multiple
sections of leaf elements can be employed to form a perimeter
structure corresponding to the structure of the mating surface.
Inventors: |
Holemans, Walter;
(Washington, DC) |
Correspondence
Address: |
ROBERT M MCDERMOTT, ESQ.
16 SAMUELSON ROAD
WESTON
CT
06883
|
Assignee: |
Planetary Systems
Corporation
Washington
DC
|
Family ID: |
23101213 |
Appl. No.: |
09/848886 |
Filed: |
May 4, 2001 |
Related U.S. Patent Documents
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Application
Number |
Filing Date |
Patent Number |
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09848886 |
May 4, 2001 |
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09287038 |
Apr 6, 1999 |
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6227493 |
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Current U.S.
Class: |
244/158.1 |
Current CPC
Class: |
B64G 1/645 20130101;
B64G 1/641 20130101 |
Class at
Publication: |
244/158.00R |
International
Class: |
B64G 001/00 |
Claims
I claim:
50. A separation connector assembly comprising: a first connector
device comprising: a plurality of leaf elements, each leaf element
of the plurality of leaf elements having a leaf lip that includes a
first mating surface, a second connector device comprising: a
receiving surface having a second mating surface substantially
corresponding to an inverse of the first mating surface for
receiving each leaf lip of the plurality of leaf elements, a band
that is configured to form a perimeter within the plurality of leaf
elements, and is further configured to urge each leaf lip into the
receiving surface, via an expansion of a circumference of the band,
thereby facilitating a coupling of the first connector device to
the second connector device.
51. The separation connector assembly of claim 50, wherein the
first mating surface includes a protrusion and the second mating
surface includes a recess.
52. The separation connector assembly of claim 50, wherein the
first mating surface includes a recess and the second mating
surface includes a protrusion.
53. The separation connector assembly of claim 50, wherein: the
plurality of leaf elements are arranged on the first connector
device such that the leaf lips of the plurality of leaf elements
form a first leaf lip perimeter, the receiving surface has a
receiving perimeter having an inclined slope that deforms the
plurality of leaf elements such that the leaf lips form a second
leaf lip perimeter when the receiving perimeter is urged into the
first leaf lip perimeter, and the band is configured to reform the
first leaf lip perimeter.
54. The separation connector assembly of claim 50, further
including a means for urging the first connector device apart from
the second connector device.
55. The separation connector assembly of claim 50, further
including a means for coupling an electrical signal from the first
connector device to the second connector device.
56. The separation connector assembly of claim 50, further
including an expansion device that is configured to effect the
expansion of the circumference of the band.
57. The separation connector assembly of claim 50, wherein at least
one of the plurality of leaf elements is configured to retain the
band.
58. The separation connector assembly of claim 50, wherein at least
one of the first connector device, the second connector device, the
plurality of leaf elements, and the band includes an aluminum
alloy.
59. The separation connector assembly of claim 50, further
including decoupling elements that include at least one of: a
spring, a plunger, a piston, and a percussion device, and are
configured to disengage the leaf elements from the receiving
surface.
60. The separation connector assembly of claim 59, wherein the
second connector device is radially stiffened by a step that forms
an ancillary mounting surface, and the decoupling elements are
affixed to the ancillary mounting surface.
61. The separation connector assembly of claim 50, wherein each
leaf element includes a hinge to facilitate movement of the leaf
lip into and away from the receiving surface.
62. The separation connector assembly of claim 50, wherein the
first connector device and the second connector device are
configured such that, when the first connector device is coupled to
the second connector device, the plurality of leaf elements is in a
substantially unstressed state.
63. The separation connector assembly of claim 50, wherein the
first and second mating surfaces include a shearing structure that
is configured to minimize a lateral movement of the plurality of
leaf elements relative to the receiving surface when the first
connector device is coupled to the second connector device.
64. A vehicle comprising: a plurality of leaf elements, each leaf
element of the plurality of leaf elements having a leaf lip that
includes a mating surface that substantially corresponds to an
inverse of a receiving surface on an other vehicle, a band that is
configured to urge each leaf lip of the plurality of leaf elements
into the receiving surface, via an expansion of a circumference of
the band, thereby fixedly adhering the vehicle to the other
vehicle.
65. The vehicle of claim 64, further comprising: a means for urging
the vehicle away from the other vehicle.
66. The vehicle of claim 64, further comprising: a coupling device
that is configured to facilitate the expansion of the circumference
of the band.
67. The vehicle of claim 66, wherein the coupling device is further
configured to facilitate a reduction of the circumference of the
band.
68. The vehicle of claim 64, wherein the plurality of leaf lips and
the receiving surface are configured such that, when the vehicle is
coupled to the other vehicle, the plurality of leaf elements is in
a substantially unstressed state.
69. The vehicle of claim 64, wherein each leaf element includes a
hinge to facilitate movement of the leaf lip into and away from the
receiving surface.
70. The vehicle of claim 64, wherein the mating and receiving
surfaces include a shearing structure that is configured to
minimize a lateral movement of the plurality of leaf elements
relative to the receiving surface.
71. A spacecraft system comprising: a first vehicle, a second
vehicle, a coupler that is configured to couple the first vehicle
to the second vehicle, and a decoupler that is configured to
decouple the first vehicle from the second vehicle; wherein: the
first vehicle comprises a plurality of leaf elements, each leaf
element of the plurality of leaf elements having a leaf lip that
includes a mating surface that substantially corresponds to an
inverse of a receiving surface on the second vehicle, the coupler
includes: a band that is configured to urge each leaf lip of the
plurality of leaf elements into the receiving surface, via an
expansion of a circumference of the band, and the decoupler
includes decoupling elements that are configured to urge each leaf
lip away from the receiving surface.
