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특허 상세정보

Inflatable conformable fuel tank

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64D-037/02   
미국특허분류(USC) 244/135R ; 244/135B ; 244/130 ; 244/219 ; 92/035 ; 220/720
출원번호 US-0579742 (1995-12-28)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Feix & Feix
인용정보 피인용 횟수 : 18  인용 특허 : 0
초록

The invention discloses a deployable, inflatable conformable fuel tank assembly constructed to be installed at a certain location on an aircraft and to be retained at that certain location throughout the entire flight operation of the aircraft. The fuel tank assembly is constructed to be movable between a first, deployed aerodynamic configuration in which the assembly can hold a supply of liquid fuel, and a second, stowed aerodynamic configuration in which the exterior surface of the assembly conforms to a surface of the aircraft underlying the assembly....

대표
청구항

[ What is claimed is:] [1.] A method of conforming a fuel tank assembly with two different aerodynamic configurations on an aircraft, said method comprising:constructing the assembly with a first, inner, liquid chamber for containing a supply of liquid fuel in a first, aerodynamic deployed configuration of the assembly;constructing the assembly with a second, outer, gas chamber for containing a pressurized volume of gas in the first, aerodynamic deployed configuration of the assembly;incorporating bidirectionally extending structural elements in said sec...

이 특허를 인용한 특허 피인용횟수: 18

  1. Burdsall ; II Charles Wesley ; Volk John Alan. Adaptive deployable ramp for suppression of aircraft weapons bay acoustic loads. USP2000086098925.
  2. Tichenor, Clyde L.; Ginsburgh, Irwin. Aircraft fuel tank ullage safety system. USP2004036698692.
  3. Gerard, Ludovic; Gutiérrez García, Alejandro; Maldonado, Julián. Aircraft landing gear. USP2016029248905.
  4. Dittrich,Kay. Cellular actuator device and methods of making and using same. USP2006067055782.
  5. Abdel-Baset, Tarek. Conformable high pressure gaseous fuel storage system having a gas storage vessel with fractal geometry. USP2016069366203.
  6. Wille Robert Henry. Conformable weapons platform. USP1999115988567.
  7. Henderson, Trent N.; Toal, Christopher E.. External-bladder fuel system fluidly connectable to a fuel tank to receive excess. USP2018039919807.
  8. Edlund,David J.; Studebaker,R. Todd. Feedstock delivery systems, fuel processing systems, and hydrogen generation assemblies including the same. USP2008127470293.
  9. Burgess, Calvin. Fuel range for an aircraft. USP2013028376281.
  10. Burgess, Calvin. Fuel range for an aircraft. USP2012058172181.
  11. Robert H. Thompson ; Michael Joseph Harrigan, Sr. ; Michael William Soltis. Fuel system. USP2002076412476.
  12. Gallegos David Paul. Hybrid fuel containment structure. USP2000066076769.
  13. Gallegos David Paul. Hybrid fuel containment structure. USP2001016176452.
  14. John S. Mayes. Protective enclosure with peripheral fluid storage facility. USP2002066398165.
  15. Tweet, Tracy L; Shelly, Mark A. Sealing bladderless system and method. USP2013088505761.
  16. Conway, Jr., George Louis; Young, Kendall G.; Stroud, Ron L.. Single aperture conformal aircraft bays. USP2003036536711.
  17. Bofill, Steven. Sleeve and rod support for fuel bladder. USP2015069050691.
  18. Kahara Bryan D. ; Priestley Richard T. ; Seho Kenneth E.. Variable displacement fuel tank for aircraft. USP1999115975466.