$\require{mediawiki-texvc}$

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.

Windmill engine starting system with fluid driven motor and pump

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F02C-072/62
출원번호 US-0627809 (1996-04-10)
발명자 / 주소
  • Petrowicz John P.
출원인 / 주소
  • General Electric Company
대리인 / 주소
    Hess
인용정보 피인용 횟수 : 42  인용 특허 : 0

초록

An engine starting system is provided for an aircraft gas turbine engine having a fan, compressor, combustor, high pressure turbine joined to the compressor by a core shaft, and a low pressure turbine joined to the fan by a fan shaft. A fluid assist pump is operatively joined to the fan shaft, and a

대표청구항

[ I claim:] [1.] In an aircraft gas turbine engine having a fan, compressor, combustor, high pressure turbine joined to the compressor by a core shaft, and a low pressure turbine joined to the fan by a fan shaft, an engine starting system comprising:a fluid assist pump operatively joined to said fan

이 특허를 인용한 특허 (42)

  1. Ripley, David Lloyd, Accumulator assisted gas turbine engine start system and methods therefor.
  2. Dooley, Kevin Allan; Savage, William J. K., Apparatus and method for controlling engine windmilling.
  3. Fisher, Robert E., Apparatus, controller and method for controlling the cool down of an aircraft engine rotor.
  4. Dooley, Kevin Allan; Cheng, Audrey; Makuszewski, Jerzy, Combination low spool generator and ram air turbine generator.
  5. Gilbreth Mark G. ; Wall Simon R. ; Wacknov Joel B., Combustion control method and system.
  6. Edelman, Edward C., Command and control system for controlling operational sequencing of multiple turbogenerators using a selected control mode.
  7. Suciu, Gabriel L.; Glahn, Jorn A.; Merry, Brian D.; Dye, Christopher M., Constant-speed pump system for engine thermal management system AOC reduction and environmental control system loss elimination.
  8. Delaloye, Jim; Christopher, Matthew, Electric motor driven lubrication pump control system and method for turbomachine windmill operation.
  9. Bettner, James Lee, Electrical power generation and windmill starting for turbine engine and aircraft.
  10. Franchet, Michel; Hebraud, Guy, Emergency device for relighting a windmilling turbojet.
  11. Derouineau,Jean Luc, Engine power extraction control system.
  12. Kurschat, Ernest; Xiong, Yufei; Haugland, Ron; Thompson, Craig E., Engine systems with enhanced start control schedules.
  13. Denike, Stuart K.; Jira, Joseph J.; McGonigle, Gerald S.; Warriner, Jeremiah J., Flapper with insert stops for check valve.
  14. Dooley, Kevin Allan, Gas turbine engine including apparatus to transfer power between multiple shafts.
  15. Dooley, Kevin Allen, Gas turbine engine including apparatus to transfer power between multiple shafts.
  16. Wehmeier, Eric J., Gas turbine engine with variable area fan nozzle positioned for starting.
  17. Wehmeier, Eric J., Gas turbine engine with variable area fan nozzle positioned for starting.
  18. Rensch, Detlef, Jet engine with at least one emergency drive unit.
  19. Berryann, Andrew P.; Suciu, Gabriel L., Mechanism for turbine engine start from low spool.
  20. Eick, Chris D.; Gaines, Louie T.; Laidlaw, Mitchell J.; Benson, Dwayne M.; Portolese, Larry A.; Flaherty, Brian L.; Pearson, Wayne T., More electric aircraft power transfer systems and methods.
  21. Gaines,Louie T.; Auer,Peter J.; Lane,Glenn H.; Wissinger,James A., More electric aircraft starter-generator multi-speed transmission system.
  22. Ullyott, Richard, Operation of an aircraft engine after emergency shutdown.
  23. Goi, Tatsuhiko; Tanaka, Kenichiro, Power generation unit of integrated gearbox design for aircraft engine.
  24. Bannon,David G., Pressure/flow sensing stall recovery for a ram air turbine.
  25. Ellans, Christopher J.; Martin, John H., Propulsion unit.
  26. Hutto, Jr., Walter Decania, Pump for a turbine engine.
  27. Suciu, Gabriel L.; Merry, Brian D.; Dye, Christopher M.; Glahn, Jorn A., Pump system for TMS AOC reduction.
  28. Dooley, Kevin Allan, Relighting a turbofan engine.
  29. Dooley, Kevin Allan, Relighting a turbofan engine.
  30. Dooley, Kevin Allan, Relighting a turbofan engine.
  31. Dooley, Kevin Allan, Relighting a turbofan engine.
  32. Santerre,Richard, Reversible driving apparatus for PCU pumps.
  33. Kevin Richard Leamy ; Mark Gerard Butz ; Robert William Lambert, System and method for monitoring engine starting systems.
  34. Kevin Richard Leamy ; Ronald George Maruscik, System and method for monitoring thermal state to normalize engine trending data.
  35. Restivo, Anthony P.; Zupanc, Frank J., Systems and methods for preventing oil migration.
  36. Zeiner, Peter Kenneth; Libera, Tony; Langston, Todd, Turbine drive system with lock-up clutch and method.
  37. Welch, Richard C.; Bueche, Gerard H.; DeGroff, William T.; Albero, Jose; Makuszewski, Jerzy, Turbofan emergency generator.
  38. Upton, Daniel E.; Gruhn, Joel D., Wind turbine rotor blade components and machine for making same.
  39. Gruhn, Joel D.; Franklin, Ethan; Narasimhan, Kameshwaran, Wind turbine rotor blade components and methods of making same.
  40. Gruhn, Joel D.; Franklin, Ethan; Narasimhan, Kameshwaran, Wind turbine rotor blade components and methods of making same.
  41. Gruhn, Joel D.; Franklin, Ethan; Narasimhan, Kameshwaran, Wind turbine rotor blade components and methods of making same.
  42. Gruhn, Joel D.; Franklin, Ethan; Narasimhan, Kameshwaran, Wind turbine rotor blade components and methods of making same.

관련 콘텐츠

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