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특허 상세정보

Aircraft architecture with a reduced bleed aircraft secondary power system

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64B-001/24   
미국특허분류(USC) 701/003; 244/053.R; 244/058; 244/202
출원번호 US-0076898 (2002-02-14)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Bachman & LaPointe, P.C.
인용정보 피인용 횟수 : 33  인용 특허 : 7
초록

The present invention relates to an improved architecture for an aircraft. The aircraft has a first engine, a first gearbox associated with the first engine, a first starter/generator associated with the gearbox, and a first motor drive connected to the first starter/generator for providing the starter/generator with electric power to start the first engine and to receive electric power from the starter/generator after the engine has been started to operate electrically driven systems onboard the aircraft. The aircraft preferably further has at least one...

대표
청구항

The present invention relates to an improved architecture for an aircraft. The aircraft has a first engine, a first gearbox associated with the first engine, a first starter/generator associated with the gearbox, and a first motor drive connected to the first starter/generator for providing the starter/generator with electric power to start the first engine and to receive electric power from the starter/generator after the engine has been started to operate electrically driven systems onboard the aircraft. The aircraft preferably further has at least one...

이 특허를 인용한 특허 피인용횟수: 33

  1. Himmelmann, Richard A.; Lang, David. Actuator with differential and brake. USP2012098262531.
  2. Napier, James C.. Air inlet noise attenuation assembly. USP2015119194293.
  3. Burns, Donald; Rajashekara, Kaushik. Aircraft and propulsion system. USP2014048690099.
  4. Balan, Chellappa; Sheldon, Karl Edward. Aircraft auxiliary gas turbine engine and method for operating. USP2010057721554.
  5. Burns, Donald; Rajashekara, Kaushik. Aircraft, propulsion system, and system for taxiing an aircraft. USP2014048684304.
  6. Burns, Donald; Rajashekara, Kaushik. Aircraft, propulsion system, and system for taxiing an aircraft. USP2014058727270.
  7. Light, Stacey H.; Vitale, Jack V.. Auxiliary power unit inlet. USP2013058444083.
  8. Light, Stacey H.; Vitale, Jack V.. Auxiliary power unit inlet. USP2014068740135.
  9. Parikh, Pradip G.. Combined cabin air and heat exchanger RAM air inlets for aircraft environmental control systems, and associated methods of use. USP2010127849702.
  10. Fucke, Lars; Daggett, David L.. Combined fuel cell aircraft auxiliary power unit and environmental control system. USP2011098016228.
  11. Fucke,Lars; Daggett,David L.. Combined fuel cell aircraft auxiliary power unit and environmental control system. USP2008067380749.
  12. DeRoy, Robert M.. Electric compressor for use with a wing anti-ice system. USP20181210144521.
  13. Mehl, Byron R.; Baker, Donal. Electric engine start with two motors and single motor drive. USP2010077755208.
  14. Atkey,Warren A.; Bernier,Alan T.; Bowman,Michael D.; Campbell,Thomas A.; Cruse,Jonathan M.; Fiterman,Charles J.; Meis,Charles S.; Ng,Casey Y. K.; Nozari,Farhad; Zielinski,Edward. Electric-based secondary power system architectures for aircraft. USP2007057210653.
  15. Shander, Mark S.; Cote, Richard A.; Drake, Michael L.; Carter, III, Howard; Peters, John T.; Ng, Casey Y. K.; Hoag, Michael S.; Paterson, John T.. Electrical systems architecture for an aircraft, and related operating methods. USP2010037687927.
  16. Baumann, Joerg. Emergency ram air inlet valve of an aircraft. USP2013058439061.
  17. Maddali, Vijay K.; Rozman, Gregory I.; Dooley, Kevin. Engine having power bus fault short circuit control with a disconnection switch. USP2012078213136.
  18. Francisco, Jay M.; Napier, James C.. Exhaust silencer with baffles. USP2013128596568.
  19. Bayliss, Andrew J.; Paterson, John T.; Retz, Kevin. Independent power generation in aircraft. USP2015028950703.
  20. Bayliss, Andrew J.; Paterson, John T.; Retz, Kevin. Independent power generation in aircraft. USP2014028657227.
  21. Lui, Clarence W. T.; Derouineau, Jean Luc; Claeys, Henry M.. Integrated environmental control and auxiliary power system for an aircraft. USP2009107607318.
  22. Brighton, Trevor Anthony; Elms, Martin John; Jones, Maxwell William. Landing gear. USP2014078770514.
  23. Bernard,Guy. Method and apparatus for inhibiting accretion of airborne material on a surface of an aircraft. USP2007027178760.
  24. Francisco, Jay M.; Napier, James C.; Sapiro, Dan G.; Hagshenas, Behzad. Mixed-flow exhaust silencer assembly. USP2009087578369.
  25. Maier, Josef; Beutel, Michael. Power distribution architecture for aircraft. USP2014118890355.
  26. Mehrer, Michael E.; Spencer, John P.; Vaziri, Massoud. Power distribution system and load management protocol therefor. USP2009117622821.
  27. Derouineau, Jean-Luc; Pearson, Wayne T.; Jonqueres, Michel A.. Smart hybrid electric and bleed architecture. USP2011067970497.
  28. Sheldon, Karl Edward; Turco, John. System and method for providing air to a compressor of an aircraft auxiliary gas turbine engine. USP2010037673459.
  29. Berenger,Serge. System for powering and controlling electrical equipment of an aircraft engine or its environment. USP2009017482709.
  30. Space, David R.; Matera, Jane V.; Atkey, Warren A.; Fiterman, Charles J.; Gray, John; Arnaud, Timothy J.. Systems and methods for providing airflow in an aerospace vehicle. USP2011017871038.
  31. Zielinski, Edward; Bernier, Alan T.; Knechtel, Kent W.; Campbell, Thomas A.; White, Jeffrey J.; Ralston, Mark D.. Systems and methods for starting aircraft engines. USP2009047513119.
  32. Bovitz, David J.. Universal AC or DC aircraft device power supply having power factor correction. USP2010127859874.
  33. Karimi, Kamiar J.; Liu, Shengyi; Liffring, Mark E.; Helton, Steven B.; Fu, Sheau-Wei (Johnny). Vehicle electrical power management and distribution. USP2014058738268.