72. The spacecraft system of claim 71, wherein: the plurality of
leaf elements are arranged on the first vehicle such that the leaf
lips of the plurality of leaf elements form a first leaf lip
perimeter, the second vehicle has a receiving perimeter about the
receiving surface that has an inclined slope that deforms the
plurality of leaf elements such that the leaf lips form a second
leaf lip perimeter when the receiving perimeter of the second
vehicle is urged into the first leaf lip perimeter, and the
expanded band substantially reforms the first leaf lip
perimeter.
73. The spacecraft system of claim 71, further including an
expansion device that is configured to expand the circumference of
the band.
74. The spacecraft system of claim 71, wherein the expansion device
is further configured to reduce the circumference of the band.
75. The spacecraft system of claim 71, further including a means
for communicating an electrical signal from the first vehicle to
the second vehicle.
76. The spacecraft system of claim 71, wherein the plurality of
leaf lips and the receiving surface are configured such that, when
the first vehicle is coupled to the second vehicle, the plurality
of leaf elements is in a substantially unstressed state.
77. The spacecraft system of claim 71, wherein each leaf element
includes a hinge to facilitate movement of the leaf lip into and
away from the receiving surface.
78. A method of attaching a first vehicle to a second vehicle, the
first vehicle comprising a plurality of leaf elements, each leaf
element of the plurality of leaf elements having a leaf lip that
includes a mating surface that substantially corresponds to an
inverse of a receiving surface on the second vehicle, the leaf lips
of the plurality of leaf elements forming a first lip perimeter
that substantially corresponds to an inclined receiving perimeter
about the receiving surface on the second vehicle, the method
comprising the steps of: positioning the first vehicle and the
second vehicle so as to align the first lip perimeter with the
inclined receiving perimeter, urging the first vehicle and the
second vehicle together so as to deform the plurality of leaf
elements via the inclined receiving perimeter to form a second lip
perimeter that is larger than the first lip perimeter, and urging
each of the leaf lips into the receiving surface via an expansion
of a circumference of a band within a perimeter formed by the
plurality of leaf elements, thereby substantially reforming the
first lip perimeter.
79. A method of detaching a first vehicle from a second vehicle,
the first vehicle comprising a plurality of leaf elements, each
leaf element of the plurality of leaf elements having a leaf lip
that is mated to a receiving surface on the second vehicle via an
expansion of a circumference of a band within a perimeter formed by
the plurality of leaf elements, the method comprising the steps of:
reducing the circumference of the band, urging each leaf lip of the
plurality of leaf elements away from the receiving surface on the
second vehicle, and urging the first vehicle and the second vehicle
apart.
80. A separation connector assembly comprising: a first connector
device comprising a plurality of leaf elements, each leaf element
of the plurality of leaf elements having a leaf lip that includes a
first mating surface, a second connector device comprising a
receiving surface having a second mating surface substantially
corresponding to an inverse of the first mating surface for
receiving each leaf lip of the plurality of leaf elements, a band
that is configured to form a perimeter corresponding to the
plurality of leaf elements, and is further configured to urge each
leaf lip into the receiving surface, via at least one of a
tensioning and an expansion of a circumference of the band, thereby
facilitating a coupling of the first connector device to the second
connector device, wherein: the plurality of leaf elements are
arranged on the first connector device as discrete segments of leaf
elements that form a perimeter corresponding to the receiving
surface of the second connector device.
81. A separation connector assembly comprising: a first connector
device comprising a plurality of leaf elements, each leaf element
of the plurality of leaf elements having a leaf lip that includes a
first mating surface, a second connector device comprising a
receiving surface having a second mating surface substantially
corresponding to an inverse of the first mating surface for
receiving each leaf lip of the plurality of leaf elements, a band
that is configured to form a perimeter corresponding to the
plurality of leaf elements, and is further configured to urge each
leaf lip into the receiving surface, via at least one of a
tensioning and an expansion of a circumference of the band, thereby
facilitating a coupling of the first connector device to the second
connector device, wherein: the first and second mating surfaces
include a shearing structure that is configured to minimize a
lateral movement of the plurality of leaf elements relative to the
receiving surface when the first connector device is coupled to the
second connector device.
Description
CROSS REFERENCE TO RELATED APPLICATIONS
[0001] This is a Continuation-In-Part of application Ser. No.
09/287,038, filed Apr. 6, 1999.
BACKGROUND OF THE INVENTION
[0002] 1. Field of the Invention
[0003] This invention relates to the field of mechanical
connectors, and in particular to connector assemblies for stage
separation systems, such as satellite and missile systems.
[0004] 2. Description of Related Art
[0005] Transport systems, such as rockets that transport satellites
into space, vessels that transport submerged sections of ocean
structures such as oil platforms, and the like, require a means for
securely fastening different items together for transport, and
reliably and easily unfastening the items for deployment.
Multi-stage rockets also require a means for fastening the stages
together, and reliably unfastening the stages as each stage is
spent. In other situations, such as aircraft carrier based
aircraft, the items are transported or stored in a disassembled
state and require a means for rapidly fastening the items for
deployment, and reliably and easily unfastening the items for
subsequent storage or transport.
