U.S. patent application number 13/974322 was filed with the patent office on 2015-02-26 for closure system for containers.
This patent application is currently assigned to Becklin Holdings, Inc.. The applicant listed for this patent is Becklin Holdings, Inc.. Invention is credited to Dennis S. Becklin, Adrian P. Tayne, Dean Weathers.
Application Number | 20150053683 13/974322 |
Document ID | / |
Family ID | 52479444 |
Filed Date | 2015-02-26 |
United States Patent
Application |
20150053683 |
Kind Code |
A1 |
Becklin; Dennis S. ; et
al. |
February 26, 2015 |
CLOSURE SYSTEM FOR CONTAINERS
Abstract
A closure assembly for sealing a container lid and base is
disclosed. The closure assembly includes a male member and a female
member that are coupled to a container lid and base, respectively.
The female member includes an alignment feature and a gasket
channel with a gasket in the gasket channel. The male member
includes a corresponding alignment feature and a gasket sealing
feature that protrudes into the gasket channel and forms a seal
with the gasket when the closure assembly is in a closed
position.
Inventors: |
Becklin; Dennis S.; (Grants
Pass, OR) ; Weathers; Dean; (Medford, OR) ;
Tayne; Adrian P.; (Grants Pass, OR) |
|
Applicant: |
Name |
City |
State |
Country |
Type |
Becklin Holdings, Inc. |
Reno |
NV |
US |
|
|
Assignee: |
Becklin Holdings, Inc.
Reno
NV
|
Family ID: |
52479444 |
Appl. No.: |
13/974322 |
Filed: |
August 23, 2013 |
Current U.S.
Class: |
220/324 ;
220/345.3; 220/345.6 |
Current CPC
Class: |
B65D 45/24 20130101;
F41C 33/06 20130101; F42B 39/22 20130101 |
Class at
Publication: |
220/324 ;
220/345.6; 220/345.3 |
International
Class: |
B65D 43/02 20060101
B65D043/02; B65D 53/02 20060101 B65D053/02; B65D 45/02 20060101
B65D045/02 |
Claims
1. A closure assembly for a container having a first wall and a
second wall that come together to close the container, the closure
assembly comprising: a female member comprising-- a main body
including a first compression stop interface; a channel formed in
the main body configured to receive the first wall of the container
to secure the female member to the first wall of the container; a
female alignment feature formed in the first compression stop
interface; and a gasket channel in the first compression stop
interface, wherein the gasket channel contains a gasket; a male
member comprising-- a main body including a second compression stop
interface; a channel formed in the main body configured to receive
the second wall of the container to secure the male member to the
second wall of the container; a male alignment feature protruding
from the second compression stop interface and extending into the
female alignment feature; and a male gasket sealing feature
protruding from the second compression stop interface and into the
gasket channel, wherein the male gasket sealing feature forms a
seal with the gasket; a latch coupling the male member to the
female member, the latch having an outer extent; and a bumper
extending beyond the outer extent of the latch.
2. The closure assembly of claim 1, wherein the male alignment
feature protrudes outwardly from the second compression stop
interface a greater extent than the male gasket sealing
feature.
3. The closure assembly of claim 1, wherein female member and male
member are formed according to one of an extrusion process and a
pultrusion process.
4. The closure assembly of claim 1, where in the channels of the
male and female members define a plurality of at least one of
grooves and ridges.
5. The closure assembly of claim 1, wherein the first and second
compression stop interface are at least three times a thickness of
the first and second walls.
6. The closure assembly of claim 1, wherein the male and female
include a plurality of apertures disposed along the channel for
receiving fasteners.
7. The closure assembly of claim 1, wherein the main body of the
male member defines a cutout for receiving the latch.
8. The closure assembly of claim 1, wherein the gasket channel
defines a flared seating surface defining an opening and a gasket
chamber connected to the opening, the gasket being positioned
within the gasket chamber and the opening being smaller than a
width of the chamber, and the male gasket sealing feature being
tapered to conform to the flared seating surface.
9. The closure assembly of claim 1, wherein: the male member
further comprises corner protrusions positioned inwardly from the
male alignment feature and the male gasket sealing feature and
protruding outwardly from the second compression stop interface a
greater extent than the male alignment feature and male gasket
sealing feature, the corner protrusions defining first engagement
surfaces; the female member further comprises corner receivers
positioned inwardly from the female alignment feature and the
gasket channel and extending from the first compression stop
interface in a same direction as the female alignment feature, the
corner receivers defining second engagement surfaces configured to
mate with the first engagement surfaces.
