U.S. patent application number 10/065243 was filed with the patent office on 2004-04-01 for crush tube assembly.
This patent application is currently assigned to FORD GLOBAL TECHNOLOGIES, INC.. Invention is credited to Sellepack, Joseph Daniel, Wu, Chi-Chin.
Application Number | 20040060790 10/065243 |
Document ID | / |
Family ID | 32028507 |
Filed Date | 2004-04-01 |
United States Patent
Application |
20040060790 |
Kind Code |
A1 |
Wu, Chi-Chin ; et
al. |
April 1, 2004 |
CRUSH TUBE ASSEMBLY
Abstract
A crush tube assembly for absorbing impact energy is provided. A
first tube substantially free from convolutions is disposed about a
second tube substantially free from convolutions. A third tube
having convolutions is also disposed within the first tube, and may
be interposed between the first and second tubes. The convolutions
support the axial integrity, and minimize lateral bucking of the
first and second tubes during the absorption of impact energy.
Additional alternating layers of smooth and convoluted tubes may be
alternatively disposed within the assembly to provide further
strength and control for absorbing energy. A method for absorbing
impact energy is also provided. The method includes the steps of
providing a first tube substantially free from convolutions,
disposing within said first tube a second tube substantially free
from convolutions, interposing between said first and second tubes
a third tube having convolutions; and impacting said first, second,
and third tubes.
Inventors: |
Wu, Chi-Chin; (West
Bloomfield, MI) ; Sellepack, Joseph Daniel; (Taylor,
MI) |
Correspondence
Address: |
DYKEMA GOSSETT PLLC
39577 WOODWARD AVENUE
SUITE 300
BLOOMFIELD HILLS
MI
48304
US
|
Assignee: |
FORD GLOBAL TECHNOLOGIES,
INC.
DEARBORN
MI
|
Family ID: |
32028507 |
Appl. No.: |
10/065243 |
Filed: |
September 27, 2002 |
Current U.S.
Class: |
188/377 |
Current CPC
Class: |
F16F 7/123 20130101 |
Class at
Publication: |
188/377 |
International
Class: |
F16F 007/12 |
Claims
1. A crush tube assembly, comprising: a first crush tube; a second
crush tube disposed within said first crush tube; a third crush
tube disposed within said first crush tube, said third crush tube
having convolutions.
2. The crush tube assembly of claim 1 wherein said convolutions are
substantially disposed about an end segment of said third tube.
3. The crush tube assembly of claim 1, wherein said third tube is
interposed between said first tube and said second tube.
4. The crush tube assembly of claim 3, wherein said first and
second tubes are substantially free from convolutions.
5. The crush tube assembly of claim 3, wherein said convolutions
are substantially disposed about the periphery of said third
tube.
6. The crush tube assembly of claim 3, wherein said convolutions
support the inner periphery of said first tube and wherein said
convolutions support the outer periphery of said second tube.
7. The crush tube assembly of claim 3, wherein said convolutions
are sinusoidal in shape.
8. The crush tube assembly of claim 3 wherein said convolutions are
gear-tooth waved in shape.
9. The crush tube assembly of claim 3 wherein said convolutions are
screw shaped.
10. The crush tube assembly of claim 3, wherein said first, second,
and third tubes are substantially cylindrical.
11. The crush tube assembly of claim 3, wherein said first, second,
and third tubes are substantially rectangular.
12. A crush tube assembly, comprising: a plurality of tubes each
disposed about a longitudinal axis, said plurality of tubes
comprising: a first tube substantially free from convolutions; a
second tube substantially free from convolutions and disposed
within said first tube; a third tube disposed within said second
tube, said third tube having a body and an end segment, said body
substantially free from convolutions and said end segment having
convolutions.
13. The crush tube assembly of claim 12, further comprising a
fourth tube interposed between said first tube and said second
tube, said fourth tube having convolutions, and a fifth tube
interposed between said second tube and said third tube, said fifth
tube having convolutions.
14. The crush tube assembly of claim 13, wherein said convolutions
of said fourth tube and of said fifth tube are screw shaped.
