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특허 상세정보

Variable geometry nacelle assembly for a gas turbine engine

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02K-003/02   
미국특허분류(USC) 060/226.1; 137/015.1; 244/053B
출원번호 US-0749260 (2007-05-16)
등록번호 US-8205430 (2012-06-26)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Carlson, Gaskey & Olds PC
인용정보 피인용 횟수 : 1  인용 특허 : 51

A nacelle assembly includes an inlet lip section and a cowl section positioned downstream of the inlet lip section. At least a portion of the cowl section is moveable to influence an effective boundary layer thickness of the nacelle assembly.


1. A nacelle assembly, comprising: an inlet lip section; anda cowl section downstream of said inlet lip section, wherein at least a portion of said cowl section is selectively moveable between a first position and a second position to influence an effective boundary layer thickness of the nacelle assembly, wherein said second position is radially outward from an exterior wall of the nacelle assembly, and wherein a leading edge of said portion of said cowl section is positioned radially outward from and adjacent to a trailing edge of said inlet lip sectio...

이 특허에 인용된 특허 (51)

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