[0006] A variety of devices have been developed to secure two items
together while also allowing the items to be separated quickly and
reliably. In the aerospace industry, the common connection devices
include bolts and bands that can be severed. Bolts are used to
fasten the two items together, and an explosive charge is typically
used to sever the bolts at the proper time, thereby unfastening the
two items. Depending upon the application, ancillary devices such
as springs may be used to urge the two items apart when the bolts
are severed. To assure a reliable separation, the number of bolts
used to fasten the two items is kept to a minimum; this results in
load points at the bolts far in excess of the load imposed by a
distributed fastening system.
[0007] Belt structures are commonly used to provide for a
distributed load. A belt structure that is commonly employed to
fasten items together is a "V-band", typified by U.S. Pat. No.
4,715,565, incorporated by reference herein. The V-band includes a
tension belt for securing a plurality of retainers against camming
surfaces on flange members on separable spacecraft component parts.
A typical V-band embodiment consists of an upper ring attached to
the payload, a lower ring attached to the launch vehicle, and a
clampband that is circumferentially tensioned to the flanges of the
upper and lower rings, as illustrated in FIG. 1. The upper ring 101
and lower ring 102 each have flanges that, when joined, form a "V"
shaped projection 150A. The clampband consists of a belt 110 and a
plurality of clamps 120. Each of the clamps 120 has a recess 150B
corresponding to the shape of the projection 150A of the upper 101
and lower 102 rings. When the belt 110 is tensioned, the recesses
150B of the clamps 120 are compressed against the projections 150A,
thereby securing the upper 101 and lower 102 rings together.
[0008] The belt 110 is conventionally tensioned by bolts (not
shown) that are in line with the belt 110, and explosive bolt
cutters are used to sever the bolts to release the tension. When
the tension in the belt 110 is released, the clamps 120 are free to
separate from the projection 150A, thereby decoupling the upper 101
and lower 102 rings. The conventional V band structure also
includes means, such as springs, for urging the clamps 120 apart
from the projection 150A, to provide for a reliable separation.
Means are also provided to retain the belt 110 and clamps 120 after
separation, to minimize the occurrence of "space junk".
[0009] For V-bands to work properly, the tension required in the
tensioning belt 110 is relatively high (about 3800 pounds for a 38
inch diameter; 6800 pounds for a 66 inch diameter). This high
tension requires radial stiffeners in the rings 101, 102. The
sudden release of this stored energy generates high shock, and
imposes additional requirements on the means used to retain the
fast moving belt and clamps after separation. Because of the high
tension requirements, the combined weight of the belt, clamps, and
ancillary required devices is substantial (as much as 25 pounds for
a 38 inch diameter V-band structure). The high tension requirements
of V-bands often require specialized tools and instruments to
tension the band. The high tension and high release shock effects
also limits the reliable life of the components, thereby limiting
the amount of testing that can be applied to the components that
are actually flown.
[0010] Another structure that is commonly used to provide for an
easily separable connection is an explosive frangible joint, as
typified by U.S. Pat. Nos. 4,685,376 and 5,390,606. An explosive
detonating cord is placed within a contained space that forms the
frangible joint between the two items. Separation is achieved by
detonating the cord within the contained space, forcing a rapid
crack propagation through the frangible joint. Although the weight
of an explosive frangible joint is less than that of an equivalent
sized V-band, it is still substantial (as much as 17 pounds for a
38 inch diameter joint). The destructive nature of this separation
system precludes testing of the joints that are actually flown.
[0011] Each of the aforementioned separation connectors also
imparts a substantial shock to the connected items upon separation,
and the explosive nature of the devices used for separation
introduce a risk of personal injury, particularly during pre-launch
assembly and testing. Because of the shock effects, such separation
connectors are not commonly used on items that are routinely
disassembled for storage or transport.
BRIEF SUMMARY OF THE INVENTION
[0012] It is an object of this invention to provide a separation
connector that is light weight. It is a further object of this
invention to provide a separation connector that allows for
repeated testing. It is a further object of this invention to
provide a separation connector that allows for separation with
minimal shock effects. It is a further object of this invention to
provide a method for connecting components that is simple, secure,
and reliable. It is a further object of this invention to provide a
connector component that is stiff, strong, and easy to use.
[0013] These objects and others are achieved by a separation
connector that comprises a plurality of leaves with leaf lips that
are secured within a mating surface by a tensioned band in one
embodiment, and a compression band in another embodiment. The
leaves and mating surface are designed such that the tension or
compression required on the band is significantly less than the
tension required on a V-band. A shear structure is also provided
that minimizes translation of the leaves with respect to mating
surface. In a preferred embodiment, the tensioned band is
detensioned by a thermal device that melts, decomposes, or severs
the band, and the compressed band is decompressed by a contraction
or removal of an expansion element. When the band is detensioned or
decompressed, springs urge the leaves away from the mating surface,
thereby allowing for the separation of the connected items.
Preferably, the leaves are hinged, allowing for ease of coupling
and decoupling to the mating surface. Multiple sections of leaf
elements can be employed to form a perimeter structure
corresponding to the structure of the mating surface.
BRIEF DESCRIPTION OF THE DRAWINGS
[0014] The invention is explained in further detail, and by way of
example, with reference to the accompanying drawings wherein:
[0015] FIG. 1 illustrates an example prior art V-band separation
connector.
[0016] FIG. 2 illustrates an example separation connector in
accordance with this invention.
[0017] FIGS. 3A-3D illustrate the coupling of two items via an
example separation connector in accordance with this invention.
[0018] FIG. 4 illustrates an example vehicle coupling system in
accordance with this invention.
