WO1997017195B1 - High strength, lightweight pressurized vehicle skin structure - Google Patents
High strength, lightweight pressurized vehicle skin structureInfo
- 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
Links
- 210000003491 Skin Anatomy 0.000 title claims abstract 55
- 238000010276 construction Methods 0.000 claims abstract 32
- 239000000463 material Substances 0.000 claims abstract 4
- 239000007789 gas Substances 0.000 claims 14
- 239000001307 helium Substances 0.000 claims 3
- 229910052734 helium Inorganic materials 0.000 claims 3
- SWQJXJOGLNCZEY-UHFFFAOYSA-N helium(0) Chemical compound [He] SWQJXJOGLNCZEY-UHFFFAOYSA-N 0.000 claims 3
- 238000004519 manufacturing process Methods 0.000 abstract 1
- 230000035882 stress Effects 0.000 abstract 1
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.
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
AU12710/97A AU1271097A (en) | 1995-11-06 | 1996-11-04 | High strength, lightweight pressurized vehicle skin structure |
EP96943480A EP0883483A4 (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) |
Families Citing this family (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE19615505C2 (en) * | 1996-04-19 | 2001-09-06 | Bluemle Blueco Technik | Double plate body |
WO2000004256A1 (en) * | 1998-07-13 | 2000-01-27 | Prospective Concepts Ag | Shape-free pneumatic member |
US6412232B1 (en) | 1999-03-26 | 2002-07-02 | Anthony Italo Provitola | Structural system of toroidal elements and method of construction therewith |
DE19921037C2 (en) * | 1999-05-08 | 2001-09-27 | Genima Innovations Marketing G | Quick-build and formwork panel and method for preparing one |
AU5802100A (en) | 1999-05-08 | 2000-11-21 | Gunter Tannhauser | Rapid construction and formwork panel, method for trimming the same, and method and device for the production thereof |
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 |
CA3008499C (en) * | 2016-10-31 | 2021-04-13 | 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 |
Family Cites Families (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3013641A (en) * | 1957-04-29 | 1961-12-19 | Thompson Ramo Wooldridge Inc | Structural element |
US4043721A (en) * | 1968-07-11 | 1977-08-23 | Lemelson Jerome H | Composite body molding apparatus |
US3596622A (en) * | 1969-01-27 | 1971-08-03 | Moore Alvin E | Light-weight wreck-resistant vehicle |
US3742663A (en) * | 1971-08-02 | 1973-07-03 | Mc Donnell Douglas Corp | Panel blocking |
BE792077A (en) * | 1971-11-29 | 1973-03-16 | Ici Australia Ltd | |
US3876492A (en) * | 1973-05-21 | 1975-04-08 | Lawrence A Schott | Reinforced cellular panel construction |
US3865679A (en) * | 1973-07-09 | 1975-02-11 | Jesse R Hale | Sandwich panel having cellular core structure with reinforcing elements |
US4052025A (en) * | 1975-04-03 | 1977-10-04 | Clark Frank M | Semi-buoyant aircraft |
US4301584A (en) * | 1980-01-31 | 1981-11-24 | United Technologies Corporation | Method of forming fiber and metal matrix composite |
US4730797A (en) * | 1985-08-12 | 1988-03-15 | Minovitch Michael Andrew | Inflatable core orbital construction method and space station |
US4808457A (en) * | 1986-08-19 | 1989-02-28 | Whirlpool Corporation | Heavy gas-filled multilayer insulation panels |
US5030501A (en) * | 1989-05-31 | 1991-07-09 | Raven Marketing, Inc. | Cushioning structure |
US5266379A (en) * | 1991-03-15 | 1993-11-30 | Schaeffer Bernarr C | Tetrahedron filled panels |
US5204161A (en) * | 1991-06-03 | 1993-04-20 | Mcdonnell Douglas Corporation | Fabrication of panel structure |
US5424113A (en) * | 1993-06-23 | 1995-06-13 | The United States Of America As Represented By The Secretary Of The Navy | Lattice core sandwich construction |
-
1995
- 1995-11-06 US US08/551,841 patent/US5716693A/en not_active Expired - Fee Related
-
1996
- 1996-11-04 AU AU12710/97A patent/AU1271097A/en not_active Abandoned
- 1996-11-04 WO PCT/US1996/017611 patent/WO1997017195A1/en not_active Application Discontinuation
- 1996-11-04 EP EP96943480A patent/EP0883483A4/en not_active Withdrawn
-
1997
- 1997-09-16 US US08/932,143 patent/US6074509A/en not_active Expired - Fee Related
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