15. The crush tube assembly of claim 13, wherein said convolutions
of said fourth tube support the inner periphery of said first tube
and the outer periphery of said second tube; and wherein said
convolutions of said fifth tube support the inner periphery of said
second tube and the outer periphery of said third tube.
16. The crush tube assembly of claim 13, wherein said convolutions
of said fourth tube and said convolutions of said fifth tube are
sinusoidal in shape.
17. The crush tube assembly of claim 13 wherein said convolutions
of said fourth tube and said convolutions of said fifth tube
convolutions are gear-tooth waved in shape.
18. The crush tube assembly of claim 13 wherein said convolutions
of said fourth tube and said convolutions of said fifth tube
convolutions are screw shaped.
19. The crush tube assembly of claim 13, wherein said plurality of
tubes are substantially cylindrical.
20. The crush tube assembly of claim 13, wherein said plurality of
tubes are substantially rectangular.
21. A method of absorbing crash energy, comprising: providing a
first tube substantially free from convolutions; disposing within
said first tube a second tube substantially free from convolutions;
interposing between said first and second tubes a third tube having
convolutions; and impacting said first, second, and third
tubes.
22. The method of claim 21, wherein the step of impacting further
comprises impacting said first, second and third tubes
substantially along a longitudinal axis of said first, second and
third tubes.
23. The method of claim 22, further comprising the step of
laterally supporting said first tube and said second tube with said
convolutions.
Description
BACKGROUND OF THE INVENTION
[0001] 1. Field of the Invention
[0002] This invention relates to an impact energy absorption
system, and in particular to a crushable tubular assembly for
efficient and controllable energy absorption.
[0003] 2. Background of the Invention
[0004] In current vehicle structures, and particularly in front-end
structures, it has become increasingly difficult to obtain package
space for components that absorb impact energy created during a
vehicle crash. Conventional designs for absorbing high-energy
impacts, such as that described in U.S. Pat. No. 3,831,997 to
Myers, typically include tubular structures that are made from high
strength materials like various high strength steels. These tubular
structures may be designed as vehicle rails, or may be separately
positioned in a fore/aft direction of the vehicle to absorb the
energy of a fore/aft collision. However, such designs have a
tendency to buckle laterally if the load is offset, that is, if the
load is not concentric with the tube.
[0005] Moreover, because of the limited package spaces available,
with limited frame selection allowed, improving the axial strength
of such structures tends to increase the degree of lateral
instability of the tubes.
[0006] Other conventional designs include tubular assemblies that
have structures for initiating deformations in the assembly, such
as described in U.S. Pat. No. 5,914,163 to Browne. These features
include slits or other structures to initiate longitudinal
splitting, tearing, or peeling of the tubular assembly. While
providing such structures may assist in controlling the energy
absorbed in an impact, the overall axial strength of such tubular
structures may be compromised.
[0007] Still other systems for absorbing frontal impact energy
include entire redesigns of an automotive vehicle body structure,
such as, for example, the vehicle body structure described in U.S.
Pat. No. 6,312,038 to Kawamura, et al. Such designs may include
extensions of the vehicle body/frame in the fore/aft direction in
order to accommodate one or more energy absorbing members. Such
redesigns, however, are expensive to develop and are not compatible
with automobiles in present production.
[0008] In particular, presently produced automobiles may not have
the necessary package space available for housing an increased
number of absorbing members, or tubes.
[0009] There is thus a need for an impact energy absorption system
that will minimize or eliminate one or more of the above-mentioned
deficiencies.
SUMMARY OF THE INVENTION
[0010] The present invention provides an improved impact energy
absorption system, and a method for absorbing impact energy.
[0011] An impact energy absorption system in accordance with the
present invention comprises an assembly of crush tubes. The crush
tube assembly includes a first tube disposed about a second tube. A
third tube having convolutions is also disposed within the first
tube, and may be interposed between the first and second tubes. The
third tube may alternatively be disposed within the second tube.
