$\require{mediawiki-texvc}$
  • 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"
쳇봇 이모티콘
안녕하세요!
ScienceON 챗봇입니다.
궁금한 것은 저에게 물어봐주세요.

특허 상세정보

Fuel system for a gas turbine engine

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02C-007/22   
미국특허분류(USC) 060/039.094; 060/039.281; 060/734
출원번호 US-0461205 (2003-06-13)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Reinhart Boerner Van Deuren P.C.
인용정보 피인용 횟수 : 15  인용 특허 : 3
초록

A system for automatically transferring the fuel from one or more engine fuel manifolds directly to the engine fuel tank(s) during engine shutdown using an ejector pump has been presented. A checkvalve, which may be integrated with the ejector pump, is also used. A metering valve initiates fuel flow shutoff and is used in the draining of the fuel manifolds, thereby eliminating the need for an additional solenoid dedicated mainly to the shutoff function. The shutoff and pressurizing valve provides flow division between manifolds and manifold drain for sys...

대표
청구항

What is claimed is: 1. A system for transferring fuel from at least one engine fuel manifold of a gas turbine engine to a fuel tank comprising: a fuel metering and shutoff valve configured to provide high pressure fuel to the at least one engine fuel manifold; a bypass valve in fluid communication with the fuel metering and shutoff valve; an ejector having an inlet port for receiving fuel from the bypass valve during engine operation, an outlet port in fluid communication with one of the fuel tank and a fuel tank ejector, and a suction port, the ejector...

이 특허를 인용한 특허 피인용횟수: 15

  1. Heitz, Steven A.. Aircraft engine fuel system. USP2015038991152.
  2. Delaloye, Jim E.. Airframe mounted electric motor driven lubrication pump control deoil system. USP2011017871248.
  3. Futa, Paul; Tuttle, David; Lawrence, David. Flow equalizing override assembly for fuel divider system. USP2012118316630.
  4. Baker, Carthel C.; Voskuil, Terence J.. Flow sensing shutoff valve. USP2012068192172.
  5. Dore, Bastien; Pora, Loïc. Fuel feed device for aviation engine. USP2015038991148.
  6. Van Alen, Frederick Ehrwulf. Fuel manifold cooling flow recirculation. USP2018059957891.
  7. Bickley,Daniel James. Fuel system. USP2008037337761.
  8. Heitz, Steven A.. Fuel system. USP2015099133772.
  9. Smith, David R.; Burg, Joe James; Rogstad, Robert R.. Offset ambient level fuel feed system. USP2014118881764.
  10. Nyzen, Robert; Clements, Martin A.. Pressure compensation control of a fixed displacement pump in a pumping and metering system and associated method. USP20180810041497.
  11. Van Der Ploeg, Govert Gerardus Pieter. Process to provide a particulate solid material to a pressurised reactor. USP2015109149779.
  12. Snodgrass, Brett J.; Schaefer, Paul J.; Lawver, Brian K.. Regulator flow damping. USP2016099435311.
  13. Kleckler, Joel W.. System for metering a fuel supply. USP2011067966994.
  14. Mailander, William James; Goodwin, Paul Bryant. Thermoelectrically cooled components for distributed electronics control system for gas turbine engines. USP2010087779811.
  15. Goguet-Chapuis, Benjamin Andre; Bregani, Benjamin. Valve for fuel circuit of an aircraft engine. USP2016089428278.