[0019] FIG. 5 illustrates an example tension and detension system
in accordance with this invention.
[0020] FIG. 6 illustrates an example spring mechanism for urging a
separation of the separation connector in accordance with this
invention.
[0021] FIG. 7 illustrates an alternative example separation
connector in accordance with this invention.
[0022] FIGS. 8A-8E illustrate an example embodiment of a leaf
element of a separation connector in accordance with this
invention.
[0023] FIG. 9 illustrates an example electrical connector of a
separation connector in accordance with this invention.
[0024] FIGS. 10A-10F illustrate example alternative configurations
of the leaf elements of separation connectors in accordance with
this invention.
[0025] FIG. 11 illustrates an example dual separation connector in
accordance with this invention.
[0026] FIG. 12 illustrates an example hinged leaf element in
accordance with this invention.
[0027] FIGS. 13A-13B illustrate an example alternative
configuration wherein the coupling is achieved via an expansion
ring that holds each leaf element in position via compression in
accordance with this invention.
DETAILED DESCRIPTION OF THE INVENTION
[0028] FIG. 2 illustrates an example separation connector 200 for
connecting an upper ring 201 and lower ring 202 in accordance with
this invention. For ease of understanding, the invention is
presented in the context of an aerospace transport system; other
applications will be evident to one of ordinary skill in the art in
view of the principles presented herein. The upper 201 and lower
202 rings are typically fastened to the items being connected (401,
402 in FIG. 4), such as a launch vehicle and satellite.
Alternatively, the upper 201 and lower 202 rings may be an integral
part of the items being connected. As used herein, the terms
"upper", "lower", and "rings" are used for ease of reference and
understanding. Alternative arrangements, configurations, and
orientations will be evident to one of ordinary skill in the art,
in view of the principles of the invention presented herein. Also
for ease of reference, various aspects of the invention are
initially disclosed with regard to an example configuration wherein
the leaf elements form an outer perimeter about a mating surface. A
complementary arrangement, having the mating surface forming the
outer perimeter, is also presented, and illustrated in FIG. 13. The
application of each of the aspects of this invention to the
complementary structure of FIG. 13 will be evident to one of
ordinary skill in the art.
[0029] The example separation connector 200 includes leaf elements
210 secured to the lower ring 202 that each have a leaf lip 211
that conforms to a recess 212 in the upper ring 201. The leaf
elements 2 10 also include a filament groove 214 that is used to
position a filament (320 in FIG. 3D) about a perimeter formed by
the leaf lips 211. As discussed below, the leaf elements 210 are
typically circularly arranged, although other arrangements may be
used to conform to alternatively shaped connected items. An eight
leaf configuration is illustrated in FIG. 2 for clarity, although
additional leaf elements may be employed. For example, a preferred
embodiment for Athena, Atlas, Delta, Pegasus, and other launch
vehicles, uses 59 leaf elements 210 for a 38 inch diameter upper
201 and lower 202 ring design. Also illustrated in FIG. 2 are eight
spring elements 230 with plungers 231 whose function is detailed
below; in a preferred embodiment, two spring elements 230 are
provided per leaf element 210. In a preferred embodiment of this
invention, the upper 201 and lower 202 rings are radially stiffened
by introducing a circumferential step 206, 207 in each. In the
upper 201 and lower 202 rings, the stepped surfaces 208, 209 serve
as the mounting surface for ancillary devices, such as the spring
elements 230 and other devices discussed further herein.
[0030] FIGS. 3A-3D illustrate a detailed view of the operation of
the separation connector 200 for connecting the upper 201 and lower
202 rings. In FIG. 3A, the upper ring 201 is urged 300 into the
leaf elements 210 of the lower ring 202. In accordance with one
aspect of this invention, the leaf elements 210 are arranged so
that the unbiased position of the leaf lips 211 conform to the
location of the recess 212 in the upper ring 201; that is, in a
preferred embodiment, when the leaf lip 211 is seated in the recess
212, the leaf element 210 is in a substantially unbiased and
unstressed position. The upper ring 201 is shaped to provide an
inclined perimeter surface 305 that deforms the leaf elements 210
outward 310 as the upper ring 201 is urged 300 into the leaf
elements 210.
[0031] FIG. 3B illustrates the result of further downward urging
300 on the upper ring 201. The spring element 230 is designed to
exert a force, via the plunger 231, that is larger than the
resilient inward force exerted by the resilience of the deformed
leaf element 210. That is, the spring element 230 and plunger 231
are designed such that the urging 300 of the upper ring 201 into
the leaf elements 210 continues to deform the leaf element 210
outward 310.
[0032] FIG. 3C illustrates the result of further downward urging
300 on the upper ring 201. In a preferred embodiment, the leaf
element 210 is designed to provide a surface 316 that operates in
conjunction with a surface 306 on the upper ring 201 to resist
downward movement of the upper ring 201 when the leaf lip 211 of
the leaf element 210 is adjacent the matching recess 212 in the
upper ring 201.