The convolutions of the third tube support the axial integrity, and
minimize lateral bucking of the first and second tubes during the
absorption of impact energy. Additional alternating layers of
smooth and convoluted tubes may be alternatively disposed within
the assembly to provide further strength and control for absorbing
energy.
[0012] A method for absorbing impact energy is also provided. The
method includes the steps of providing a first tube substantially
free from convolutions, disposing within said first tube a second
tube substantially free from convolutions, interposing between said
first and second tubes a third tube having convolutions; and
impacting said first, second, and third tubes.
[0013] An impact energy absorption system in accordance with the
present invention has several advantages as compared to
conventional systems. The inventive device provides the axial
strength of a conventional smooth, or unconvoluted tube and the
energy absorption control of a convoluted tube. The inventive
device, therefore, can absorb high-energy impacts that may be
offset, while reducing the tendency to buckle laterally.
Additionally, the inventive device maximizes the use of available
package space by disposing each crush tube about one another.
Accordingly, the present invention is able to absorb broad ranges
of crush energy and maintain its lateral stability during a
crash.
[0014] These and other features and objects of this invention will
become apparent to one skilled in the art from the following
detailed description and the accompanying drawings illustrating the
features of this invention by way of example.
BRIEF DESCRIPTION OF DRAWINGS
[0015] FIG. 1 is an exploded cross-sectional perspective view of a
crush tube assembly in accordance with one embodiment of the
present invention.
[0016] FIG. 2 is a side view of the components of the crush tube
assembly of FIG. 1.
[0017] FIG. 3 is a cross-sectional view of the crush tube assembly
of FIG. 1.
[0018] FIG. 4 is a magnified view of section 4 of the crush tube
assembly of FIG. 3.
[0019] FIG. 5 is a side view of alternative convoluted tubes for
the crush tube assembly of FIG. 1.
[0020] FIG. 6 is an exploded cross-sectional perspective view of a
crush tube assembly in accordance with another embodiment of the
present invention.
[0021] FIG. 7 is a perspective view of the components of the crush
tube assembly of FIG. 6.
[0022] FIG. 8 is a partial cross-sectional side view of the crush
tube assembly shown in FIG. 1.
[0023] FIG. 9 is a magnified view of section 9 of the crush tube
assembly shown in FIG. 8.
[0024] FIG. 10 is a deformation profile of a conventional smooth
crush tube.
[0025] FIG. 11 is a deformation profile of a crush tube assembly in
accordance with one embodiment of the present invention.
[0026] FIG. 12 is a partial cross-sectional perspective view of a
deformed crush tube assembly in accordance with the embodiment of
the present invention shown in FIG. 1.
[0027] FIG. 13 is a perspective view of each tube, contained within
the deformed crush tube assembly shown in FIG. 12.
DETAILED DESCRIPTION
[0028] Referring now to the drawings wherein like reference
numerals are used to identify identical components in the various
views, FIGS. 1, 2, and 3 illustrate a crush tube assembly 10 in
accordance with one embodiment of the present invention. Assembly
10 is provided to absorb impact energy sustained during an
automobile collision.
[0029] Assembly 10 is configured for use in a front-end structure
of a vehicle, such as vehicle frame rails. It should be understood,
however, that assembly 10 might find use in a variety of locations
of and components for a vehicle structure. Assembly 10 includes a
plurality of alternating smooth and convoluted crush tubes of a
general cylindrical shape. It will be appreciated by those skilled
in the art that other shapes may also be suitable. As discussed in
greater detail below, assembly 10 may include an outer tube 12, an
inner tube 14, a core tube 16, a first convoluted tube 18, a second
convoluted tube 20, and a seal cap 22.
[0030] Tube 12 provides a rigid outer support structure for
assembly 10. Tube 12 may be generally "flat" or "smooth," which, as
used herein, means substantially free from convolutions. Tube 12
may be constructed from various grades of mild steel, high strength
steel or ultrahigh strength steel, such as dual phases steels or
TRIP steels. It may further be constructed from composite materials
such as Sheet Molded Composites (SMC) or Glass Reinforced Polyester
Composites. It should be understood, however, that material
composition and method of manufacture of tube 12, as well as any
other tube of this invention, might be varied without departing
from the spirit of the present invention. Tube 12 may be disposed
about a longitudinal axis 24. Tube 12 may further have a neck, or
turtleneck, 26 at one end. Neck 26 may be provided to initially
receive the impact energy from a force directed along, or
substantially along, axis 24. Upon impact, neck 26 collapses, or
otherwise axially directs the impact energy through assembly 10.
