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특허 상세정보

Turbojet equipped with a deicing system on the intake case

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02C-007/047   
미국특허분류(USC) 60/39093 ; 415/175 ; 219/679 ; 244/134 ; D
출원번호 US-0509054 (1995-07-31)
우선권정보 FR-0010102 (1994-08-18)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 18  인용 특허 : 4
초록

A turbojet having an air intake case including radial arms between an outer annular structure and an inner central structure, and a deicing unit configured to deice the radial arms by microwaves and located in the central structure. The deicing unit has a microwave generator and a transmitting element configured to transmit energy and including an inside annular waveguide located inside of the central structure. An energy distributing element configured to eliminate ice is coupled with the transmitting element by a coupling element. The radial arms are m...

대표
청구항

A turbojet comprising: an air intake case having radial arms between an outer annular structure and an inner central structure, said radial arms being made from a dielectric composite material; a deicing unit configured to deice said radial arms by microwaves and located in said central structure, said deicing unit having a microwave generator and a transmitting element configured to transmit energy supplied by said microwave generator, said transmitting element comprising an inside annular waveguide located inside of said central structure; an energy di...

이 특허를 인용한 특허 피인용횟수: 18

  1. Raad, Bernard A.. Air gap deicing device. USP2003076593547.
  2. Porte, Alain; Fargues, Matthieu; Marro, Martial. Aircraft nacelle comprising a reinforced connection between an air intake and a powerplant. USP2017029567905.
  3. Francisco, Jay M.; Napier, James C.. Arrangement for maintaining flow to an air inlet of an auxiliary power unit assembly. USP2014058733694.
  4. Davis, Brian Michael; Wood, Billy T.; Reimels, Gregory William; Lorenzi, Louis Bruno. Bushing and clock spring assembly for moveable turbine vane. USP2012068197196.
  5. Feher, Lambert. Compact microwave system for de-icing and for preventing icing of the outer surfaces of hollow or shell structures which are exposed to meterological influences. USP2003086610969.
  6. Feher, Lambert. Compact millimeterwave system for De-icing and for preventing the formation of ice on the outer surfaces of shell structures exposed to meterological influences. USP2003116642490.
  7. Haehner, Edgar; Royer, Eric. Device for de-icing the air intake of a gas turbine. USP2013088499540.
  8. Euvino, Jr., Frank J.; Vinciquerra, Anthony J.. Electrothermal inlet ice protection system. USP2013028366047.
  9. Lockwood, Clive. Engine arrangement. USP2011098011172.
  10. Chaney, Tina H.; Dischinger, Dave G.; Tiltman, Alan G.; Vettel, Dwight D.. Gas turbine engine anti-ice formation device and system. USP2011017874137.
  11. Jensen, Joseph M.; Bolla, James D.; Humphrey, Joseph T.; Nguyen, Steve H.. Heated engine nose cone using spiral channels. USP2012078210825.
  12. Eccles, Steven R.; Schindler, Wayne G.. Heating device and method for deployable ram air turbine. USP2003016503056.
  13. Thompson,Robert G.. Inlet muff anti-icing system for an auxiliary power unit. USP2006117137240.
  14. Nunnally William C.. Onboard aircraft de-icing using lasers. USP2001036206325.
  15. Davis, Brian Michael; Wood, Billy T.; Huber, Kent Gerhard; Lorenzi, Louis Bruno. Slipring bushing assembly for moveable turbine vane. USP2011118061975.
  16. Zhang, Hua; Zhang, Jianmin. System for ice and/or frost prevention using guided wave energy. USP2013088505273.
  17. Kulczyk, Wojciech Konrad. Temperature sensor and method for measuring temperature. USP2012048157440.
  18. Wolford, Robert Lee. Thermal system for a working member of a power plant. USP2012088246291.