$\require{mediawiki-texvc}$
  • 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"
쳇봇 이모티콘
안녕하세요!
ScienceON 챗봇입니다.
궁금한 것은 저에게 물어봐주세요.

특허 상세정보

Integrated auxiliary power and environmental control unit

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02C-006/08   
미국특허분류(USC) 60/3907 ; 60/3915 ; 60/39183
출원번호 US-0422118 (1982-09-23)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 28  인용 특허 : 2
초록

An integrated auxiliary power unit and environmental control unit for an airplane 2, said integrated unit 2 comprising a prime mover 4, a variable geometry compressor 22 operable selectably by bleed air from the propulsion engine of said airplane or connectable via an overrunning clutch 18 to said prime mover, a controlled emission turbine 24 which is shaft-coupled to said compressor 22 and cooperating with said compressor to form an environmental control unit, and means for diverting a portion of the output of said compressor for use as an auxiliary pow...

대표
청구항

An integrated environmental control and auxiliary power unit for a vehicle having a propulsion engine, said unit comprising: a prime mover; a variable geometry compressor including a diffuser having a plurality of controllable variable exit vanes; means for positioning said variable exit vanes to control the output flow of said compressor; an overrunning clutch operable to couple said prime mover to drive said compressor; means for supplying bleed air from said propulsion engine to drive said compressor when said prime mover is not running; a controlled ...

이 특허를 인용한 특허 피인용횟수: 28

  1. Thompson,Robert G.; Hagshenas,Bezhad. Auxiliary power unit with an oil-free compressor. USP2006087093447.
  2. Jones, Anthony; Julien, Andre; Menheere, David; Thomassin, Jean; Ullyott, Richard; Van Den Ende, Daniel. Auxiliary power unit with variable speed ratio. USP20190310240521.
  3. Knight, Glenn A; Maguire, Alan R; Robinson, Daniel; Bostock, George; Wilson, Mark J. Compressor tip injector. USP20181210145387.
  4. Beaud, Southdary; Martin, Laurent. Device and a method for regulating a turbine engine, and an aircraft. USP2014088800295.
  5. Asfia, Julie F.; Williams, Kenneth R.; Atkey, Warren A.; Fiterman, Charles J.; Loukusa, Steven M.; Ng, Casey Y.. Electric air conditioning system for an aircraft. USP2003036526775.
  6. 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. USP2007047207521.
  7. 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.
  8. 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.
  9. Kimura Shigeaki (2-120 ; 35-1 ; Oshitate-cho 1-chome ; Fuchu-shi Tokyo JPX). Energy supply system utilizing gas and steam turbines. USP1997105678401.
  10. Horner Michael W.. Extracted, cooled, compressed/intercooled, cooling/ combustion air for a gas turbine engine. USP2000046050080.
  11. Horner Michael W.. Extracted, cooled, compressed/intercooled, cooling/combustion air for a gas turbine engine. USP1998035724806.
  12. Rodgers Colin (San Diego CA). Fast recharge compressor. USP1991085042970.
  13. Gustafson,James R.. Gas turbine engine system having an electric starter motor with integral clutch. USP2006117131275.
  14. Butt, David C; Maguire, Alan R. Generator assembly. USP2009067543439.
  15. Bayliss, Andrew J.; Paterson, John T.; Retz, Kevin. Independent power generation in aircraft. USP2015028950703.
  16. Bayliss, Andrew J.; Paterson, John T.; Retz, Kevin. Independent power generation in aircraft. USP2014028657227.
  17. Lui, Clarence W. T.; Derouineau, Jean Luc; Claeys, Henry M.. Integrated environmental control and auxiliary power system for an aircraft. USP2009107607318.
  18. Dittmar,Kevin S.; Edmonds,David H.; Schenk,Bjoern; Sheoran,Yogendra Y.. Integrated gearless and nonlubricated auxiliary power unit. USP2007087251942.
  19. Leamy, Kevin Richard; Breig, Benjamin Paul; Epstein, Michael Jay; Parrilla, Javier Armando; Hurt, Matthew John; Brinson, Thomas Edward; Fleming, Andrew James. Jet engine cold air cooling system. USP20190410247100.
  20. Ho, Yu-Hang. Magnetically coupled integrated power and cooling unit. USP2004086776002.
  21. Barkowsky, Jan; Dittmar, Jan. Main engine start by means of an aircraft air conditioning system. USP2014098844296.
  22. Coons, Terry L.. Method and system for providing cooling and power. USP2011098019522.
  23. Weber Kent ; Short Keith E.. Multi-path secondary power system for an aircraft. USP2000116142418.
  24. Scothern, David P.. Propulsion engine. USP2012108297039.
  25. White, Jeffrey J.; Toy, David K.; Groat, J. Everett. Systems and methods for controlling aircraft electrical power. USP2012048155876.
  26. 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.
  27. 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.
  28. Karimi, Kamiar J.; Liu, Shengyi; Liffring, Mark E.; Helton, Steven B.; Fu, Sheau-Wei (Johnny). Vehicle electrical power management and distribution. USP2014058738268.