The remaining portion of tube 12 provides axial strength to
assembly 10 for absorbing impact energy and provides a structure in
which other tubes may be disposed.
[0031] Tube 14 is disposed within tube 12. Tube 14 may be disposed
about a longitudinal axis which is common to axis 24 of tube 12. In
the embodiment shown in FIGS. 1, 2, and 3 tube 14 is concentrically
disposed within tube 12. However, it will be recognized by those
skilled in the art that the longitudinal axes of tube 12 and tube
14 need not be concentric. As shown, tube 14 is generally smooth.
Tube 14 is provided to reinforce the axial strength of assembly 10
for absorbing impact energy.
[0032] Tube 14 may be constructed from the same materials as tube
12. Tube 14 may be shorter than tube 12. As shown in FIG. 4, tube
14 may further have a collar 28 extending radially outward at one
end. Collar 28 provided to abut seal cap 22 and transmit an axial
load to seal cap 22.
[0033] Tube 16 is disposed within tube 14. Tube 16 may be disposed
about a longitudinal axis which is common to axis 24 of tube 12. In
the embodiment illustrated in FIGS. 1, 2, and 3 tube 16 is
concentric with tube 12 and tube 14. Tube 16 may be constructed
from the same materials as tube 12 and tube 14. Tube 16 may be
approximately same length as tube 12. Tube 16 may have a generally
smooth body. Tube 16 may further have an end segment 30 that has
convolutions 31. End 30 may be the approximate difference between
the lengths of tube 12 and tube 14, and extends axially distal from
collar 28. The convolutions 31of end 30 may project radially
outward to the inner periphery of seal cap 22. Convolutions 31 may
be formed similar to the convolutions of tube 18 and tube 20,
discussed below. Convolutions 31 are provided to allow tube 16 to
axially deform to reduce the tendency to buckle laterally.
[0034] Tube 18 is interposed between tube 12 and tube 14. Tube 18
may be constructed from the same materials as tube 12. Tube 18 may
be disposed about a longitudinal axis. In the embodiment shown in
FIGS. 1, 2, and 3, tube 18 is concentric with tubes 12, 14, and 16.
Tube 18 may be shorter than tube 12, and substantially the same
length as tube 14. Tube 18 may have convolutions 32, a smooth
extended end 34, and a collar 36.
[0035] Convolutions 32 are substantially disposed about the
periphery of tube 18. In the embodiment illustrated in FIGS. 1, 2,
and 3, convolutions 32 are entirely disposed about the body of tube
18. As illustrated in FIGS. 1 and 2, convolutions 32 generally
project radially outward from tube 18. However, it will be
appreciated by those skilled in the art that convolutions 32 may
also project radially inward, or project both radially outward and
inward from tube 18. Convolutions 32 are provided to control the
energy absorption from an impact to assembly 10. Upon impact to
assembly 10, convolutions 32 compress axially and provide lateral
stability to assembly 10 by minimizing, or preventing, buckling.
Convolutions 32 may be shaped in sinusoidal waveform or gear tooth
wave, however it will be appreciated by those skilled in the art
that other shapes will be suitable. Convolutions 32 may be formed
by molding, cutting, hydro-forming, or any other conventional
industrial manufacturing method.
[0036] As discussed in greater detail below and as specifically
shown in FIGS. 8 and 9, convolutions 32 project outward to the
inner periphery of tube 12. Inward convolutions would similarly
project to the outer periphery of tube 14.
[0037] Smooth end 34 extends from the convoluted body of tube 18
and is disposed within neck 26 of tube 12. Smooth end 34 provide
additional rigid support within neck 26. Collar 36 projects
radially outward from the other end of tube 18. As shown in FIG. 4,
Collar 36 abuts collar 28 for transmitting an axial load toward
seal cap 22.
