Inflatable flying body for the rescue descent of a person

• US 6,607,166 B1
• Filed: 08/06/2002
• Issued: 08/19/2003
• Est. Priority Date: 08/06/2002
• Status: Expired due to Term

• Current Assignee: Airbus Defence and Space GmbH
• Original Assignee: Astrium GmbH (Airbus SE)
• Inventors: Walter, Stephan, Zaytsev, Igor, Pichkhadze, Konstantin
• Primary Examiner(s): Carone, Michael J.
• Assistant Examiner(s): Semunegus, Lulit
• Application Number:
  US10/214,284
• Time in Patent Office: 378 Days
• Field of Search: 244/138.R, 244/141, 244/140, 244/146, 244/160
• US Class Current: 244/138.00R
• CPC Class Codes: A62B 1/22 by making use of jumping devices, e.g. jumping-sheets, jumping-mattresses
• CPC Class Codes: B64D 1/14 Absorbing landing shocks
• CPC Class Codes: B64D 19/00 Non-canopied parachutes
• CPC Class Codes: B64D 25/08 Ejecting or escaping means escape apertures B64C

Abstract

A person can safely descend from a burning high-rise building or the like using an inflatable flying body that has a hollow conical form in an inflated deployed condition, but is deflated and folded into a backpack form in a stowed condition. The flying body includes an upper stabilizing ring, a lower nose structure with a pneumatic damping body, spoke struts extending conically therebetween, a cover skin covering the abovementioned inflatable components to form the conical outer surface and provide aerodynamic braking drag, and gas generators to inflate the inflatable components. A person straps on the apparatus in the stowed backpack form and pulls a handle to actuate the gas generators for inflating the apparatus, whereby the expanding apparatus ejects the person from the building and then orients itself in a nose-down attitude during the descent. The pneumatic damping body damps and dissipates the landing impact energy.

Claims

1. An apparatus for enabling a person or cargo to descend from an elevation higher than a landing area, wherein said apparatus is unfoldable and inflatable into a deployed configuration having a generally conical outer shape with a narrower nose end and a wider end opposite thereto and a hollow inner space, and wherein said apparatus in said deployed configuration comprises:

an inflatable outer stabilizing ring at said wider end;

a nose structure including an inflatable central pneumatic damping element at said narrower nose end;

plural inflatable spoke struts extending conically between said nose structure and said outer stabilizing ring;

a cover skin arranged on and spanning between said spoke struts to define at least a portion of said generally conical outer shape;

at least one gas generator pneumatically connected to and adapted to inflate said outer stabilizing ring, said central pneumatic damping element, and said spoke struts; and

a load support element that is adapted to receive the person or cargo thereon and that is arranged and secured in or on said nose structure at a location on or above said central pneumatic damping element in said deployed configuration.

2. The apparatus according to claim 1, wherein said apparatus is further deflatable and foldable into a stowed configuration, and wherein said at least one gas generator is actuatable to inflate said outer stabilizing ring, said central pneumatic damping element and said spoke struts and thereby to deploy said apparatus from said stowed configuration to said deployed configuration.

3. The apparatus according to claim 2, wherein said stowed configuration is a backpack configuration adapted to be worn and carried on the back of the person, and further comprising securing straps that are secured to said load support element and adapted to secure said apparatus onto the person with the load support element on the back of the person.

4. The apparatus according to claim 1, wherein said load support element comprises a flexible membrane arranged in, on or above said central pneumatic damping element.

5. The apparatus according to claim 1, wherein said load support element comprises a rigid load bearing frame.

6. The apparatus according to claim 1, wherein said load support element comprises a rigid load bearing platform.

7. The apparatus according to claim 1, further comprising securing straps with at least one buckle, which are secured on said load support element and which are adapted and configured to be secured about the shoulders and chest of the person with the load support element arranged on the back of the person.

8. The apparatus according to claim 1, wherein said hollow inner space is surrounded and enclosed by said nose structure, said spoke struts, said outer stabilizing ring and said cover skin, and is open to an external environment outside of said apparatus through an open inner diameter of said outer stabilizing ring at said wider end.

9. The apparatus according to claim 1, wherein said central pneumatic damping element comprises an inflatable ring element.

10. The apparatus according to claim 9, wherein said inflatable ring element has a hollow conically tapering inflated shape that forms a tapered conical frustum nose tip portion of said nose structure at said narrower nose end.

11. The apparatus according to claim 1, wherein said central pneumatic damping element comprises an inflatable spherical element that forms a rounded nose tip portion of said nose structure at said narrower nose end.

12. The apparatus according to claim 11, wherein said nose structure further comprises an inflatable inner stabilizing ring connected to said central pneumatic damping element, and wherein said spoke struts extend conically between said inner stabilizing ring and said outer stabilizing ring.

13. The apparatus according to claim 1, wherein said nose structure further comprises an inflatable inner stabilizing ring connected to said central pneumatic damping element, and wherein said spoke struts extend conically between said inner stabilizing ring and said outer stabilizing ring.

14. The apparatus according to claim 1, wherein said at least one gas generator comprises a first gas generator pneumatically connected to said outer stabilizing ring and a second gas generator that is separate from said first gas generator and is pneumatically connected to said central pneumatic damping element.

15. The apparatus according to claim 1, wherein said generally conical outer shape spans a conical angle in a range from 80°

to 100°

.

16. The apparatus according to claim 1, wherein said generally conical outer shape spans a conical angle of about 90°

.

17. The apparatus according to claim 1, wherein said generally conical outer shape is a circular conical outer shape.

18. The apparatus according to claim 1, wherein said apparatus is so configured in said deployed configuration such that said apparatus is self-orienting with said narrower nose end oriented downward and said wider end oriented upward in a free-fall descent of said apparatus with the person or cargo on the load support element.

19. The apparatus according to claim 1, wherein said apparatus in said deployed configuration has a center of gravity relatively closer to said narrower nose end and a center of aerodynamic drag relatively closer to said wider end in a free-fall descent of said apparatus with the person or cargo on said load support element.

20. The apparatus according to claim 1, wherein said apparatus in said deployed configuration is so configured as to limit a free-fall descent velocity of said apparatus with the person or cargo on said load support element to a maximum terminal velocity of not more than 8.5 m/sec.

21. The apparatus according to claim 1, wherein said apparatus is adapted to be deployed to said deployed configuration and utilized to descend from any elevation of at least 5 m.

22. A method for a person to descend from a structure at an elevation of at least 5 meters above a landing area, using the apparatus according to claim 1, which is initially deflated and folded into a stowed configuration having a compact package shape and which is unfoldable and inflatable from said stowed configuration into said deployed configuration having said generally conical outer shape, said method comprising the following steps:

a) securing said apparatus in said stowed configuration on a person'"'"'s back in the manner of a backpack;

b) positioning said person adjacent to an egress of said structure with said apparatus and said person'"'"'s back facing outwardly away from said structure;

c) actuating at least one said gas generator to inflate and deploy said apparatus from said stowed configuration to said deployed configuration, whereby an inflation of said apparatus pulls said person out of and away from said structure;

d) descending said person from said structure to said landing area with said apparatus in said deployed configuration, wherein said generally conical outer shape is oriented with said narrower nose end thereof pointed downward; and

e) touching said apparatus down onto said landing area while a touchdown impact is cushioned by said pneumatic damping element of said apparatus.