$\require{mediawiki-texvc}$
  • 검색어에 아래의 연산자를 사용하시면 더 정확한 검색결과를 얻을 수 있습니다.
  • 검색연산자
검색연산자 기능 검색시 예
() 우선순위가 가장 높은 연산자 예1) (나노 (기계 | machine))
공백 두 개의 검색어(식)을 모두 포함하고 있는 문서 검색 예1) (나노 기계)
예2) 나노 장영실
| 두 개의 검색어(식) 중 하나 이상 포함하고 있는 문서 검색 예1) (줄기세포 | 면역)
예2) 줄기세포 | 장영실
! NOT 이후에 있는 검색어가 포함된 문서는 제외 예1) (황금 !백금)
예2) !image
* 검색어의 *란에 0개 이상의 임의의 문자가 포함된 문서 검색 예) semi*
"" 따옴표 내의 구문과 완전히 일치하는 문서만 검색 예) "Transform and Quantization"

특허 상세정보

Assembly for mounting a turbine engine to a pylon

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64D-027/10    B64D-027/26    F02C-007/20    F02K-003/06   
미국특허분류(USC) 244/054; 248/554; 248/555; 060/796; 060/797
출원번호 US-0601395 (2012-08-31)
등록번호 US-8985509 (2015-03-24)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    O'Shea Getz P.C.
인용정보 피인용 횟수 : 3  인용 특허 : 17
초록

An assembly for mounting a turbine engine to a pylon includes a mounting beam, a plurality of fasteners, a first mounting linkage and a second mounting linkage. The mounting beam includes a mount beam fitting that extends axially between a first mount beam end and a second mount beam end, and a mount beam flange that extends radially out from the mount beam fitting at the first mount beam end. A first fastener aperture extends radially through the mount beam fitting, and a second fastener aperture extends axially through the mount beam flange. The fasten...

대표
청구항

1. An assembly for mounting a turbine engine to a pylon, the turbine engine comprising a first engine attachment arranged circumferentially between a plurality of second engine attachments, the assembly comprising: a mounting beam comprising a mount beam fitting that extends axially between a first mount beam end and a second mount beam end, and a mount beam flange that extends radially out from the mount beam fitting at the first mount beam end, wherein a first fastener aperture extends radially through the mount beam fitting, and a second fastener aper...

이 특허에 인용된 특허 (17)

  1. Seelen Laurence (Cincinnati OH) Joseph Thomas P. (West Chester OH) Spofford Hahn M. (West Chester OH) Orkiszewski Charles S. (Cincinnati OH). Aircraft engine forward mount. USP1994015277382.
  2. Mangeiga John A. ; Wilusz Christopher J. ; Dykhuizen Cornelius H.. Aircraft engine mount. USP2001126330995.
  3. Manteiga, John Alan; Wilusz, Christopher James; Dykhuizen, Cornelius Harm. Aircraft engine mount with single thrust link. USP2003086607165.
  4. Spofford, Hahn M.; Wakeman, Thomas G.; Bellia, Donald L.; Joseph, Thomas P.; Wilson, Gregg H.; Cencula, James E.; Tegarden, Frederick W.; Schneider, Michael H.. Aircraft engine thrust mount. USP1994065320307.
  5. Le Blaye Sebastien,FRX. Attachment device for an aircraft engine. USP2001016173919.
  6. Balk, Wouter. Attachment of a multiflow turbojet engine to an aircraft. USP2012078215580.
  7. Greenberg Paul B. (Manchester CT) Lenkeit C. Heinz (South Windsor CT) Seibert Willard J. (Manchester CT). Case deflection control in aircraft gas turbine engines. USP1984014428189.
  8. Pascal Jule FR; Alain Porte FR; Stephane Levert FR. Device for attaching an aircraft engine to a strut. USP2002026347765.
  9. Suciu, Gabriel L.; Merry, Brian D.; Dye, Christopher M.; Johnson, Steven B.. Engine mount system for a turbofan gas turbine engine. USP2012038128021.
  10. Foster, Lawrence David. Engine mounting apparatus. USP2011128074923.
  11. Manteiga, John Alan; Wilusz, Christopher James; Dykhuizen, Cornelius Harm. Fail-safe aircraft engine mounting system. USP2005016843449.
  12. Prario Aldo (Wethersfield CT). Gas turbine engine assembly. USP1987084687413.
  13. Lafont, Laurent; Journade, Frederic. Mounting assembly for securing an engine to an aircraft wing. USP2010097797947.
  14. Suciu, Gabriel L.; Merry, Brian D.; Franklin, David W. J.; Dye, Christopher M.. Mounting system for a gas turbine engine. USP2012058167237.
  15. Brodell Robert F. (Marlborough CT) Hovan Edward J. (Manchester CT) Selfors Steven T. (Somerville MA) Loffredo Constantino V. (Newington CT) Duesler Paul W. (Manchester CT). Nacelle and mounting arrangement for an aircraft engine. USP1996065524847.
  16. Demouzon Francis Michel,FRX ; Fer Rene Pierre,FRX ; Huet Patrick Jean Alibert,FRX ; Marnas Laurent Pierre Elysee Gaston,FRX. Redundant front suspension system for a turboshaft engine. USP1999025871177.
  17. Chouard, Pierre-Alain Jean-Marie Philippe Hugues; Lefort, Guillaume. Suspension for mounting a turbojet engine on an aircraft. USP2012018104708.