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특허 상세정보

Aircraft anti-icing plenum

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64D-015/04   
미국특허분류(USC) 244/134B ; 60/3909 ; D ; 244/42CC
출원번호 US-0502059 (1974-08-30)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 44  인용 특허 : 0

The leading edge of the jet engine nacelle is provided with structure to prevent the formation of ice particles at the inlet of the jet engine. The nacelle is split into leading and trailing chambers and there is a partition separating the chambers, the leading one of which includes the anti-icing apparatus. The leading chamber includes a double skin generally facing interiorly toward the jet engine and that double skin defines the nacelle therebetween which permits the passage of the hot gases which heat the outer skin from the inside thereof. Conduit m...


Anti-icing plenum to eliminate formation of ice at the leading edge of a jet engine nacelle, the nacelle being divided into leading and trailing chambers, and a partition separating said chambers, a portion of the leading and trailing chambers comprises a double skin along the side thereof generally facing interiorly toward the jet engine, said double skin defining therebetween a cell for the passage of hot gases which heat the leading chamber outer skin from the inside thereof, a series of spaced apertures formed in the inner skin of said leading chambe...

이 특허를 인용한 특허 피인용횟수: 44

  1. Chelin, Frédéric; Surply, Thierry; Bourdeau, Christophe. Air outlet system for aircraft leading edge. USP2013058434724.
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  7. Porte, Alain; Chene, Gilles; Hormiere, Arnaud. Aircraft nacelle including hot air discharge means. USP2013058448901.
  8. Etling, Keith A.. Anti-icing apparatus for honeycomb structures. USP2011118052089.
  9. Tall, Jr., Michael Thomas; Lund, Brian C.; Huang, Jianming. Anti-icing internal manifold. USP2018039920691.
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  12. Haslund Ralph L. (Mercer Island WA). Apparatus and method for providing an aero-optical interface. USP1987114703904.
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  14. Alain Porte FR; Stephane Viala FR. Device for discharging hot air for a jet engine air inlet cowl, with a deicing circuit. USP2002086427434.
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  18. Pollard, Berwyn Owain; Scott, David Russell. Heat exhanger apparatus including heat transfer surfaces. USP2016029260191.
  19. Vest Michael S.. Hot air injection for swirling rotational anti-icing system. USP2001076267328.
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  25. 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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  29. Friddell,Stephen D.; Prichard,Alan K.. Method and apparatus for liquid containment, such as for aircraft fuel vessels. USP2006087090167.
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  31. Hurlin, Herve; Caruel, Pierre. Method of manufacturing a sound absorbing panel. USP2016079390704.
  32. Cook, Donald E.; Feider, Michael P.. Methods and systems for detecting icing conditions. USP2014048711008.
  33. Atassi, Oliver V.. Nacelle with porous surfaces. USP2015038974177.
  34. Porte, Alain; Chelin, Frédéric; Dida, Stéphane; Hormiere, Arnaud. Panel for an air intake of an aircraft nacelle that ensures optimized acoustic treatment and frost treatment. USP2015028960589.
  35. Porte, Alain; Chelin, Frédéric; Albet, Grégory. Panel for the acoustic treatment comprising hot air ducts and at least one annular channel. USP2016059353648.
  36. Porte, Alain; Albet, Grégory; Ring, Guillaume; Galletti, Pascal. Panel for the acoustic treatment comprising hot air ducts and at least one stabilization chamber. USP2016079388767.
  37. Porte, Alain; Pascal, Nathalie; Chene, Gilles; Montetagaud, Fabienne. Process for de-icing an air intake cowling of a reaction motor and device for practicing the same. USP2003076592078.
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  44. Calder, David Patrick. Turbomachine nacelle and anti-icing system and method therefor. USP2013028382039.