$\require{mediawiki-texvc}$
  • 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

Gas turbine engine with stacked accessory components

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02C-007/32   
출원번호 US-0413634 (2009-03-30)
등록번호 US-9816441 (2017-11-14)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Carlson, Gaskey & Olds, P.C.
인용정보 피인용 횟수 : 1  인용 특허 : 32
초록

An engine accessory system for a gas turbine engine includes a first accessory component defined along an accessory axis and a second accessory component mounted to the first accessory component along the accessory axis.

대표
청구항

1. An engine accessory system for a gas turbine engine comprising: a nacelle assembly comprising a core nacelle that surrounds a core engine and a fan nacelle that at least partially surrounds said core nacelle;a fan case surrounded by said fan nacelle, said fan case defining a fan case outermost diameter;an intermediate case mounted between said fan case and a high pressure compressor case, said intermediate case defined by an outermost diameter that is less than said fan case outermost diameter at an aft end of said fan case;an accessory gearbox case s...

이 특허에 인용된 특허 (32)

  1. Ciokajlo John J. (Cincinnati OH) O\Brien Michael T. (Cincinnati OH). Air-start assembly and method. USP1994095349814.
  2. Dunbar Donald K. (Sharonville OH) Delaney Bobby R. (Loveland OH). Aircraft bypass turbofan engine thrust reverser. USP1994055315821.
  3. Moulebhar, Djamal. Aircraft with disengageable engine and auxiliary power unit components. USP2010107805947.
  4. Miller,Guy Wallace. Apparatus for driving an accessory gearbox in a gas turbine engine. USP2006067055330.
  5. Pullen Keith R. (London GB2) Horton Kevin J. (Ansley GB2) Etemad Mohammad R. (London GB2) Fenocchi Arnoldo (London GB2) Eggleston Laurence W. (London GB2) Bolton Hugh R. (Epsom GB2). Axial field electrical generator. USP1991065021698.
  6. Rodgers Colin (San Diego CA) Vershure ; Jr. Roy W. (Escondido CA). Combined auxiliary and emergency power unit. USP1989094864812.
  7. Griffin James G. (West Hartford CT) Schwarz Frederick M. (Glastonbury CT). Cooling system for the electrical generator of a turbofan gas turbine engine. USP1984104474001.
  8. Edwards Geoffrey (Rugby GB2) Clarke Michael G. (Dorset GB2). Differential gear assembly. USP1992045103631.
  9. Webster,John R. Drive apparatus. USP2007017160159.
  10. El Hamel,Karim; Newton,Arnold C. Engine arrangement. USP2006097107755.
  11. Hanson, Russell B.. Fan variable area nozzle for a gas turbine engine fan nacelle. USP2010057721551.
  12. Walsh, Philip P.; Fletcher, Paul. Gas turbine engine. USP2005036865891.
  13. Walsh,Philip P.; Fletcher,Paul. Gas turbine engine. USP2006117134269.
  14. Newton Arnold C. (Derby GB2). Gas turbine engine starting. USP1993105253470.
  15. Newton Arnold C.,GB2 ; Sharp John,GB2. Gas turbine engine system. USP1999025867979.
  16. Ryan K. Snyder ; Alexander P. Girgenti ; Keven G. Van Duyn ; Peter C. Tiziani ; Thomas B. Avis ; Antonio J. Portelinha. Gearbox accessory mount. USP2002036357220.
  17. Hill, Jason E; Mountain, Steven J; Mitcham, Alan J. Generator arrangements. USP2004116825640.
  18. Butt, David C; Maguire, Alan R. Generator assembly. USP2009067543439.
  19. Marnot Paul H. (Cornillon-Confoux FRX). Mechanism for transmitting power between a driving shaft and two assemblies to be driven. USP1993125271295.
  20. Sterka William E. (3446 Anglin Dr. Sarasota FL 34242). Model airplane engine mounting system. USP1994045303896.
  21. Sadil Andreas (Wallingford CT) Sarcich Stephen A. (Vernon CT). Mounting bracket for an aircraft engine accessory. USP1995075435124.
  22. 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.
  23. MacFarlane, Ian Alexander; Szlanta, Zenon; Mitrovic, Lazar; Morgan, Keith Martin. Offset drive for gas turbine engine. USP2004056735954.
  24. Clark Ralph J. (Rochester MI). Oil scavening system for gas turbine engine. USP1985074525995.
  25. Razzell, Anthony G; Care, Ian C D; Cullen, John J A. Shaft bearings. USP2004076765328.
  26. Hield Paul M. (Bristol GB2) Cundy John M. (Derby GB2) Midgley Ronald A. (Derby GB2) Newton Arnold C. (Derby GB2) Rowe Arthur L. (Derby GB2). Shaft power transfer in gas turbine engines with machines operable as generators or motors. USP1997125694765.
  27. Linet, Hugues Henri Raymond; Mouchnino, Cyril Franck; Pettinotti, Serge Dominique. System for driving accessory machines of a double-bodied turbine engine. USP2010047690185.
  28. Cornax Dennis (Chula Vista CA). Torque link fan jet engine support for reducing engine bending. USP1993075226288.
  29. Rolt,Andrew M. Turbofan arrangement. USP2006097107756.
  30. Beutin,Bruno; Yvon,Didier; Mazeaud,Georges; Burdin,Fabien. Turbojet designed to be fixed onto the AFT part of the fuselage of an aircraft, in upper position. USP2006037007890.
  31. Bart, Jacques Rene; Beutin, Bruno Albert; Morel, Patrick Charles Georges. Twin spool turbine engine with power take-off means on the low-pressure and high-pressure rotors, and power take-off module for the turbine engine. USP2009067552591.
  32. Duesler Paul W. (Manchester CT) Loso Wendell R. (Manchester CT). Utility conduit enclosure for turbine engine. USP1992125174110.