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특허 상세정보

Integrated thermal anti-icing and environmental control system

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64D-015/02    B64D-013/08   
미국특허분류(USC) 244/134R ; 60/3909 ; D ; 165/42 ; 244/53B
출원번호 US-0535928 (1974-12-23)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 50  인용 특허 : 0

An integrated thermal anti-icing and environmental control system for a gas turbine powered aircraft uses hot high pressure bleed air from the turbine compressor to de-ice the wings and the engine air inlet, and supplies conditioned air for the aircraft cabin. In order to minimize total bleed air requirements and maximize heat recovery, bleed air exhausted from the inlet anti-icing system is passed sequentially through other systems. In this invention, the usual pre-cooler unit and the associated heat sink are eliminated and the pre-cooling function is p...


An integrated thermal anti-icing and environmental control system for use on aircraft having a wing, a passenger cabin, a gas turbine powerplant, an inlet supplying air to the powerplant and an acoustic ring mounted with said inlet comprising: a source of hot, compressed air; first means connected to the source for distributing a portion of the air within the wing for anti-icing purposes; second means connected to said source for distributing a second portion of the air within the inlet for anti-icing purposes and for cooling that portion of the air to a...

이 특허를 인용한 특허 피인용횟수: 50

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