[0038] Tube 20 may be interposed between tube 14 and tube 16. Tube
20 may be constructed from the same materials as tube 12. Tube 20
may be disposed about a longitudinal axis. In the embodiment shown
in FIGS. 1, 2, and 3, tube 20 is concentric with tubes 12, 14, 16,
and 18. Tube 20 may be shorter than tube 12, and substantially the
same length as tubes 14 and 16. Tube 20 may have convolutions 38, a
smooth extended end 40, and a collar 42.
[0039] Convolutions 38 are substantially disposed about the
periphery of tube 20. In the embodiment illustrated in FIGS. 1, 2,
and 3, convolutions 38 are entirely disposed about the body of tube
20. As illustrated in FIG. 1 and 2, convolutions 38 generally
project radially inward from tube 20. However, it will be
appreciated by those skilled in the art that convolutions 38 may
also project radially outward, or project both radially outward and
inward from tube 20. Convolutions 38 are provided to control the
energy absorption from an impact to assembly 10. Upon impact to
assembly 10 convolutions 38 compress axially and provide lateral
stability to assembly 10 by minimizing, or preventing, buckling.
Convolutions 38 may be formed by the same methods as convolutions
32. As discussed in greater detail below and specifically shown in
FIGS. 8 and 9, convolutions 38 project inward to the outer
periphery of tube 16. Outward convolutions would similarly project
to the inner periphery of tube 14.
[0040] Smooth end 40 extends from the convoluted body of tube 20
and is disposed within neck 26 of tube 12. Smooth end 40 provides
additional rigid support within neck 26. Collar 42 projects
radially inward from the other end of tube 20. As shown in FIG. 4,
Collar 42 abuts for transmitting an axial load toward seal cap
22.
[0041] Seal cap 22 is provided for additional axial support of
tubes 14, 16, 18, and 20. Seal cap 22 is disposed within tube 12
and about convoluted end 30 of tube 16. Seal cap 22 may have a
collar 44 projecting radially outward. As-shown in FIG. 4, collar
44 is axially adjacent to and supports axial loads transmitted from
collars 28, 36, and 42. Seal cap 22 may be made out of the same
material as tube 12.
[0042] FIGS. 1 and 2 further illustrate the construction of crush
tube assembly 10. Smooth tube 12 is provided. Smooth tube 14 is
disposed within smooth tube 12, and smooth tube 16 is disposed
within smooth tube 14. Convoluted tube 18 is interposed between
tube 12 and tube 14. Convoluted tube 20 is interposed between tube
14 and tube 16. Upon the disposition of tubes within tube 12, seal
cap 22 may be disposed within tube 12 and about end 30 of tube 16.
The assembly 10 may then be sealed at the neck end 20 and at the
seal cap 22 end.
[0043] While FIGS. 1, 2, and 3 depicts assembly 10 as including
outer tube 12, inner tube 14, core tube 16, first convoluted tube
18, second convoluted tube 20, and seal cap 22, it will be
appreciated by those skilled in the art that the inventive assembly
may include greater or fewer convoluted tubes. For example,
depending on the size of tube 12, additional alternating layers of
smooth and convoluted crush tubes may be alternatively disposed
within assembly 10 to provide further strength and control for
absorbing impact energy. Similarly, assembly 10 may include fewer
tubes than depicted. For example, assembly 10 may include outer
tube 12-, inner tube 14 disposed within tube 12, and core tube 16,
disposed within tube 14, having convolutions 31 at end 30.
Alternatively, assembly 10 may include outer tube 12, tube 14
disposed within tube 12, and convoluted tube 18 interposed between
tube 12 and tube 14.
[0044] FIG. 5 depicts alternative convoluted crush tubes 19, 21,
which can replace convoluted tubes 18, 20, respectively, in
assembly 10. Convoluted crush tubes 19, 21 are substantially the
same as convoluted tubes 18, 20, respectively, except that the form
of convolutions 32, 38 are replaced with screw formed convolutions
33, 39, respectively. Convolutions 33 may be in clockwise screw
form, while convolutions 39 may be in counter-clockwise screw form.
