$\require{mediawiki-texvc}$

연합인증

연합인증 가입 기관의 연구자들은 소속기관의 인증정보(ID와 암호)를 이용해 다른 대학, 연구기관, 서비스 공급자의 다양한 온라인 자원과 연구 데이터를 이용할 수 있습니다.

이는 여행자가 자국에서 발행 받은 여권으로 세계 각국을 자유롭게 여행할 수 있는 것과 같습니다.

연합인증으로 이용이 가능한 서비스는 NTIS, DataON, Edison, Kafe, Webinar 등이 있습니다.

한번의 인증절차만으로 연합인증 가입 서비스에 추가 로그인 없이 이용이 가능합니다.

다만, 연합인증을 위해서는 최초 1회만 인증 절차가 필요합니다. (회원이 아닐 경우 회원 가입이 필요합니다.)

연합인증 절차는 다음과 같습니다.

최초이용시에는
ScienceON에 로그인 → 연합인증 서비스 접속 → 로그인 (본인 확인 또는 회원가입) → 서비스 이용

그 이후에는
ScienceON 로그인 → 연합인증 서비스 접속 → 서비스 이용

연합인증을 활용하시면 KISTI가 제공하는 다양한 서비스를 편리하게 이용하실 수 있습니다.

Variable area bypass injector 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F02K-003/02
출원번호 US-0098994 (1993-07-29)
발명자 / 주소
  • Johnson Kenneth L. (Cincinnati OH) Corsmeier Donald M. (Cincinnati OH) Weaver William L. (West Chester OH) Lewis Eric H. (Loveland OH)
출원인 / 주소
  • General Electric Company (Cincinnati OH 02)
인용정보 피인용 횟수 : 32  인용 특허 : 0

초록

A variable area bypass injector (VABI) for a variable cycle gas turbine engine includes a circumferentially continuous valve with a conical surface sloping into a screech suppressor surface, a circumferentially segmented seal attached to the diffuser, and a valve actuator located outside the outer d

대표청구항

A variable area bypass injector (VABI) for a variable cycle gas turbine engine having a longitudinal axis, an inner casing defining a core gas flow, and an outer casing spaced from said inner casing defining a bypass duct for supplying a bypass air flow, said VABI comprising: a VABI valve comprising

이 특허를 인용한 특허 (32)

  1. Rudolph Peter K. C., Aircraft chute ejector nozzle.
  2. Lidstone Gary L. ; Sandquist David L. ; Clark Larry T. ; Szupkay Imre A., Aircraft engine ejector nozzle.
  3. Rudolph Peter K. C., Aircraft turbofan engine mixing apparatus.
  4. Koshoffer,John Michael, Augmenter swirler pilot.
  5. Philippona Derk S., Bypass air valve for a gas turbine.
  6. Narcus Andrew R. ; Hayes Douglas A. ; Auxier Thomas A., Bypass air valve for a gas turbine engine.
  7. Stewart Jeffrey B. (Palm Beach Gardens FL) Minick Alan B. (Stuart FL), Bypass air valve for turbofan engine.
  8. McCracken, Ivan Andrew; Slenes, Chad Johan; Rogers, Tony; Close, Shawn Michael; Weaver, William Bruce; Freitag, Chad David, Check valve unit for solid ink reservoir system.
  9. McCracken, Ivan Andrew; Slenes, Chad Johan; Rogers, Tony; Close, Shawn Michael; Weaver, William Bruce; Freitag, Chad David, Check valve unit for solid ink reservoir system.
  10. Smith, J. Walter, Controlled fan stream flow bypass.
  11. Bachman, Frank Gerald; Lewis, Randy Lee; Bockwich, Robert Steven; Bunnag, Shane, Ejector purge of cavity adjacent exhaust flowpath.
  12. Lidstone Gary L. ; Clark Larry T. ; Szupkay Imre A. ; Sandquist David L., Engine noise suppression ejector nozzle.
  13. Danescu, Radu Ioan; Johnson, David Martin, Helical seal system for a turbomachine.
  14. Ruthemeyer, Michael Anthony, Integrated variable geometry flow restrictor and heat exchanger.
  15. Sadil, Andreas; Muldoon, Marc J.; Jlidi, Bessem, Leaf spring damper for a turbine engine fuel delivery system.
  16. Corsmeier, Donald Michael; Perveiler, David Andrew; Johnson, George Joseph, Method and apparatus for regulating fluid flow through a turbine engine.
  17. Lidstone Gary L. ; Clark Larry T. ; Szupkay Imre A. ; Sandquist David L., Stowable mixer ejection nozzle.
  18. Lovett, Jeffery A.; Philippona, Derk S., Systems and methods involving reduced thermo-acoustic coupling of gas turbine engine augmentors.
  19. Park, Roger James, Turbine engine fuel injector with helmholtz resonators.
  20. Corsmeier, Donald Michael; Dawson, David Lynn, Turbine engine valve assembly and method of assembling the same.
  21. Giffin ; III Rollin G. ; Johnson James E. ; Crall David W. ; Salvage John W. ; Szucs Peter N., Turbofan engine with a core driven supercharged bypass duct.
  22. Kasibhotla, Ravi Shankar Venkata; Adis, William Edward; Anjuri, Venkata Siva Jagadeeswararao; Bhagavatheeswaran, Anantha Padmanabhan, Turbomachine seal assembly.
  23. Corsmeier, Donald Michael, Valve assembly for a gas turbine engine.
  24. Corsmeier,Donald Michael, Valve assembly for a gas turbine engine.
  25. Ostebee, Heath Michael; Ziminsky, Willy Steve; Johnson, Thomas Edward; Keener, Christopher Paul, Variable volume combustor.
  26. Johnson, Thomas Edward; McConnaughhay, Johnie Franklin; Keener, Chrisophter Paul; Ostebee, Heath Michael, Variable volume combustor with a conical liner support.
  27. McConnaughhay, Johnie Franklin; Keener, Christopher Paul; Johnson, Thomas Edward; Ostebee, Heath Michael, Variable volume combustor with aerodynamic fuel flanges for nozzle mounting.
  28. Ostebee, Heath Michael; Johnson, Thomas Edward; Stewart, Jason Thurman; Keener, Christopher Paul, Variable volume combustor with aerodynamic support struts.
  29. Johnson, Thomas Edward; Ziminsky, Willy Steve; Ostebee, Heath Michael; Keener, Christopher Paul, Variable volume combustor with an air bypass system.
  30. Ostebee, Heath Michael; McConnaughhay, Johnie Franklin; Stewart, Jason Thurman; Keener, Christopher Paul, Variable volume combustor with center hub fuel staging.
  31. McConnaughhay, Johnie Franklin; Keener, Christopher Paul; Johnson, Thomas Edward; Ostebee, Heath Michael, Variable volume combustor with nested fuel manifold system.
  32. Keener, Christopher Paul; Johnson, Thomas Edward; McConnaughhay, Johnie Franklin; Ostebee, Heath Michael, Variable volume combustor with pre-nozzle fuel injection system.
섹션별 컨텐츠 바로가기

AI-Helper ※ AI-Helper는 오픈소스 모델을 사용합니다.

AI-Helper 아이콘
AI-Helper
안녕하세요, AI-Helper입니다. 좌측 "선택된 텍스트"에서 텍스트를 선택하여 요약, 번역, 용어설명을 실행하세요.
※ AI-Helper는 부적절한 답변을 할 수 있습니다.

선택된 텍스트

맨위로