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특허 상세정보

Cooling system for high speed aircraft

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64D-037/34    B64C-001/40   
미국특허분류(USC) 244/117A ; 60/730 ; 60/267 ; 60/259
출원번호 US-0008210 (1979-01-31)
발명자 / 주소
인용정보 피인용 횟수 : 19  인용 특허 : 0
초록

The invention is for a system which provides total cooling for an aircraft airframe which is designed to fly in the speed range of Mach 2 to Mach 8. The system eliminates the necessity of shielding an aircraft airframe constructed of material such as aluminum. Cooling is accomplished by passing a coolant through the aircraft airframe, the coolant acting as a carrier to remove heat from the airframe. The coolant is circulated through a heat pump and a heat exchanger which together extract essentially all of the added heat from the coolant. The heat is tra...

대표
청구항

A cooling system for a high speed aircraft comprising: an aircraft; fuel means carried by said aircraft; said aircraft having airframe cooling means; heat pump means comprising evaporator and condenser means for receiving coolant medium from within said airframe cooling means and extracting heat therefrom in said evaporator means; heat exchanger means for receiving fuel from said fuel means and receiving said coolant medium from said evaporator means and transferring heat from said coolant medium to said fuel said condenser means receiving fuel from said...

이 특허를 인용한 특허 피인용횟수: 19

  1. Kim Kyusik (5026 Rhoads Ave. Santa Barbara CA 93111). Aerodynamic heated steam generating apparatus. USP1986084605184.
  2. Lu, Qiao; Godecker, William. Aircraft galley liquid cooling system. USP2015119188380.
  3. Weber, Richard M.. Aircraft thermal management system for cooling using expendable coolants. USP2017029561857.
  4. Mhadeshwar, Ashish B.; Norton, Daniel; Perry, Robert James; Glaser, Paul; Pastecki, Patrick Edward. Catalytic alcohol dehydrogenation heat sink for mobile application. USP2015028961891.
  5. Brewer George D. (San Marcos CA) Marshall David P. (Powder Springs GA). Combination boundary layer control system for high altitude aircraft. USP1989024807831.
  6. Stromath David K. (Redondo Beach CA) Wiler Curtiss D. (Palos Verdes CA). Cooling structure. USP1991014986495.
  7. Veilleux, Jr., Leo J.. Cooling system for electronic device in a gas turbine engine system. USP2013048424285.
  8. Jones, Alan R.. Cooling systems. USP2005086931834.
  9. Vaisman, Igor. Cooling systems for high mach applications. USP2017089739200.
  10. Uken Arthur H. (Brigham City UT). Energy efficient solid propellant attitude control system. USP1988114786019.
  11. Ho, Yuhang. Environmental control system for an aircraft. USP2005096948331.
  12. Niggemann Richard E. (Rockford IL). Heat management system for spacecraft. USP1986084603732.
  13. Michel Engelhardt. Heat pipe cooling of aircraft skins for infrared radiation matching. USP2002086435454.
  14. Norton, Daniel G.; Perry, Robert J.. High capacity heat sink. USP2013078496201.
  15. Bulin, Guillaume; Dittmar, Jan. Method for controlling thermal effluents generated by an aircraft and cooling device for an aircraft implementing said method. USP2014038677755.
  16. Lutzer Wilhelm,DEX. System for removing incident heat from aircraft during flight. USP1998085794888.
  17. Smith, J. Walter. Systems and methods for thermal management in a gas turbine powerplant. USP2013098534044.
  18. Smith, J. Walter. Systems and methods for thermal management in a gas turbine powerplant. USP2011077984606.
  19. Niggemann Richard E. ; Nguyen Dam. Thermal and energy management method and apparatus for an aircraft. USP2001026182435.