$\require{mediawiki-texvc}$
  • 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 combustor assembly

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02C-007/042   
미국특허분류(USC) 60/3923 ; 60/3927 ; 60/3929 ; 60/737
출원번호 US-0279960 (1981-07-02)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 14  인용 특허 : 2
초록

An improved gas turbine engine combustor assembly particularly for automotive application including a primary reaction chamber disposed in a pressurized air plenum of the engine, fixed area air flow ports between the reaction chamber and the plenum, a prechamber housing at an upstream end of the reaction chamber having an annular fixed area air passage between the plenum and the reaction chamber, a radially expandable annular partition in the air passage dividing the latter into an inner annular prechamber portion and an outer annular excess air portion,...

대표
청구항

In a gas turbine engine having a pressurized air plenum and a combustor assembly disposed in said plenum including wall means having a plurality of fixed flow area ports between said plenum and a reaction chamber defined by said wall means, the combination comprising means on said combustor assembly defining at an upstream end thereof an annular air passage between said plenum and said reaction chamber having a plurality of generally radially extending swirl inducing vanes therein, a radially adjustable cylindrical partition disposed in said air passage ...

이 특허를 인용한 특허 피인용횟수: 14

  1. Subramanian, Karthik; Romig, Bryan Wesley. Apparatus and method for a fuel nozzle. USP2014128919673.
  2. Kuhn, Terrel E.; Freeman, William G.; Maszk, Francis S.; Freiberg, Douglas P.; Struzek, Kenneth A.; Kobold, Lawrence A.. Apparatus and method for controlling combustor liner carbon formation. USP2005036868675.
  3. Snyder Timothy S. ; Sowa William A. ; Morford Stephen A. ; Van Dyke Kevin J.. Bluff body premixing fuel injector and method for premixing fuel and air. USP2001016176087.
  4. Stratton John F. (Accrington GB2). Combustion equipment. USP1987094689961.
  5. Sandoval, Jonathan P.; Smith, Randolph J.. Conjoined grommet assembly for a combustor. USP2017119810430.
  6. Stoia, Lucas John; DeForest, Russell Pierson; Melton, Patrick Benedict. Flowsleeve of a turbomachine component. USP2015099140455.
  7. Shimizu Nobuo (Hitachi JPX) Kuroda Michio (Hitachi JPX) Kirikami Seiichi (Hitachi JPX) Sato Isao (Hitachi JPX) Arai Osamu (Hitachi JPX). Fuel-air premixing device for a gas turbine. USP1991055016443.
  8. Guo, Cliff Yi; Stevenson, John Saunders; Davis, Dustin Wayne; Avagliano, Aaron John. Methods and systems for mixing reactor feed. USP2013058434700.
  9. Dean Anthony John ; Goebel Steven George. Mixer having intervane fuel injection. USP2001106301899.
  10. Snyder, Timothy S.; Sowa, William A.; Morford, Stephen A.; Van Dyke, Kevin J.. Premixing fuel and air. USP2003026513329.
  11. Ohmori Takashi (Hitachi JPX) Sato Isao (Hitachi JPX) Ishibashi Yoji (Hitachi JPX) Minakawa Yoshimitsu (Hitachi JPX) Kuroda Michio (Hitachi JPX) Tamura Zensuke (Hitachi JPX). Premixing swirling burner. USP1986054587809.
  12. Tyler, Peter Michael. Testing of a transient voltage protection device. USP2016089411016.
  13. Coughlan Joseph D. ; Goetschius Alan J.. Thermally decoupled swirler for a gas turbine combustor. USP1999125996352.
  14. Greene Walter (South Windsor CT) Liebke William R. (Vernon CT). Variable area inlet guide vanes. USP1986084606190.