10. The closure assembly of claim 1, wherein the male alignment
feature defines a taper angle and the female alignment feature
defines a flare angle, the flare angle being greater than the taper
angle.
11. A container comprising: a first container shell defining a
first rim; a second container shell defining a second rim; a female
member comprising a main body including a first compression stop
interface; a channel formed in the main body having the first rim
secured therein; a female alignment feature formed in the first
compression stop interface; and a gasket channel in the first
compression stop interface, wherein the gasket channel contains a
gasket; a male member comprising a main body including a second
compression stop interface; a channel formed in the main body
having the second rim secured therein; a male alignment feature
protruding from the second compression stop interface and extending
into the female alignment feature; and a male gasket sealing
feature protruding from the second compression stop interface and
into the gasket channel, wherein the male gasket sealing feature
forms a seal with the gasket; a latch coupling the male member to
the female member, the latch having an outer extent; and a bumper
extending beyond the outer extent of the latch.
12. The container of claim 11, wherein the male alignment feature
protrudes outwardly from the second compression stop interface a
greater extent than the male gasket sealing feature.
13. The container of claim 11, wherein female member and male
member are formed according to one of an extrusion process and a
pultrusion process.
14. The container of claim 11, where in the channels of the male
and female members define a plurality of at least one of grooves
and ridges.
15. The container of claim 14, further comprising an adhesive
positioned in the channels of the male and female members.
16. The container of claim 10, further comprising a plurality of
first fasteners extending through the female member and the first
rim and a plurality of second fasteners extending through female
member and the second rim.
17. The closure assembly of claim 1, wherein the main body of the
male member defines a cutout for receiving the latch.
18. The closure assembly of claim 1, wherein the gasket channel
defines a flared seating surface defining an opening and a gasket
chamber connected to the opening, the gasket being positioned
within the gasket chamber and the opening being smaller than a
width of the chamber, and the male gasket sealing feature being
tapered to conform to the flared seating surface.
19. The closure assembly of claim 1, wherein: the male member
further comprises corner protrusions positioned inwardly from the
male alignment feature and the male gasket sealing feature and
protruding outwardly from the second compression stop interface a
greater extent than the male alignment feature and male gasket
sealing feature, the corner protrusions defining first engagement
surfaces; the female member further comprises corner receivers
positioned inwardly from the female alignment feature and the
gasket channel and extending from the first compression stop
interface in a same direction as the female alignment feature, the
corner receivers defining second engagement surfaces configured to
mate with the first engagement surfaces.
20. The closure assembly of claim 1, wherein the male alignment
feature defines a taper angle and the female alignment feature
defines a flare angle, the flare angle being greater than the taper
angle.
Description
FIELD OF THE INVENTION
[0001] The present invention relates to a closure system for
containers having an alignment feature, a sealing feature, a latch,
and a latch protection feature.
BACKGROUND OF THE INVENTION
[0002] Containers for electronic equipment for use in remote or
hostile environments, such as military installations, must be
strong, resilient, and resistant to the harsh environments in which
they are used. Delicate and expensive electronic equipment is
particularly subject to damage if exposed to moisture or debris
such as sand or dirt. However, space in such installations is at a
premium, so the above needs must be met without resorting to an
excessively bulky system. Also, the containers should provide easy
access and reparability. Accordingly, there is a need for a strong,
resilient, accessible container closure system that is easy to
access, repair, and prevents alien substances from entering the
container.
SUMMARY OF THE INVENTION
[0003] In one aspect of the invention, a closure assembly for a
container includes a first wall and a second wall that come
together to close the container. The closure assembly further
includes a female member including a main body including a first
compression stop interface. The female member further defines a
channel formed in the main body and configured to receive the first
wall of the container to secure the female member to the first wall
of the container. A female alignment feature and a gasket channel
containing a gasket are formed in the first compression stop
interface.
[0004] The closure assembly further includes a male member
including a main body including a second compression stop
interface. The male member further defines a channel formed in the
main body and configured to receive the second wall of the
container to secure the male member to the second wall of the
container. A male alignment feature protrudes from the second
compression stop interface and extends into the female alignment
feature. A male gasket sealing feature protruding from the second
compression stop interface and into the gasket channel, wherein the
male gasket sealing feature forms a seal with the gasket. A latch
couples the male member to the female member, the latch having an
outer extent. One or more of the female and male members further
define a bumper extending beyond the outer extent of the latch.
