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특허 상세정보

Deployable segmented exhaust nozzle for a jet engine

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02K-001/10    F02K-001/06   
미국특허분류(USC) 060/204; 060/264; 060/262; 181/220; 239/265.19
출원번호 US-0157681 (2002-05-29)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Harness Dickey & Pierce P.L.C.
인용정보 피인용 횟수 : 56  인용 특허 : 6
초록

An exhaust flow nozzle for a jet engine having a plurality of flow altering components extending from a lip portion of a secondary exhaust nozzle that are movable between first and second positions. In the first position the flow altering components are disposed substantially parallel to an exhaust gas flow path and thereby do not produce drag or a reduction of thrust from the engine. In the second position the flow altering components bend or are deformed to project into the exhaust gas flow path exiting from the secondary exhaust nozzle. The flow alter...

대표
청구항

An exhaust flow nozzle for a jet engine having a plurality of flow altering components extending from a lip portion of a secondary exhaust nozzle that are movable between first and second positions. In the first position the flow altering components are disposed substantially parallel to an exhaust gas flow path and thereby do not produce drag or a reduction of thrust from the engine. In the second position the flow altering components bend or are deformed to project into the exhaust gas flow path exiting from the secondary exhaust nozzle. The flow alter...

이 특허를 인용한 특허 피인용횟수: 56

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