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특허 상세정보

Turbine engine tailcone resonator

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F01N-001/02   
미국특허분류(USC) 181/250; 181/212; 181/213; 181/214
출원번호 UP-0412756 (2006-04-27)
등록번호 US-7552796 (2009-07-09)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Bachman & LaPointe, P.C.
인용정보 피인용 횟수 : 4  인용 특허 : 33

A turbine engine resonator comprising a panel and a vessel. The panel is along a flow path within the engine and has an aperture. The vessel has a mounting flange secured to the panel. The flange has an aperture mated to the aperture of the panel. The vessel has a body secured to the mounting flange with an interior of the body in communication with the flange aperture. A first portion of the panel extends into the mounting flange aperture and may redirect a leakage flow, if any, to limit an effect of leakage upon resonator performance.


What is claimed is 1. A turbine engine resonator comprising: a panel along a flow path within the engine and having an aperture; a resonator vessel having: a mounting flange secured to the panel and having an aperture mated to the aperture of the panel; and a body secured to the mounting flange with an interior of the body in communication with the flange aperture, wherein: a first portion of the panel extends into the mounting flange aperture. 2. The resonator of claim 1 wherein: a gap, open toward the body interior, circumscribes the first portio...

이 특허에 인용된 특허 (33)

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