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Infrared radiation suppressor for gas turbine engine 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F02C-007/18
  • F02C-007/24
출원번호 US-0596593 (1975-07-17)
발명자 / 주소
  • Hurley John F. (Huntington CT)
출원인 / 주소
  • Avco Corporation (Stratford CT 02)
인용정보 피인용 횟수 : 95  인용 특허 : 0

초록 ▼

Apparatus for suppressing infrared radiation emitted from hot metal parts at the aft end of a gas turbine engine and from the exhaust gas plume thereof is provided and such apparatus employs components which utilize an ejector principle to provide cooling action utilizing ambient air and such compon

대표청구항 ▼

An apparatus for suppressing infrared radiation emitted from hot metal parts at the aft end of a gas turbine engine and from the exhaust gas plume thereof during engine operation comprising a dogleg duct and means supporting said duct adjacent said engine to receive its exhaust gases, said duct comp

이 특허를 인용한 특허 (95)

  1. Brunetti, Massimo; Cogliati, Andrea; Iannucci, Dario; Scandroglio, Alessandro, Aircraft capable of hovering having an exhaust duct with thermoelectric conversion circuit.
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  3. Hurley John F. (Easton CT), Apparatus for and method of suppressing infrared radiation emitted from gas turbine engine.
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  4. Gustafsson, Bernhard, Arrangement for propelling an aircraft, aircraft and outlet nozzle for a jet engine.
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  7. Durand, Yves, Device for reducing turboprop infrared emissions.
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