[0033] In accordance with this invention, a circumferential band or
filament 320 is placed in the filament groove 214 of the leaf
element 210, and tensioned to exert an inward force 321 to urge the
leaf lips 211 of the leaf elements 210 into the conforming recess
212 in the upper ring 201. In a preferred embodiment of this
invention, the filament 320 is a polymer having a high strength and
stiffness to weight ratio, such as KEVLAR.TM. (Dupont) or
VECTRAN.TM. (Hoechst Celanese). It is significant to note that the
tension of the filament 320 need only overcome the aforementioned
force of the springs 230 in order to urge the leaf lips 211 into
the recess 212. For improved load bearing potential, the filament
320 is further tensioned, as discussed below. It is also
significant to note that in the tensioned position of FIG. 3D, the
leaf elements 210 are in their substantially unstressed,
non-deformed, positions, thereby providing near maximum load
bearing potential. The leaf lip 211 of each leaf element 210 and
the recess 212 of the upper ring 201 are designed to conform as
closely as practical, thereby distributing the potential
compression and expansion loads throughout the bearing surfaces 311
of the leaf lip 211 and recess 212. As discussed below with
reference to FIGS. 8A-8D, to reduce manufacturing costs, the leaf
element 210 is preferably flat, whereas the recess 212 is typically
curved, and some stress is introduced as the flat leaf element 210
is tensioned to conform to the recess 212. In a preferred
embodiment, each leaf element 210 is less than two inches long and
the perimeter of the upper ring 201 at the recess 212 is typically
over 30 inches, and thus the stress induced by the bending of the
leaf element 210 to conform to the recess 212 is minor. In a
maximum load-bearing embodiment, flats are introduced in the recess
212 to conform to the flat profile of the leaf lip 211, as
illustrated in FIG. 8B and discussed further below.
[0034] Although the bearing surfaces 311 are illustrated as being
significantly sloped, for ease of illustration, one of ordinary
skill in the art will recognize that the bearing surfaces 311
should be substantially perpendicular to the lines of compression
and expansion forces, the inclination being provided to ease the
release of the leaf lip 211 from the recess 212. In a preferred
embodiment, to provide a substantial bearing surface 311 while
allowing for an ease of release of the leaf lip 211, the slopes of
the bearing surfaces 311 is 15 degrees.
[0035] As is evident from the sequence of FIGS. 3A-3D, the
connection of items via a separation connector 200 in accordance
with this invention is a relatively simple press 300 and tension
321 process. In a typical staged assembly process, as illustrated
for example in FIG. 4, each stage 401 is merely positioned above
the prior stage 402 and lowered until the leaf lips 211 of the leaf
elements 210 of the lower ring 202 are adjacent the recess 212 of
the upper ring 201. The lowering or urging of the stage 401 into
the lower ring 202 has the effect of increasing the perimeter
formed by the leaf lips 211, due to the sloped perimeter 305 of the
upper ring 201. If the filament 320 is placed about the perimeter
before the stages are positioned, sufficient slack is provided to
allow the perimeter of the leaf lips 211 to be expanded. When the
leaf lips 211 are adjacent the recess 212, the perimeter of the
leaf lips 211 is subsequently returned to its original diameter by
a tensioning of the filament 320, typically via a ratchet or other
tension retaining device.
[0036] Illustrated in FIG. 5 is an example tension device 550 and
detension device 570 that are mounted on the lower ring 202. In the
example embodiment of FIG. 5, a free end 320A of the filament 320
is secured to the detension device 570 and, as illustrated by
dashed lines, is routed 320A-320B through the detension device 570.
Alternatively, the filament 320 may be a continuous loop that is
sized to be slightly larger than the largest perimeter formed when
the leaf lips 211 are deformed by the insertion of the upper loop
201, thereby obviating the need to secure it to the detension
device 570. The filament 320 is routed about the perimeter formed
by the leaf lips of leaf elements 210A-210N, where N symbolizes the
total number of leaf elements 210. The filament groove 214 of at
least one of the leaf elements 210A-210N is shaped so as to retain
the filament 320 after it is detensioned. This retention also aids
the routing 320B-320C of the filament 320 about the perimeter. The
filament end 320D is routed through the detension device 570, as
indicated by dashed lines, and secured to the tension device 550.
If the filament 320 is continuous, the portion of the filament 320
that is adjacent the tension device 550 is secured to the tension
device 550. A rotation of the tension wheel 560 in the direction
565 tensions the filament 320 about the perimeter formed by the
leaf lips of leaf elements 210A-210N. In a preferred embodiment,
the tension wheel 560 is ratcheted 562 to retain the tension. In a
preferred embodiment, a 450 pound tension has been calculated to be
sufficient to support an axial load of over 140,000 pounds and
lateral moment over 825,000 inch-pounds using the aforementioned 38
inch diameter configuration of 59 leaf elements 210. In this
configuration, the leaf elements 210 are made of aluminum alloy
(6061-T6), approximately two inches tall, two inches wide, and less
than a quarter inch thick. The leaf lip 211 and recess 212 are also
less than a quarter inch in depth. The upper 201 and lower 202
rings are made of aluminum alloy (7075-T7).
[0037] The release of the connection between the upper 201 and
lower 201 rings is effected by detensioning the filament 320. In a
preferred embodiment, two redundant electric thermal line
de-tensioners 571A, 571B heat the filament 320 to its melting
point, or decomposition point, and redundantly detensions both ends
320A-B, 320C-D within 30 seconds. An example thermal line
detensioner is detailed in U.S. Pat. No. 4,540,873, and is
incorporated by reference herein. Depending upon the filament 320
material composition, the detensioning occurs as a result of
filament 320 stretching or breaking, or both, at or near its
melting or decomposition point. Alternative detensioning means,
common in the art, can be used as well. For example, the tension
wheel 360 may contain a clutch or latch that can be remotely
released. In like manner, the tension device 550 may include an
electric motor, that allows for remote tensioning as well as
detensioning. Because the tension on the filament 320 is
substantially less (about 1/8th) than the conventional V-band
tension, and because the thermal detensioning process is a
relatively slower process, the shock that is introduced by the
de-tensioning of the filament 320 is substantially less than the
shock that is introduced by the de-tensioning of the conventional
V-band. The preferred use of a thermal line de-tensioner also
avoids the shock effects and risk of potential injury typically
associated with explosive de-tensioning means.
