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WO1997017195B1 - High strength, lightweight pressurized vehicle skin structure - Google Patents

High strength, lightweight pressurized vehicle skin structure

Info

Publication number
WO1997017195B1
WO1997017195B1 PCT/US1996/017611 US9617611W WO9717195B1 WO 1997017195 B1 WO1997017195 B1 WO 1997017195B1 US 9617611 W US9617611 W US 9617611W WO 9717195 B1 WO9717195 B1 WO 9717195B1
Authority
WO
WIPO (PCT)
Prior art keywords
cone
skin construction
sandwich
sandwich skin
cones
Prior art date
Application number
PCT/US1996/017611
Other languages
French (fr)
Other versions
WO1997017195A1 (en
Filing date
Publication date
Priority claimed from US08/551,841 external-priority patent/US5716693A/en
Application filed filed Critical
Priority to EP96943480A priority Critical patent/EP0883483A4/en
Priority to AU12710/97A priority patent/AU1271097A/en
Publication of WO1997017195A1 publication Critical patent/WO1997017195A1/en
Publication of WO1997017195B1 publication Critical patent/WO1997017195B1/en

Links

Abstract

A sandwich skin construction (10) that is comprised of an internal structure (16) comprising a plurality of cones (12) disposed between two outer skins (14a) is disclosed. The interior contains a pressurized gas to give the resulting sandwich skin construction (10) added strength over a similarly constructed non-pressurized structure of the same material with an equivalent mass. Various attributes of the cones (12) can be adjusted, for example, size and angle, to optimize the performance of the sandwich skin construction (10) to a variety of external stresses. Moreover, a method is provided for manufacturing the sandwich skin construction (10). The structure can be placed in a pressurized environment before attaching the outer skins (14a).

Claims

AMENDED CLAIMS
[received by the International Bureau on 20 May 1997 (20.05.97); original claims 1-26 amended; remaining claims unchanged (6 pages)]
1. A sandwich skin construction comprising: an internal structure comprising a plurality of substantially similarly shaped and sized cones having hollow cores; a first skin attached to one surface of said internal structure forming a first pressure seal at a top of selected ones of said plurality of cones; and, a second skin attached to the other surface of said internal structure forming a second pressure seal at a bottom of said selected ones of said plurality of cones, whereby each of said selected ones of said plurality of cones is separately sealed and pressurized.
2. A sandwich skin construction as in claim 1 wherein said cones are coupled side-by-side such that each cone is inverted with respect to each adjacent cone.
3. A sandwich skin construction as in claim 1 further comprising a gas disposed within said internal structure forming a pressure between said first and second skins different from the atmospheric pressure.
4. A sandwich skin construction as in claim 3 wherein said gas comprises a doping gas.
5. A sandwich skin construction as in claim 4 wherein said doping gas comprises helium.
6. A sandwich skin construction as in claim 2 wherein the pressure of said gas is selected to be substantially equivalent to a working pressure of the skin material.
7. A sandwich skin construction as in claim 1 wherein said cones are characterized by angles selected to oppose an expected force incident upon the surface of one of said first and second skins. 8. A sandwich skin construction as in claim 7 wherein said angles are individually selected throughout the
internal structure relative to a localized expected force incident upon the surface of at least one of said first and second skins.
9. A sandwich skin construction as in claim 1 wherein a top rim of each said cone is sealably affixed to one of said first and second skin and a base rim of each said cone is sealably affixed to the other one of said first and second skin forming a pressurized cell, whereby a puncture in one of said skins is localized and results in minimal loss of pressure and structural integrity.
10. A sandwich skin construction comprising: an internal structure comprising a plurality of substantially similarly shaped and sized cells, wherein each cell encloses a volume; a first skin attached to one surface of said internal structure forming a first pressure seal on a top of selected ones of said plurality of cells,- a second skin attached to the other surface of said internal structure forming a second pressure seal on a bottom of said selected ones of said plurality of cells whereby each of said selected ones of said plurality of cells is separately sealed and pressurized; and, a gas disposed within said volume of said selected ones of said plurality of cells forming a pressure between said first and second skins different from the atmospheric pressure.
11. A sandwich skin construction as in claim 10 wherein said cells are cones having a hollow core.
12. A sandwich skin construction as in claim 11 wherein said cones are coupled side-by-side such that each cone is inverted with respect to each adjacent cone.
13. A sandwich skin construction as in claim 11 wherein said cones are major cones having a minor cone invertedly disposed within said hollow core of said major cone such that the base rim of said minor cone is attached to the interior wall of said major cone, the top of said minor cone
is attached to one of said first and second skin, and the axes of said major cone and said minor cone are substantially aligned.
14. A sandwich skin construction as in claim 10 wherein said gas comprises a doping gas for detecting leaks in the sandwich skin construction.
15. A sandwich skin construction as in claim 14 wherein said doping gas is helium.
16. A sandwich skin construction as in claim 10 wherein said pressure of said gas is selected to be substantially equivalent to the working pressure of the skin material.
17. A sandwich skin construction as in claim 11 wherein said cones are characterized by angles selected to oppose the force incident upon the surface of one of said first and second skins.
18. A sandwich skin construction as in claim 17 wherein said angles are individually selected throughout the internal structure relative to localized force incident upon the surface of at least one of said first and second skins.
19. A sandwich skin construction as in claim 10 wherein each said cell is sealably affixed to said first and second skins, whereby a puncture in one of said skins is substantially localized and results in minimal loss of pressure and structural integrity.
20. A sandwich skin construction comprising: a substantially planar internal structure comprising a plurality of similarly shaped and sized cone members, wherein said cone members comprise a major cone having a hollow core and a minor cone having a hollow core and invertedly disposed within said major cone such that a base rim of said minor cone is attached to an interior wall of said major cone, a top of said minor cone extends substantially to the base of said major cone, and the axes of said major cone and said minor cone are substantially aligned; a first skin attached to one surface of said internal structure forming a first pressure seal on a top of selected ones of said plurality of cone members; and, a second skin attached to an other surface of said internal structure forming a second pressure seal on a bottom of said selected ones of said plurality of cones whereby each of said selected ones of said plurality of cells is separately sealed and pressurized.
21. A sandwich skin construction as in claim 20 wherein said cone members are coupled side-by-side such that each said cone member is inverted with respect to each adjacent cone member.
22. A sandwich skin construction as in claim 20 further comprising a gas disposed within said internal structure forming a pressure different from the atmospheric pressure between said first and second skins.
23. A sandwich skin construction as in claim 22 wherein said pressure is selected to be substantially equivalent to the working pressure of the skin material.
2 . A sandwich skin construction as in claim 22 wherein said gas comprises a doping gas for detecting leaks in the sandwich skin construction.
25. A sandwich skin construction as in claim 24 wherein said doping gas is helium.
26. A sandwich skin construction as in claim 20 wherein said cones are characterized by angles selected to oppose the force incident upon the surface of one of said first and second skins.
PCT/US1996/017611 1995-11-06 1996-11-04 High strength, lightweight pressurized vehicle skin structure WO1997017195A1 (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
EP96943480A EP0883483A4 (en) 1995-11-06 1996-11-04 High strength, lightweight pressurized vehicle skin structure
AU12710/97A AU1271097A (en) 1995-11-06 1996-11-04 High strength, lightweight pressurized vehicle skin structure