BRIEF DESCRIPTION OF THE DRAWINGS
[0005] The preferred and alternative embodiments of the present
invention are described in detail below with reference to the
following drawings, in which:
[0006] FIGS. 1A and 1B are end and side views of a container in
accordance with an embodiment of the present invention;
[0007] FIG. 2 is a side cross-sectional view of a container closure
system in accordance with an embodiment of the present
invention;
[0008] FIG. 3 is a partial isometric view of a male corner portion
of a closure system in accordance with an embodiment of the present
invention;
[0009] FIG. 4 is a partial isometric view of a female corner
portion of a closure system in accordance with an embodiment of the
present invention;
[0010] FIG. 5 is a partial isometric view of male and female corner
portions engaged with one another in accordance with an embodiment
of the present invention; and
[0011] FIG. 6 is a top plan view of a disassembled UAV stored in a
container in accordance with an embodiment of the present
invention.
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT
[0012] FIG. 1 illustrates a container 10 having a lid 12, a base
14, and a closure assembly 16 according to embodiments of the
present invention. The lid 12 and base 14 can be any two container
portions that come together in a clamshell configuration. The
closure assembly 16 can be used more broadly to join any two shell
members together. The container 10 can be virtually any type of
container, including large-scale, military style containers, or
smaller containers for household use.
[0013] FIG. 2 is a cross sectional view taken along line A-A of
FIG. 1 to better illustrate the closure assembly 16. The closure
assembly 16 may be understood with respect to a vertical direction
18 that generally corresponds to vertical when the container 10 is
resting on a flat surface and a horizontal direction 20 that is
generally parallel to a surface on which the container 10 is
resting. The directions 18, 20 provide a frame of reference in
understanding the structures disclosed but may have any actual
orientation with respect to actual vertical and horizontal
directions.
[0014] The closure assembly 16 includes a female member 22 and a
male member 24. The female member 22 is coupled to the lid 12 and
the male member 24 is coupled to the base 14, and the female member
22 is coupled to the male member 24 to form a sealable closure for
the container 10. The female member 22 includes a channel 26 that
receives a portion of the lid 12, e.g. a rim or edge portion of the
lid 12. The female member 22 can be coupled to the lid 12 by an
adhesive material (not shown), such as an epoxy resin, in the
channel 26. The channel 26 is generally U-shaped. A plurality of
bolts 28 can be placed through the female member 22 and through a
portion of the lid 12 at various locations around the lid 12 to
further secure the female member 22 to the container 10. Other
suitable couplings, such as snap-fit joints, press-fit joints, or
the equivalent can also be used to join the female member 22 to the
lid 12. The channel 26 can include grooves 30, teeth, or other
texturing feature, on an interior surface of the channel 26 to
prevent the lid 12 from receding from the channel 26. A similar
channel 26 may be included on the male member 24 to couple the male
member 24 to an edge or rim portion of the base 14. The channels 26
may be generally oriented along a vertical direction 18, with the
channel 26 of the female member 22 opening upwardly and the channel
26 of the male member 24 opening downwardly.
[0015] The female and male members 22, 24 may define a compression
stop interface 32, which can include several different surfaces,
contact one another when the closure system 16 is closed. The
compression stop interface surfaces 32 can be generally flat, but
can have other profiles, such as jagged, or having other
complementary patterns. The female member 22 may include a female
alignment feature 34 having a V-shaped, or other concave, profile.
The female member 22 may also include a gasket channel 36 with a
gasket 38 inside. The gasket 38 can be made of a suitable sealing,
resilient material, such as silicone sponge gasket. The gasket
channel 36 may have a retention lip 40 to hold the gasket 38 in the
channel 36. Below the gasket channel 36, the female member 22 may
further define a seat 42. The seat 42 may define an opening into
the gasket channel 36. The seat 42 may also be flared or have some
other concave shape.