[0038] When the filament 320 is detensioned, the leaf elements 210
are urged by the spring element 230 and plunger 231 to the deformed
positions illustrated in FIGS. 3B and 3C. Ancillary devices are
employed in a preferred embodiment to urge the upper ring from the
lower ring. FIG. 6 illustrates an example spring device 680 that
urges the upper ring 201 from the lower ring 202 in a direction
600. In a preferred embodiment, multiple springs 680 are affixed to
the lower ring 202 to provide a uniform upward 600 urging force;
the upper ring 201 is keyed to the lower ring 202, and a button 681
from each spring 680 seats the spring 680 into a corresponding
recess 682 in the upper ring 201. Because the direction 600 is
opposite to the direction 300, the sequence of operations
illustrated in FIGS. 3C-3B-3A is retraced, thereby separating the
upper 201 and lower 202 rings.
[0039] It is important to note that, as illustrated in FIG. 3B, the
plunger 231 urges the leaf element 210 outward 310 such that a gap
375 exists between the farthest extent of the leaf lip 211 and the
inclined surface 305 of the upper ring 201. In this manner, when
the plunger 231 releases the coupling of the leaf elements 210 from
the upper ring 201 by urging the leaf lip 211 from the recess 212,
the leaf elements 210 are not obstructed by the upper ring 201.
When the leaf lip 211 falls away, or is urged away, from the
plunger 231 in a direction opposite direction 300 in FIG. 3A, the
resilient force of the leaf element 310 against the inclined
surface 305 of the upper ring 201 further urges the separation of
the upper ring 201 from the lower ring 202 in the direction
opposite to direction 300, resulting in the decoupled state
illustrated in FIG. 2.
[0040] It is significant to note that upon separation, the primary
components of the separation connector 200 remain intact; only the
filament 320 is affected by the decoupling process. As mentioned
above, in a preferred embodiment, one or more of the filament
grooves 214 are formed so as to retain the filament 320 after it is
detensioned. Because only the filament 320 is affected by the
decoupling process, a separation connector in accordance with this
invention allows for rapid and efficient coupling and decoupling
during prelaunch test and assembly.
[0041] FIGS. 7A-7B illustrate an alternative embodiment of a
separation connector 200'. Items having the same function as in
prior figures are illustrated with the same reference numeral. In
this alternative embodiment, the unbiased and unstressed position
of the leaf element 710 is positioned such that a gap 775 exists
between the leaf lip 211 and the farthest extent of the lower
bearing surface 711 of the upper ring 201 when the leaf element 710
is in an unbiased position, as illustrated in FIG. 7A. As
illustrated in FIG. 7B, the filament 320 in this embodiment is used
to tension and deform the leaf element 710 so as to seat the leaf
lip 211 of the leaf element 710 into the recess 212 of the upper
ring 201. Note the example C-shaped filament groove 214 in FIG. 7B;
the C-shape retains the filament after detensioning, as discussed
above. In this embodiment, when the filament 320 is detensioned,
the resilience of the leaf element 710 forces the leaf element 710
to its unbiased position shown in FIG. 7A, thereby releasing the
upper ring 201 from the lower ring 202. As would be evident to one
of ordinary skill in the art, the use of the resiliency of the leaf
element 710 to urge the leaf lip 211 from the recess 212 obviates
the need for the spring structures 230 of FIG. 2, but the reduced
load bearing capabilities of the deformed and stressed leaf
elements 710 of this embodiment limits its use to a reduced load,
as compared to the substantially unstressed leaf elements 210 of
FIG. 2.
[0042] The foregoing illustrates the principles of the invention.
It will thus be appreciated that those skilled in the art will be
able to devise various arrangements which, although not explicitly
described or shown herein, embody the principles of the invention
and are thus within its spirit and scope. The following alternative
embodiments illustrate such varied arrangements.
[0043] As illustrated in FIG. 8A, the upper ring 201 is circular,
whereas the leaf elements 210 are substantially flat elements
arranged in a circular perimeter. The meeting of the flat surface
811 of the leaf element 210 and curved perimeter 812 of the recess
212 in the upper ring 201 provides contact only where the flat
surface 811 is tangent 815 to the curved perimeter 812. This
configuration introduces a stress on the leaf elements 210 to
conform to the curved perimeter 812. Where maximum load bearing
potential is required, flats 825 as in FIG. 8B are used.
Alternatively (not shown), the leaf lips 211 may be formed as a
curved surface to conform to a curved perimeter 812. In these
embodiments, because the resiliency of the leaf element does not
act to urge the leaf lip 211 out of the recess 212, greater
strength springs 230 are required to urge the leaf lip 211 out of
the recess 212. Each of these alternatives requires a more complex
manufacturing process.