It will be appreciated by those skilled in the art that the
directions of such convolutions may be reversed. The interlacing
screw form of convolutions 33 and convolutions 39 provides a strong
support to each other and complement the torsional deformation in
tube 19 and tube 21, which in turn provides a substantial stability
for the entire assembly 10. Additionally, screw form convolutions
33, 39 may be more economic to manufacture than other shapes.
[0045] FIGS. 6 and 7 illustrate an alternative crush tube assembly
48 according to the present invention. Crush tube assembly 48 is
similar to assembly 10, but is generally rectangular in
cross-sectional shape. Assembly 48 includes a plurality of
alternating smooth and convoluted crush tubes. Assembly 48 may
include an outer tube 50, an inner tube 52, a core tube 54, a first
convoluted tube 56, a second tube convoluted tube 58, and a seal
cap 60. Tube 50 and tube 52 may be similar to tube 12 and tube 14,
respectively, as tube 50 and tube 52 may generally be smooth.
Further, like tube 12, tube 50 includes neck 62 at one of its ends.
Tube 52 may have a collar 64 projecting outward from the end distal
to neck 62. Tube 54 may be similar to tube 16 as it may have an end
66 with convolutions 68. Convoluted tube 56 may be interposed
between tube 50 and tube 52, and convoluted tube 58 may be
interposed between tube 52 and tube 54. Like tube 18, tube 56 may
have outward projecting convolutions 57, and like tube 20, tube 58
may have inward projecting convolutions 59. Those skilled in the
art, however, will similarly recognize that convolutions 57 and
convolutions 59 may be outwardly projecting, inwardly projecting,
or both outwardly and inwardly projecting from their respective
tubes. Tube 56 may have a smooth extended end 70 disposed within
neck 62 and an outwardly projecting collar 72 disposed about its
other end. Similarly, tube 58 may have a smooth extended end 74
disposed within neck 62 and an inwardly projecting collar 76
disposed about its other end. The smooth ends 70, 74 and collars
72, 76 serve similar functions as smooth ends 34, 40 and collars
36, 42, respectively. Depending on the size of tube SO, additional
layers of alternating smooth and convoluted crush tubes may be
alternatively disposed within assembly 48 to provide further
strength and control for absorbing impact energy. Seal cap 60 is
similar to seal cap 22 and has a collar 78 projecting from its end
proximate to collars 64, 72, and 76. Seal cap 60 axially supports
loads transmitted from tube 52, tube 54, tube 56, and tube 58.
[0046] FIG. 8 illustrates a partial side sectional view of assembly
10 and depicts, from outer most to inner most, outer smooth tube
12, convoluted tube 18, smooth tube 14, convoluted tube 20, and
smooth tube 16. FIG. 9 depicts a magnified view of portion 9 in
FIG. 8. FIG. 9 further shows the development of membrane forces
during axial loading. During an impact, axial force 80 is loaded on
assembly 10. Axial force 80 causes a variety of compressive forces
throughout assembly 10. In particular, axial force 80 results in
longitudinal compressive forces 82, 84, and 86 on smooth tubes 12,
14, and 16, respectively and compressive forces 88 and 90 on
convolutions 32, 38 respectively. Compression force 88 transfers to
convolutions 32 of tube 18, and results in compressive forces 92
along convolutions 32 and normal contact forces 96 on the smooth
tubes 12 and 14. Similarly, compression force 90 transfers to
convolutions 38 of tube 20, and results in compressive forces 94
along convolutions 38 and normal contact forces 96 on the smooth
tubes 14 and 16. Compressive forces 92 and 94 act to compress, or
collapse, the convolutions of tubes 18 and 20, respectively. As
convolutions 32 and 38 are being compressed, the convolutions
provide lateral forces 96 to support the smooth tubes of assembly
10. For example, convolutions 32 support the inner periphery of
tube 12 and the outer periphery of tube 14, and convolutions 38
support the inner periphery of tube 14 and the outer periphery of
tube 16. Lateral forces 96 stabilize and reduce the buckling
tendency of smooth tubes 12, 14, and 16 during axial loading. Such
stabilization improves the ability of assembly 10 to absorb axial
loaded impact energy. The angle of convolutions 32 and convolutions
38 may be adjusted to vary the energy absorption and stabilization
capacity of tubes 12, 14, and 16. The energy absorption and
stabilization capacity are inversely related to each other. For
example, as the angle of convolution is increased, that is, as the
convoluted tube approaches a smooth tube, the energy absorbing
capacity of the convoluted tube increases, but the amount of
lateral forces 96 the convolution provides decreases. Those skilled
in the art will recognize that the angle of convolution may be
optimized based on the application of the invention.