[0016] The male member 24 includes a male alignment feature 44 that
corresponds to the female alignment feature 24 in size, shape, and
position such that the male alignment feature 44 fits within the
female alignment feature 34 when the closure assembly 16 is in the
closed position. The alignment features 34, 44 can be sloped to
facilitate alignment when closing the container 10. For example,
the male alignment feature may include a convex shape conforming to
the concave shape of the female alignment feature 34. In the
illustrated embodiment, the male alignment feature 44 defines a
taper angle 46 that is smaller than or equal to a corresponding
flare angle of the female alignment feature 34. Stated differently,
an opening of the female alignment feature 34 (e.g. at the
compression stop interface 32 of female member 22) may be equal to
or larger than a base of the male alignment feature 44 (e.g. at the
compression stop interface 32 of the male member 24).
[0017] The male member 24 may also include a male gasket sealing
feature 48 that, when the container 10 is closed, protrudes into
the female member 22 into the gasket channel 36 to such a degree
that it deforms the gasket 38 to create a seal for the container
10. The male gasket sealing feature 48 can be comparable to the
male alignment feature 44 in shape. In the pictured embodiment,
however, the male and female alignment features 34, 44 are
significantly taller in vertical direction 18 than the male gasket
sealing feature 48 and the gasket channel 36. This may
advantageously protect the gasket sealing feature 48 from
scratching or other damage that might impair its ability to create
a seal with the gasket 38. The gasket sealing feature 48 may define
a taper angle 50 that generally corresponds to a flare angle of the
seat 42 such that the gasket sealing feature 48 may fit within the
seat 42. As shown in FIG. 2, the seat 42 has a depth such that at
least a portion of the gasket sealing feature 48 protrudes into the
gasket channel 36 and engages the gasket 38.
[0018] In some embodiments the female alignment feature 34 can
include a gasket channel and gasket into which the male alignment
feature 44 protrudes. In some embodiments the closure assembly 16
can include multiple alignment features and multiple gasket
channels. The gasket channel 36 can extend around the entire
perimeter of the container 10 to create a full seal. In other
embodiments, the gasket channel can extend around a portion of the
container 10. The male and female alignment features 34, 44 can
also extend around the entire perimeter of the container 10, or
only a portion. For example, the male alignment feature 44 can be a
post and the female alignment feature 34 can be a blind hole.
[0019] The closure assembly 10 may include a latch 52 to secure the
closure assembly 16 in the closed position. The latch has a main
body 54, a lever 56, and a latch arm 58. As shown by the dotted
representation 60, the latch arm has an open position (dotted) and
a closed position enabling the container 10 to be opened and
closed. The latch 52 may be secured to the male member 24 and the
female member 22 may include a latch strike 62 that extends from
the main body of the female member 22. The latch arm 58 engages
with the latch strike 62 to secure the closure assembly 16 in the
closed position with the compression stop interfaces 32 pressed
together and with the male gasket sealing feature 48 pressed
sealably against the gasket 38.
[0020] The closure assembly 16 may also include a bumper 64 formed
on the female member 22. The bumper 64 may protect the strike 62
and the portion of the arm 58 engaging the strike 62. For example,
the male member 24 may define a recess 66 above the strike 62 that
enables the arm 58 to move into and out of engagement with the
strike 62. The bumper 64 may be positioned vertically above the
recess 66 and protrude horizontally outwardly a greater extent than
the strike 62 and the horizontal extent of the latch arm 58 when
engaging the strike 62. The bumper 64 may be positioned such that
at least a portion thereof that extends horizontally outwardly
further than the strike 62 and/or a portion of the latch arm 58
engaged therewith is vertically offset from the strike 62 by an
amount between 1.1 and 5 times the vertical travel of the latch arm
58 required to move the latch arm 58 into and out of engagement
with the strike. In this manner, the bumper 64 may absorb many
collisions that might otherwise impact the strike 62 and latch arm
58.
[0021] In some embodiments, a bumper 68 may secure to the male
member 24. The bumpers 68 may extend horizontally outwardly from
the main body of the male member 24 a greater extent than the latch
52. In some embodiments, the latch 52 may seat within a cutout
portion of the bumper 68. The bumper 68 may extend from the
compression stop interface 32 downwardly along a major vertical
extent of the latch 52. In this manner, collisions that might
impact the latch 52 and thereby cause damage or unintended opening
of the latch may be prevented or otherwise reduced. In the
illustrated embodiment, the bumper 68 does not extend vertically
downward completely past the lever 56 of the latch 52 thereby
providing accessibility in order to open and close the latch 52.
However, in other embodiments, the bumper 68 does extend vertically
along the entire extent of the latch 52 including the lever 56.