[0044] In a preferred embodiment, as illustrated in FIG. 8C, the
leaf element 810 contains cuts 818 that allow for a lower stress
deformation of the leaf lip 211 to better conform to a curved
perimeter when the filament 320 is circumferentially tensioned, as
illustrated in FIG. 8D. This embodiment allows for the manufacture
of a constant depth recess 212 in the upper ring 201 and a
substantially flat leaf element 810; it also provides for a more
uniform distribution of load within the recess 212. As illustrated
in FIG. 8D, the tensioning of the filament (not shown) introduces a
curvature to the leaf element 810, and the resiliency of the leaf
element 810 will cause the leaf lip 211 to spring back to its
original flat shape when the filament is detensioned, thereby
acting to urge the extremities of the leaf lip 211 out of the
recess 212. It should be noted that, in a preferred embodiment, the
cuts 818 are shallow, and do not extend into upright portion 830 of
the leaf element 810. In this manner, the leaf element 210 retains
its lateral strength and integrity to support high lateral forces.
FIG. 8C illustrates a top and front profile of a preferred
embodiment of a leaf element 810 having relatively small cuts 818,
as used in the aforementioned 59 leaf element, 38 inch diameter
circular configuration. Also shown in FIG. 8C are end sections 816.
In this embodiment, the filament grooves 214 are formed such that
the filament 320 is retained by the "C" shape formed within each of
these end sections 816. An "O" shape may also be used, but would
require a threading of the filament through each "O".
[0045] FIG. 8E illustrates a preferred embodiment of the upper ring
201, wherein elements 860 are spaced around the perimeter of the
ring 201, to react any shear forces that may occur. In this
embodiment, the cuts 818 are configured to allow for these elements
860 as the leaf element 810 is urged into the ring 201. The
elements 860 span the recess that forms the receiving surface for
the leaf lip, and are preferably embodied as pins that are inserted
into milled or drilled holes in the ring 201, to avoid the need to
form the recess of the ring 201 with web elements that span the
recess. The elements 860 and cuts 818 are configured to prevent
translation 865 of the leaf elements 810 with respect to the ring
201 when the leaf lips of the leaf elements 810 are operationally
coupled to the receiving surface of the ring 201.
[0046] Typically, some electronic communication or power
transmission is required between the connected items. FIG. 9
illustrates mating electrical connectors 981 and 982 that are
attached to the upper 201 and lower 202 rings, respectively. As
would be evident to one of ordinary skill in the art, the
connectors 981 and 982 may contain multiple electrical connections,
as required. Note that in accordance with this invention, the
electrical mating of the connectors 981 and 982 is effected by the
same downward force 300 that effects the aforementioned alignment
of leaf lip 211 and recess 212.
[0047] In a preferred embodiment, the arrangement of leaf elements
210 conforms to a structural form of the joined items. In the
aerospace industry, cylindrical shapes are common, and FIG. 2
illustrates a corresponding circular arrangement. In accordance
with the principles of this invention, other arrangements are
possible as well, as illustrated in FIGS. 10A-10F. FIG. 10A
illustrates an example square or rectangular arrangement; FIG. 10B
illustrates an example open arrangement; FIG. 10C illustrates an
example triangular arrangement, and so on. These arrangements will
typically correspond somewhat to the shape of the shape of the
items being joined. For example, the oval arrangement of FIG. 10D
may be employed for connecting a wing of an aircraft to the
fuselage, the oval shape corresponding somewhat to the profile of
an airplane wing. The complex shape of FIG. 10E may be employed for
a twin engine jet, such as used on an F-14 or F-15 aircraft. The
example arrangement of FIG. 10F may be employed for six triangular
shaped satellites that are mounted to a common launch vehicle.
These and other configurations and shapes will be evident to one of
ordinary skill in the art in light of the principles presented
herein. It is important to note that the perimeter formed by the
arrangement of leaf elements 210 should be curved, such that a
tensioning of the filament or band 320 will effect an urging of the
leaf lip 211 of each leaf element 210 into the recess 212 of the
upper ring 201, or, as discussed below, such that an expansion of a
ring or band will urge the leaf lips outward into a surrounding
recess. In the conventional forms of FIG. 2, and FIG. 10A-10D, the
leaf lips 211 face the inside of the perimeter formed by the leaf
element 210. As illustrated by the arrows 321 of FIG. 10A
tensioning of the filament 320 about the perimeter has the effect
of reducing the perimeter, forcing the leaf lips toward the center,
and into the corresponding outward facing recess 212. If the
orientation of the radius of curvature changes, the orientation of
the leaf lips 211 and recess 212 should correspondingly change, as
illustrated by the arrows 321 and 321' of FIG. 10E. That is, as
illustrated in FIG. 10E, the leaf elements 210 are positioned such
that a tensioning of the filament 320 has the effect of moving the
leaf lips 211 in the directions 321 and 321' into corresponding
recesses 212. In an alternative arrangement, some or all of the
leaf lips and mating surface are oriented such that the mating
surface is exterior to the leaf lips, relative to the radius of
curvature forming each segment of the coupling perimeter, and the
filament is in the form of a band that can transmit an outward
force relative to the curvature, so that the leaf lips are forced
outward to the mating surface.
[0048] To facilitate manufacturing and assembly, the leaf elements
of this invention may be individually mounted, or segments of a
plurality of leaf elements, may be provided to facilitate the
creation of larger, and potentially more or less complex
perimeters. In a preferred embodiment, arc segments comprising
multiple leaf elements are provided, allowing circles and other
curved perimeters to be created easily as a plurality of adjacent
segments. The segmentation of large circumference coupling
structures also eases shipping and handling complexities and
costs.
[0049] As would be evident to one of ordinary skill in the art in
light of this disclosure, the load-bearing capacity of the
separation connector may be increased by a variety of common
mechanical design techniques. FIG. 11 illustrates, for example, a
separation connector that contains dual rings of leaf elements
210a, 210b and leaf lips 211a, 211b on the lower ring 202, and
corresponding dual recesses 212a and 212b in the upper ring
201.