[0047] Computer simulated deformation profiles for a single smooth
crush tube 98 and crush tube assembly 10" are shown in FIGS. 10 and
11, respectively. FIG. 10 illustrates a section view of a
conventional smooth tube 98 after a simulated axially loading of a
high-speed impact at end 100. After a high-speed impact at end 100,
energy is only absorbed by the relatively small area of deformation
102. If the same space, material and weight of material are
available, smooth tube 98 will result in less dissipated energy
because, after impact, less material resulted in plastic
(non-linear) deformation state as compared with the inventive
assembly 10". The structure of tube 98 may produce higher impact
force and intrusion to the backup structure where occupants of the
vehicle may be seated. Conversely, a reduction of the gauge of
smooth tube 98, so as to reduce the impact and intrusion to the
backup structure, results in an increased tendency for tube 98 to
buckle laterally.
[0048] In contrast, FIG. 11 depicts crush tube assembly 10"
following a similar impact to crush tube assembly 10. Assembly 10"
includes the same structure of assembly 10 and its features are
identified by the same reference number with a prime"" "to indicate
that such features have sustained an impact. Neck area 26" receives
the axial load. The convolutions of tubes 18" and 20" compress and
provide lateral support to the peripheries of smooth tubes 12", 14"
and 16". Accordingly, smooth tubes 12", 14", and 16" did not buckle
and instead absorbed the axial impact energy while supported
laterally by the convolutions so as to minimize the tendency to
buckle.
[0049] FIGS. 12 and 13 illustrate perspective views of assembly
10", and of each deformed tube. Neck area 26" has absorbed
significant impact energy, as it is shown to be significantly
deformed in the axial direction. That is, neck area 26" axially
collapses, or telescopes, toward the seal cap end of assembly 10".
Convolutions of tubes 18" and 20" have compressed in the axial
direction and provide lateral support to tubes 12", 14", and 16".
Additionally, convolutions 31of end 30 of tube 16" have also
compressed axially to further prevent tube 16 from buckling. Smooth
tubes 12", 14", and 16" did not buckle and instead absorbed the
axial load as indicated by deformation areas 104, 106, and 108,
respectively.
[0050] FIGS. 1, 11, 12, and 13 further depict a method of absorbing
crash energy. Smooth tube 12 is provided. Smooth tube 14 is
disposed within tube 12. Smooth tube 16 is disposed within tube 14,
and may include an end 30 with convolutions 31. Convoluted tube 18
is interposed between tube 12 and tube 14, and convoluted tube 20
is interposed between tube 14 and tube 16. The assembly of tubes is
then axially impacted. During impact, the convolutions of tube 18
and tube 20 laterally support smooth tubes 12, 14 and 16.
[0051] Through various combinations of smooth and convoluted tubes,
and through various arrangements of convolutions, the present
invention accommodates broad ranges of crush energy absorption. The
present invention further maintains lateral stability and constant
axial compression force during upon impact. Additionally, the
invention efficiently employs package space through the use of
nested, or telescoping tubes. While the invention has been
particularly shown and described with reference to the preferred
embodiments thereof, it will be appreciated by those skilled in the
art that various changes and modifications can be made in the
invention without departing from the spirit and scope of the
invention.
* * * * *