Expandable fuel cell

• US 5,927,651 A
• Filed: 05/15/1997
• Issued: 07/27/1999
• Est. Priority Date: 05/15/1997
• Status: Expired due to Term

• Current Assignee: Mcdonnell Douglas
• Original Assignee: Mcdonnell Douglas
• Inventors: Geders, Paul Francis, Groeneveld, John David, Wille, Robert Henry
• Primary Examiner(s): Jordan, Charles T.
• Assistant Examiner(s): Wesson, Theresa M.
• Application Number:
  US08/856,961
• Time in Patent Office: 803 Days
• Field of Search: 244/135 R, 244/135 B, 244/119, 244/120, 244/130, 244/133
• US Class Current: 244/135.00B
• CPC Class Codes: B64D 37/04 Arrangement thereof in or on aircraft

Abstract

An expandable fuel cell (72) for an aircraft (70) has a flexible structure (126) having a perimeter (124) attached to an airframe of the aircraft (70). The flexible structure (126) has an empty position, in which the flexible structure (126) approximately conforms to a moldline (76) of the aircraft (70), and a full position, in which the flexible structure (126) forms a smooth curvilinear protrusion from the moldline (76) of the aircraft (70). A fuel bladder (152) is positioned between the flexible structure (126) and the airframe.

Claims

1. An expandable fuel cell for an aircraft, comprising:

a collapsible fuel cell bladder; and

a reinforced elastomer structure covering the collapsible fuel cell bladder, the reinforced elastomer structure having a tapered leading edge, a tapered trailing edge, and a connecting center section, the reinforced elastomer structure having a perimeter attached to an airframe of the aircraft, the reinforced elastomer structure having a retracted position conforming substantially to a moldline of the aircraft and continuously expanding to a full position, in which the reinforced elastomer structure forms a smooth curvilinear bulge in the moldline of the aircraft.

2. The expandable fuel cell of claim 1, wherein the reinforced elastomer structure comprises a plurality of reinforced elastomer panels connected to a plurality of rigid panels.

3. The expandable fuel cell of claim 1, wherein the perimeter of the reinforced elastomer structure is attached to a fuselage of the aircraft.

4. The expandable fuel cell of claim 1, wherein a volume of the smooth curvilinear bulge is directly proportional to a fuel volume in the collapsible fuel cell bladder.

5. The expandable fuel cell of claim 1, wherein the reinforced elastomer structure comprises a reinforced elastomer sheet, a perimeter rigid block attached to the reinforced elastomer sheet, and a longitudinal strut attached to the reinforced elastomer sheet.

6. The expandable fuel cell of claim 1, further including a rigid skeleton between the collapsible fuel cell bladder and the reinforced elastomer surface.

7. The expandable fuel cell of claim 1, wherein the collapsible fuel cell bladder has a fuel liner attached to the perimeter.

8. The expandable fuel cell of claim 7, wherein the collapsible fuel cell bladder includes a fuel-proof coating applied to a skin of the aircraft.

9. The expandable fuel cell of claim 8, wherein the fuel coating is a polyurethane.

10. An expandable fuel cell for an aircraft, comprising:

a flexible structure having a perimeter attached to an airframe of the aircraft, the flexible structure having an empty position, in which the flexible structure approximately conforms to a moldline of the aircraft, and a full position, in which the flexible structure forms a smooth curvilinear protrusion from the moldline of the aircraft; and

a fuel bladder positioned between the flexible structure and the airframe.

11. The expandable fuel cell of claim 10, wherein the flexible structure comprises a reinforced elastomer panel attached to a rigid plate.

12. The expandable fuel cell of claim 11, further including a structural skeleton between the flexible structure and the fuel bladder.

13. The expandable fuel cell of claim 12, wherein the flexible structure is attached to a wing of the aircraft.

14. The expandable fuel cell of claim 13, further including a fuel line connected between the fuel bladder and an internal fuel tank.

15. The expandable fuel cell of claim 14, further including a pump attached to the fuel line.

16. The expandable fuel cell of claim 10, wherein the perimeter is a rigid material that attaches to an airframe of the aircraft and mates with a skin of the aircraft.

17. The expandable fuel cell of claim 16, wherein the perimeter includes a fuel seal that mates with the collapsible fuel cell bladder.

18. An expandable fuel cell for an aircraft comprising:

a fuel liner; and

an elastomer structure having a perimeter attached to the airframe and mating with the fuel liner, the elastomer structure having a retracted position in which the elastomer structure approximately conforms to a moldline of the aircraft and the elastomer structure having a full position in which the elastomer structure forms a smooth curvilinear bulge on the moldline of the aircraft.

19. The expandable fuel cell of claim 18, wherein a volume contained between the fuel liner and the elastomer structure in the retracted position is equal to a standard fuel payload.

20. The expandable fuel cell of claim 19, wherein the elastomer structure has a reinforced elastomer sheet connected to a strut.

21. The expandable fuel cell of claim 19, further including a skeletal structure supporting the elastomer structure.

22. The expandable fuel cell of claim 21, wherein the elastomer structure comprises a reinforced elastomer panel attached to a rigid plate.

23. The expandable fuel cell of claim 22, wherein the rigid plate is concave.

24. An aircraft, comprising:

a fuselage;

an engine attached to the fuselage;

a pair of wings attached to the fuselage; and

an expandable fuel cell connected to the wing wherein the expandable fuel cell has fuel liner and an elastomer structure having a perimeter attached to the airframe and mating with the fuel liner, the elastomer structure having a retracted position in which the elastomer structure approximately conforms to a moldline of the aircraft and the elastomer structure having a full position in which the elastomer structure forms a smooth curvilinear bulge on the moldline of the aircraft.