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특허 상세정보

Aircraft ice protection system and aircraft provided with the same

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64D-015/02    F01D-025/02    B64D-015/04   
미국특허분류(USC) 244/134B; 244/134R; 244/134C; 239/599; 060/039.09
출원번호 US-0816562 (2011-08-30)
등록번호 US-8967543 (2015-03-03)
우선권정보 JP-2010-192618 (2010-08-30)
국제출원번호 PCT/JP2011/069609 (2011-08-30)
§371/§102 date 20130319 (20130319)
국제공개번호 WO2012/029782 (2012-03-08)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Wenderoth, Lind & Ponack, L.L.P.
인용정보 피인용 횟수 : 2  인용 특허 : 31
초록

An aircraft ice protection system is provided for preventing ice accretion on a wing of an aircraft or removing the accreted ice. Bleed air extracted from a main engine of the aircraft and air introduced from an air intake installed on an airframe and heated by a heat source of the airframe of the aircraft are selectively supplied to a hot air chamber formed inside the wing, thereby carrying out ice protection.

대표
청구항

1. An aircraft ice protection system for preventing ice accretion on a wing of an aircraft or removing the accreted ice, the ice protection system comprising:a hot air chamber which is formed inside the wing of the aircraft;a bleed air supply line which supplies bleed air extracted from a main engine of the aircraft to the hot air chamber;a heated air supply line which supplies air introduced from an air intake of the aircraft to the hot air chamber via a heat source of the aircraft; andswitching device which selectively supplies the bleed air and the ai...

이 특허에 인용된 특허 (31)

  1. Andre, Robert; Porte, Alain. Air inlet cowl for a jet engine, provided with deicing means. USP2003076585191.
  2. Vauchel, Guy Bernard; Beilliard, Stephane. Air intake structure for an aircraft nacelle. USP2014078777164.
  3. Chelin, Frédéric; Surply, Thierry; Bourdeau, Christophe. Air outlet system for aircraft leading edge. USP2013058434724.
  4. Porte, Alain; Hormiere, Arnaud; Dega, Alain. Aircraft nacelle air intake incorporating optimized ice-treatment hot air injection means. USP2014068757547.
  5. Wollaston, Timothy. Aircraft slat assembly with anti-icing system. USP2013118579236.
  6. DuPont, Henry Morgan. Airfoil anti-icing assembly and method. USP2004036702233.
  7. Nieman, Ronald J.; Hughes, Jason M.. Anti-icing piccolo tube standoff. USP2012018100364.
  8. Parente Charles A.. Combined acoustic and anti-ice engine inlet liner. USP1998115841079.
  9. Pike Walter E. ; Shafer Jan C.. Double-walled duct assembly for aircraft anti-icing conduit systems. USP1999126003814.
  10. Gerardi Joseph J. ; Ingram Richard B.. Electro-magnetic expulsion de-icing system. USP2000086102333.
  11. Al-Khalil, Kamel. Energy-efficient electro-thermal and electro-mechanical ice-protection method. USP2010127854412.
  12. Al-Khalil, Kamel. Energy-efficient electro-thermal and electro-mechanical ice-protection method. USP2013048430359.
  13. Porte Alain,FRX. Hot air diffuser for a jet engine air inlet cowl with de-icing circuit. USP2000066079670.
  14. Vest Michael S.. Hot air injection for swirling rotational anti-icing system. USP2001076267328.
  15. Al-Khalil Kamel M. ; Ferguson Thomas F. W.. Hybrid ice protection system for use on roughness-sensitive airfoils. USP2001036196500.
  16. Al-Khalil Kamel M. ; Ferguson Thomas F. W. ; Phillips Dennis M.. Hybrid ice-protection system for use on roughness-sensitive airfoils. USP1999075921502.
  17. Linton, Alan. Ice protection system. USP2005026848656.
  18. Stothers, Ian McGregor. Ice protection system. USP2013128602359.
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  20. Breer, Marlin D.; Olsen, Ronald F.; Kunze, Jr., Robert K.; Riedel, Brian L.. Method and apparatus for aircraft inlet ice protection. USP2004026688558.
  21. Marlin D. Breer ; Ronald F. Olsen ; Robert K. Kunze, Jr. ; Brian L. Riedel. Method and apparatus for aircraft inlet ice protection. USP2002046371411.
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  23. Kawabe Shun,JPX ; Sato Keiichi,JPX ; Yamashita Daiya,JPX ; Nakayama Haruo,JPX ; Shiraishi Koji,JPX ; Matsumoto Keizo,JPX. Method of maufacturing a leading edge structure for aircraft. USP1998095807454.
  24. Birbragher Fernando (Miami FL). Nacelle anti-icing system. USP1988044738416.
  25. Sternberger, Joe E.. Nacelle inlet thermal anti-icing spray duct support system. USP2011037900872.
  26. Radhakrishna Chilukuri. Passive control of hot air injection for swirling rotational type anti-icing system. USP2002036354538.
  27. Rosenthal Herman A. (San Diego CA). Swirl anti-ice system. USP1987084688745.
  28. Rosenthal Herman Allen. Swirl anti-ice system. USP199906RE36215.
  29. Arnold Michael J. (Bangor GB5) Cole Derek (Bangor GB5). Thermal anti-icing of aircraft structures. USP1995035400984.
  30. McLaren Douglas (Seattle WA) Orr William W. (Mercer Island WA). Thermal anti-icing system for aircraft. USP1991045011098.
  31. Gatzke, Sten. Wing-engine combination, an aircraft, and a wing section of an aircraft comprising an engine bleed-air duct arrangement. USP2013018342443.