[0022] In the illustrated embodiment, the lid 12 and base 14 may
have a material thickness 70 at the edge portions positioned within
the channels 26. The female member 22 and male member 24 may have a
horizontal width 72 that is substantially greater than the
thickness 70. For example, the compression stop surface 32 may have
a width 72 that is between four and eight, preferably between five
and seven times the width 70. In this manner, the closure system 16
provides rigidity to the lid 12 and base 14 and resists twisting
and bending that would make mating of the lid 12 and base 14
difficult. However, in other embodiments, where weight is more
critical, the thickness 72 may be smaller and the other benefits of
the disclosed closure system may nonetheless be achieved. Likewise,
the lid 12 and base 14 may be made thinner due to rigidity of the
members 22, 24. Also, the complexity of the members 22, 24 may be
achieved using an extrusion process, or a pultrusion process in the
case of composite materials, whereas the lid 12 and base 14 are
also made by a relatively simple manufacturing process such as
molding sheets of material, rotational molding, vacuum infusion
process (VIP), or some other process.
[0023] The closure assembly 16 can be used with any two components
sufficiently similar to a lid and base assembly. Any two web-like
structures similar to the lid 10 and base 12 can be joined by the
closure assembly 16. For example, in the illustrated embodiment,
edge portions of the lid 12 and base 14 are oriented along the
vertical direction 18, portions of the lid 12 and base 14 may
transition to a drafted angle of at least two degrees above the
closure channel into which it is bonded. The closure assembly 16
can be retrofitted to an existing structure or container to provide
additional rigidity to the container. The additional structure and
thickness of the assembly 16 gives the container more strength, and
makes aligning the lid and base of the container more easy to align
and close. The gasket 34 and alignment features provide a
leak-resistant seal that can withstand a harsh external environment
and protect the contents of the container. The closure assembly 16
can be made using an inexpensive extrusion process because, in at
least some embodiments, the profile shown in FIG. 2 is uniform
along its length. Non-uniform features may then be formed, e.g.
machined) in the extruded member to achieve the closure system 16
shown.
[0024] Although certain structures are disclosed above as being
features of or secured to the female member 22 or the male member
24, such an arrangement may be switched. For example, though the
female alignment feature 34 and gasket channel are secured to the
same member in FIG. 2, in other embodiments these features may be
formed in different members. Likewise, although the male alignment
feature 44 and gasket sealing feature 48 are secured to the same
member in FIG. 2, in other embodiments these features may be formed
on different members. Likewise, the strike 62 and latch 52 may be
secured to either of the male and female members 22, 24.
[0025] Referring to FIG. 3, the male members 24 may be joined
together by male corner members 74. For example, the corner members
74 may define receivers in which the male members 24 insert.
Likewise, the corner members 74 may define protuberances that
insert within receivers defined by the male members 24. The corner
members 74 may define curved gasket sealing features 76 that abut
the gasket sealing features 48 of the male members 24 joined to the
corner members 74. The gasket sealing features 76 may have a
similar cross section to the gasket sealing features 48. In this
manner, near-continuous engagement with a gasket is enabled. In the
illustrated embodiment, the corner members 74 do not include a
curved structure abutting the male alignment features 44 of the
male members 24 secured to the corner members 74. In some
embodiments, a continuous alignment feature is included in the
corner member 74 to bolster engagement between the lid 12 and base
14. As is apparent in FIG. 3, the male members 24 may define
cutouts 78. The cutouts 78 may intersect the bumper 68 and provide
a recess to receive the latch 52. Although not shown in FIG. 3, the
corner members 74 may also include channels 26 for receiving an
edge portion of a base 14.
[0026] In some embodiment, the corner members 74 may include corner
protrusions 80 secured thereto or formed thereon. The corner
protrusions 80 are positioned inwardly from the sealing features 76
and extend vertically outward more than the sealing features 76. As
is apparent in FIG. 3, the extent of the corner protrusions 74
vertically above the compression stop interface 32 is also larger
than the extent of the male alignment features 44. For example, the
vertical extent of the corner protrusion 74 is between two and
eight times that of the sealing feature 76. The corner protrusions
76 may define a sloped or angled surfaces 82 that join straight
surfaces 84. The sloped surfaces 82 may define a tapered portion.
