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특허 상세정보

Supersonic cruise airplane and engine

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02K-003/00   
미국특허분류(USC) 60/204 ; 60/243 ; 244/46
출원번호 US-0883596 (1978-03-06)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 21  인용 특허 : 0
초록

A supersonic airplane has a fuselage, a wing, a vertical stabilizer, a canard and a pair of turbine engines mounted in the fuselage. Each engine is of relatively simple design with a fixed inlet, a compressor and a turbine with a single drive shaft interconnecting the turbine and compressor. The engine can employ either fixed or variable exhaust nozzle geometry, depending on whether an afterburner is installed. The engine is point designed to provide maximum design thrust at a given intermediate throttle setting when the airplane is being propelled by th...

대표
청구항

In a turbine engine designed to provide a predetermined amount of thrust at a given throttle setting when propelling an airplane at a predetermined supersonic Mach number, the improvement comprising: control means for maintaining the corrected airflow in said engine substantially at a constant value at flight Mach numbers below said predetermined supersonic Mach number.

이 특허를 인용한 특허 피인용횟수: 21

  1. Johnson,James Edward. Aft FLADE engine. USP2007057216475.
  2. Dudebout,Rodolphe; Edmonds,David H.; Zupanc,Frank J.; DeRudder,Roger J.; Scaini,Mario; Reyes,Victor M.. Auxiliary power unit having a rotary fuel slinger. USP2006057036321.
  3. Kupratis, Daniel Bernard; Suydam, Adam Joseph; Hugill, Christopher G.. Control scheme using variable area turbine and exhaust nozzle to reduce drag. USP2017119822731.
  4. Kosaka Hideki (Kodaira JPX) Mimata Tsutomu (Akikawa JPX) Shimizu Tsuyoshi (Tokyo JPX) Yamamoto Hideharu (Tokyo JPX) Itoh Kaoru (Kodaira JPX) Shima Yasuhusa (Sayama JPX). Electronic device and method of fabricating the same. USP1983094405242.
  5. Hardy Richard (Seattle WA) Neumann Frank D. (Bellevue WA) Ruzicka Dennis E. (Enumclaw WA). Fighter aircraft. USP1997065636813.
  6. Hardy Richard (The Boeing Company ; P.O. Box 3999 ; M/S 80-PA Seattle WA 98124-2499) Neumann Frank D. (The Boeing Company ; P.O. Box 3999 ; M/S 80-PA Seattle WA 98124-2499) Ruzicka Dennis E. (The Boe. Fighter aircraft. USP1997115683061.
  7. Smith, Jesse Walter. Fixed nozzle thrust augmentation system. USP2010097788899.
  8. Johnson,James Edward. Flade gas turbine engine with fixed geometry inlet. USP2008077395657.
  9. Hyde, Roderick A.; Ishikawa, Muriel Y.; Jung, Edward K. Y.; Kare, Jordin T.; Myhrvold, Nathan P.; Tegreene, Clarence T.; Weaver, Thomas A.; Wood, Jr., Lowell L.; Wood, Victoria Y. H.. Hybrid propulsive engine including at least one independently rotatable compressor rotor. USP2013128596036.
  10. Foster, Glenn B.; Hyde, Roderick A.; Ishikawa, Muriel Y.; Jung, Edward K. Y.; Kare, Jordin T.; Myhrvold, Nathan P.; Tegreene, Clarence T.; Weaver, Thomas Allan; Wood, Jr., Lowell L.; Wood, Victoria Y. H.. Hybrid propulsive engine including at least one independently rotatable compressor stator. USP2012028109073.
  11. Hyde, Roderick A.; Ishikawa, Muriel Y.; Jung, Edward K. Y.; Kare, Jordin T.; Myhrvold, Nathan P.; Tegreene, Clarence T.; Weaver, Thomas A.; Wood, Jr., Lowell L.; Wood, Victoria Y. H.. Hybrid propulsive engine including at least one independently rotatable compressor stator. USP2013108549833.
  12. Foster, Glenn B.; Hyde, Roderick A.; Ishikawa, Muriel Y.; Jung, Edward K. Y.; Kare, Jordin T.; Myhrvold, Nathan P.; Tegreene, Clarence T.; Weaver, Thomas Allan; Wood, Jr., Lowell L.; Wood, Victoria Y. H.. Hybrid propulsive engine including at least one independently rotatable propeller/fan. USP2012018099944.
  13. Hyde, Roderick A.; Ishikawa, Muriel Y.; Jung, Edward K. Y.; Kare, Jordin T.; Myhrvold, Nathan P.; Tegreene, Clarence T.; Weaver, Thomas Allan; Wood, Jr., Lowell L.; Wood, Victoria Y. H.. Hybrid propulsive engine including at least one independently rotatable propeller/fan. USP2014108857191.
  14. Foster, Glenn B.; Hyde, Roderick A.; Ishikawa, Muriel Y.; Jung, Edward K. Y.; Kare, Jordin T.; Myhrvold, Nathan P.; Tegreene, Clarence T.; Weaver, Thomas Allan; Wood, Jr., Lowell L.; Wood, Victoria Y. H.. Hybrid propulsive engine including at least one independently rotatable turbine stator. USP2012108291716.
  15. Ramakrishnan, Kishore. Inlet assembly for an aircraft aft fan. USP20190410252790.
  16. Ramakrishnan, Kishore; Otta, Shourya Prakash. Inlet assembly for an aircraft aft fan. USP20190410259565.
  17. Yao, Jixian. Inlet guide vane assembly for reducing airflow swirl distortion of an aircraft aft fan. USP20190410253779.
  18. Razzell, Anthony G; Taylor, Mark D; Mason, Samuel A; Miller, Robert J. Pulse jet engine having pressure sensor means for controlling fuel delivery into a combustion chamber. USP2009127637096.
  19. Johnson,James Edward. Supersonic missile turbojet engine. USP2008097424805.
  20. Belleville, François; Beauchesne-Martel, Philippe; Morgan, Keith. System and method for engine transient power response. USP2016049322341.
  21. Baughman,John Lewis; Johnson,James Edward. Thrust vectoring aft FLADE engine. USP2006117134271.