$\require{mediawiki-texvc}$
  • 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

Method for selectively switching motive fluid supply to an aft turbine of a multicycle engine

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02K-003/06    F02K-003/12   
미국특허분류(USC) 60/204 ; 60/39.17 ; 60/261 ; 60/262
출원번호 US-0709059 (1976-07-27)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Donahue, Bernard A.Savage, Laurence A.
인용정보 피인용 횟수 : 24  인용 특허 : 0
초록

Air breathing gas turbine engine design concepts, and methods and apparatus for providing variable engine cycles are disclosed. The preferred engine embodiments involve two flow control valve systems for internal management of air, each of which have the capacity to cross-over or invert adjacent annular flow patterns, and at least one of which is capable of switching from inverted to straight through flow.

대표청구항이 없습니다

이 특허를 인용한 특허 피인용횟수: 24

  1. Zsurka, Mark. Aerodynamic track fairing for a gas turbine engine fan nacelle. USP20190310240561.
  2. Neitzel Robert E. (Marblehead MA). Convertible aircraft engine. USP1988124791783.
  3. Goebel, Steven G.; Burch, Steven D.; Migliore, Thomas P.. Flow translocator. USP2003096615872.
  4. Hanlon, Christopher J.; Kupratis, Daniel B.; Ledwith, Walter A.. Gas turbine engine with a multi-spool driven fan. USP20181110119477.
  5. Cesar Aguilera Montoya. Gas turbine engine with increased fuel efficiency and method for accomplishing the same. USP2002056385959.
  6. Zamora, Sean P.; Murphy, Michael Joseph. Gas turbine engine with variable area fan nozzle. USP2012038141366.
  7. Christopherson, Charles Kammer. Gas turbine engine with variable pressure ratio fan system. USP2005066901739.
  8. Schwarz, Frederick M.; Hasel, Karl L.. Geared turbofan engine with high compressor exit temperature. USP20180710036316.
  9. Schwarz, Frederick M.; Hasel, Karl L.. Geared turbofan engine with high compressor exit temperature. USP20181110119466.
  10. Paulino, Joseph R. High bypass turbofan. USP2012098256202.
  11. Klees Garry W. (Mercer Island WA) Wright Charles P. (Seattle WA). Internally ventilated noise suppressor with large plug nozzle. USP1985024501393.
  12. Klees Garry W. (Mercer Island WA). Jet engine and method of operating the same. USP1981124306412.
  13. Wallace ; Jr. Frank B. (Fairfield OH). Jet propulsion apparatus and methods. USP1985074527388.
  14. Davis, Jr., Lewis Berkley; Kulkarni, Parag Prakash; Reed, Robert Joseph. Power generation system exhaust cooling. USP2018049938874.
  15. Kulkarni, Parag Prakash; Davis, Jr., Lewis Berkley; Reed, Robert Joseph. Power generation system exhaust cooling. USP20190210215070.
  16. Kulkarni, Parag Prakash; Davis, Jr., Lewis Berkley; Reed, Robert Joseph; Smith, Raub Warfield. Power generation system exhaust cooling. USP20181010087801.
  17. Reed, Robert Joseph; Davis, Jr., Lewis Berkley; Kulkarni, Parag Prakash. Power generation system exhaust cooling. USP20180710030558.
  18. Reed, Robert Joseph; Davis, Jr., Lewis Berkley; Kulkarni, Parag Prakash. Power generation system exhaust cooling. USP20180810060316.
  19. Dinu, Constantin. Re-heat combustor for a gas turbine engine. USP2011088006477.
  20. Singh, Kapil Kumar; Mohamed, Sherif Hatem Abdulla. System and method for improving efficiency of a gas turbine engine. USP2017019534541.
  21. Bartos James W.. Turbofan engine with a low pressure turbine driven supercharger in a bypass duct operated by a fuel rich combustor and a. USP1999025867980.
  22. Ruberte Sanchez, Jose E.. Turbomachine bypass flow diverting assembly and method. USP20190110190506.
  23. Klees Gary W. (Mercer Island WA) Johnson Paul E. (Mercer Island WA). Turboprop engine and method of operating the same. USP1986024569199.
  24. Schwark, Jr., Fred W.; Atassi, Oliver V.; Owen, William D.. Variable area fan nozzle bearing track. USP2013058443586.