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US08/551,841 US5716693A (en) 1995-11-06 1995-11-06 High strength, lightweight pressurized structure for use as the skin of a spacecraft or other vehicle
US08/551,841 1995-11-06

Publications (2)

Publication Number Publication Date
WO1997017195A1 WO1997017195A1 (en) 1997-05-15
WO1997017195B1 true WO1997017195B1 (en) 1997-07-03

Family

ID=24202908

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/US1996/017611 WO1997017195A1 (en) 1995-11-06 1996-11-04 High strength, lightweight pressurized vehicle skin structure

Country Status (4)

Country Link
US (2) US5716693A (en)
EP (1) EP0883483A4 (en)
AU (1) AU1271097A (en)
WO (1) WO1997017195A1 (en)

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WO2000068527A1 (en) 1999-05-08 2000-11-16 Tannhaeuser Gunter Rapid construction and formwork panel, method for trimming the same, and method and device for the production thereof
DE19921037C2 (en) * 1999-05-08 2001-09-27 Genima Innovations Marketing G Quick-build and formwork panel and method for preparing one
US7389612B1 (en) * 2001-08-09 2008-06-24 Fischbeck Richard D Geodesic structure
DE102004062264A1 (en) * 2004-12-23 2006-07-06 Fraunhofer-Gesellschaft zur Förderung der angewandten Forschung e.V. Building element, in particular wall cladding, and method for its production
US7780061B2 (en) * 2007-09-27 2010-08-24 The Boeing Company Joining fixtures, methods for joining, and joined structures
EP2077357A1 (en) * 2008-01-04 2009-07-08 Siegfried Lösch Structural member and method of manufacturing the same
WO2011082979A2 (en) * 2009-12-14 2011-07-14 Dieter Walter Test device and test system for acc systems
DE202010016304U1 (en) * 2010-12-07 2011-03-17 Grod, Wassilij Composite arrangement of at least two parallel cover plates with spacer and stiffening means
IL209950A0 (en) * 2010-12-13 2011-02-28 Gigi Simovich Lightweight impact resistant panel
CN105082635A (en) * 2015-08-26 2015-11-25 杭州电子科技大学 Multicycle energy absorbing structure
SG11201805175VA (en) * 2016-10-31 2018-07-30 Yue Zhang Metal plate having hollow tubes sandwiched therein and its use
US10507935B1 (en) * 2018-05-02 2019-12-17 Northrop Grumman Systems Corporation Orthogonal shear structure
EP4240986A1 (en) * 2020-11-04 2023-09-13 Zephyros Inc. Energy absorption member

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