[0050] A variety of other configurations and applications will also
be evident in light of this disclosure. For example, the placement
of the protrusion on the leaf lip 211 and the recess 212 in the
upper ring 201 can be reversed, such that a protrusion from the
upper ring 201 is seated into a recess on the leaf lip 211 by the
filament 320. In like manner, multiple protrusions may be placed on
each leaf lip 211, and multiple recesses 212 provided in the upper
ring 201 to receive them. That is, in accordance with this
invention, the upper ring 201 has a receiving surface that contains
an inverse of the mating surface corresponding to the leaf lip 211
of each leaf element 210; preferred load bearing mating surface
shapes are common in the mechanical arts.
[0051] In like manner, alternatives to the spring mechanisms 230 of
FIG. 2, and 680 of FIG. 6 will be evident to one of ordinary skill
in the art. A pre-cocked spring, for example, having a release
mechanism that forces a sudden release of the plunger 231 may be
preferred to provide an impact force on the leaf element 210 to
overcome any binding that may occur between the leaf lip 211 and
recess 212. The use of a pre-cocked spring also allows the seating
of the leaf lip 211 into the recess 212 via the resilience of the
leaf element 210, thereby eliminating the need for a tension
filament 320 and its ancillary components in light load
applications. An electromagnetic solenoid or hydraulic device may
be used in lieu of the spring mechanisms 230 and/or 680 to provide
an impact or continuous separation force via a piston. In like
manner, although an embodiment without explosives is typically
preferred, an impact force may be imparted by an explosive
percussion device. Other urging means, such as leaf springs and the
like, are also common in the art.
[0052] Note that although the leaf element 210 has been presented
thus far as a single integral structure, alternative structures are
feasible, including a multiple component leaf element. FIG. 12
illustrates, for example, a leaf element 910 having a leaf 915 and
a base 917 connected by a hinge 916. This embodiment allows for the
coupling and decoupling of two devices without inducing a
deformation of the leaf element 910. This embodiment is
particularly well suited for structures that are frequently coupled
and decoupled, either during normal operation, or during
operational tests.
[0053] FIGS. 13A and 13B illustrate a preferred alternative
embodiment, wherein the leaf elements, such as elements 910, form
an internal perimeter, and the mating surface 930 forms an outer
perimeter. An expansion ring, or band, 920 is configured to exert
an outward force, indicated by arrows 901 in FIGS. 13A and 13B, to
urge the leaf elements outward, toward the mating surface 930. An
expansion device 950 is configured to facilitate the expansion of
the band 920 to couple the leaf elements 910 to the mating surface
930, and the release of the expansion of the band 920 to decouple
the elements 910 and surface 930. Note that the expansion of the
perimeter formed by the band 920 is effected by exerting a force
that compresses the band 920 along the ring perimeter, and thus
terms expansion and compression are used to describe the operation,
depending upon whether the term applies to the dimension of the
perimeter or the stresses within the material that forms the band
920. If the leaf elements include a retainer for the band 920, the
extraction of the leaf elements 910 from the mating surface 930 can
be effected by reducing the perimeter of the band 920, thereby
pulling the leaf elements inward, potentially obviating the need
for decoupling devices, such as the spring and plunger arrangement
230 of FIG. 2.
[0054] Preferably, the band 920 comprises an aluminum tube or rod
approximately {fraction (3/16)} inch in diameter, formed into a
perimeter, and including at least one location where it could be
circumferentially expanded by the expansion device 950, causing the
diameter of the perimeter to increase, thereby urging the leaf
elements into the groove, or grooves, of the mating surface.
Alternative materials may also be used. Preferably, the material of
the band 920 should exhibit a low creep rate, to minimize the
loosening over time caused by the contraction of the material under
continuous load.
[0055] The expansion device 950 may include any of a variety of
devices that are commonly used to expand a ring. The device 950 is
generally configured to urge the ends of a split ring apart,
thereby increasing the perimeter of the ring, and may include, for
example, a levered latch, a turnbuckle arrangement, a piston, and
so on. Correspondingly, the device 950 is also configured to reduce
the diameter of the ring, back to its unexpanded perimeter.
[0056] Although the expanding ring embodiment of FIGS. 13A and 13B
is a more complex embodiment, it does provides some advantage over
the tensioned arrangement discussed in the previous figures,
particularly with regard to re-use. As discussed above, the
simplest means for detensioning the band in a tensioned embodiment
is to sever the band; the reuse of the tensioned coupling,
therefore, will typically require a replacement of the tensioned
band. Conversely, the expansion band 920 will generally be attached
to the expansion device 950, and will be de-expanded via a
non-destructive inversion of the expansion process (i.e. a release
of a latch, an opposite turning of a turnbuckle, a release of a
piston, and so on), thereby facilitating its re-use. Additionally,
because the band 920 is in compression when under load, the
likelihood of crack growth and failure is substantially less than
that of a tensioned band.
[0057] Although the separation connector 200 of this invention is
particularly well suited for items that are expected to be
uncoupled at some time, the ease of assembly of the separation
connector 200 also warrants its use for applications that merely
require a reliable and easy to assemble connection, such as
assembling a pipeline. In these applications, for example, the
requirements for the detensioning or de-expansion mechanism, if
any, is minimal.
[0058] These and other configurations and structures will be
evident to one of ordinary skill in the mechanical arts, and are
included within the intended scope of the following claims.
* * * * *