The corner protrusion 76 may further define a chamfered upper
portion 86. In some embodiments, the corner member protrusion 76 is
formed monolithically with the corner member 74 or may fasten to
the corner member 74 as shown. In still other embodiments, the
corner protrusion 76 may be formed by two plates that protrude in a
similar fashion, each being secured to one arm of the corner member
74.
[0027] Referring to FIG. 4, female members 22 may further secure to
female corner members 88. The female corner members 88 may define
inner stops 90 secured to or formed on the corner members 88. The
inner stops 90 of a corner member 88 may define slopes surfaces 92
and straight surfaces 94 sized and configure to engage the sloped
surfaces 82 and straight surfaces 84 of the corner protrusions 80,
respectively of the male corner members 74. The inner stops 90
therefore define a receiver for receiving the corner protrusions 80
and facilitate alignment of the corner members 88 with the male
corner members 74.
[0028] Referring to FIG. 5, in use the female and male members 22,
24 may be engaged with one another and the male and female corner
members 74, 88 may also be engaged with one another as shown. The
sloped surfaces 82 of the protuberance 76 engaged the sloped
surfaces of the stops 90. Likewise, the straight surfaces 84 of the
protuberance 84 engage the straight surfaces 94 of the stops 90.
The actual configuration of the surfaces 82, 84 may define any
convex shape and surfaces 92, 94 may define any concave shape such
that the surfaces 82, 84 may be positioned in engagement with the
surfaces 92, 94 in order to align the male members 24 and female
members 22. As is apparent in FIG. 5, the chamfered surface 86 is
offset from the female corner member 88 when engaged. In this
manner, the chamfered surface accommodates slight misalignments
between the corner members 74, 88 during installation of the lid 12
onto the base 14.
[0029] Referring to FIG. 6, a container 10 using the closure system
16 described herein may be used to store various items. For
example, a unmanned aerial vehicle (UAV) may be stored in the
container 10. For example, wings 96 of the UAV may be supported and
retained within the cradles 98, such as disclosed in U.S.
application Ser. No. ______/______ filed Aug. ______, 2013 and
entitled RETENTION SYSTEM AND METHOD FOR A WING (Attorney Docket
No. ECSC-1-1024), which is hereby incorporated herein by reference
in its entirety.
[0030] In such embodiments, a plurality of cradles 98 may secure to
the container 10 either directly or indirectly by means of a
fixture or frame member. The wing 96 is mounted within the cradles
98 and is thereby retained against movement during shipping. The
remainder of the UAV may also secure within the container 10,
including the fuselage 100. For example, the fuselage 100 may have
a fastening system 102 and indexing members 104 secured thereto as
described U.S. application Ser. No. ______/______ filed Aug.
______, 2013 and entitled FUSELAGE INDEXING SYSTEM AND METHOD
(Attorney Docket No. ECSC-1-1026), which is hereby incorporated
herein by reference. The container 10 may further have receivers
106 for engaging the indexing members 104 and a corresponding frame
108 mounting the receivers to the container 10 as described in
disclosed in U.S. application Ser. No. ______/______ filed Aug.
______, 2013 and entitled FUSELAGE INDEXING SYSTEM AND METHOD
(Attorney Docket No. ECSC-1-1026).
[0031] A spar 110 of the wing 96 may be further restrained by means
of the spar retention system 112 as described in U.S. application
Ser. No. ______/______ filed Aug. ______, 2013 and entitled WING
SPAR RETENTION SYSTEM AND METHOD (Attorney Docket No. ECSC-1-1025),
which is hereby incorporated herein by reference. In this manner,
movement of the wing 96 transverse to the longitudinal axis thereof
may be restrained by means of the cradles 98 and movement along the
longitudinal axis may be restrained by the spar retention system
112.
[0032] As is apparent from the foregoing description, the disclosed
closure system 16 for a container 10 provides a stiff,
self-aligning closure that reduces time and effort to install the
lid 12 on the base 14. The closure system 16 provides inherent
stiffness to the container 10 which helps it maintain shape and
resist large forces during the large pressure changes seen during
air transport. The closure system 16 further resists relative
lateral movement between lid 12 and base 14 assemblies during large
lateral accelerations experienced during shipping.
[0033] While the preferred embodiment of the invention has been
illustrated and described, as noted above, many changes can be made
without departing from the spirit and scope of the invention.
Accordingly, the scope of the invention is not limited by the
disclosure of the preferred embodiment. Instead, the invention
should be determined entirely by reference to the claims that
follow.
* * * * *