$\require{mediawiki-texvc}$
  • 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"

과학기술 지식인프라 ScienceON

상세검색 다국어 입력
도움말도움말

특허 상세정보

MyON담기
내보내기

Aircraft environmental control system with auxiliary power output

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02C-006/08   
미국특허분류(USC) 60/3907 ; 60/39183
출원번호 US-0494824 (1983-05-16)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 45  인용 특허 : 2
초록

An environmental control system for a jet aircraft has a single compressor coupled to a cooling turbine and an auxiliary power turbine. The compressor provides air to both turbines. Air to the power turbine is mixed with fuel to form combustion gases to drive the turbine. Air to the cooling turbine is cooled by expansion and used for air conditioning the aircraft cabin. The auxiliary power turbine can be decoupled and the compressor driven by the cooling turbine, which is powered by bleed air from the main engine of the aircraft.

대표
청구항
▼

An environmental control system for a jet engine propelled aircraft, comprising: an air compressor, a cooling turbine, an overrunning clutch, and a power turbine rotatively coupled to the compressor and the cooling turbine, the clutch being located between the power turbine and said other components, means directing compressed air from the compressor to the power turbine, means for mixing fuel with said compressed air and burning said mixture to fuel the power turbine and drive the compressor, means for directing compressed air from the compressor to the...

이 특허에 인용된 특허 (2)

  1. Friedrich Helmut (Bremen DT). Apparatus for starting aircraft engines and for operating auxiliary on-board power generating equipment. USP1976063965673.
  2. Young ; Richard N.. Independent power generator. USP1978054091613.

이 특허를 인용한 특허 피인용횟수: 45

  1. Klimpel, Frank; Schmidt, Stephan-Anton; Beier, Jens. Aircraft air conditioning system comprising a separate refrigeration cycle. USP2016119487300.
  2. Mackin, Steve G.; Foutch, David W.; Landre, Eric G.. Aircraft bleed air and engine starter systems and related methods. USP20181010100744.
  3. Ho, YuHang; Knowles, Jeffrey A.. Apparatus for aircraft with high peak power equipment. USP2016059328661.
  4. Foutch, David W.; Mackin, Steve G.. Bleed air systems for use with aircraft and related methods. USP2017119810158.
  5. Foutch, David W.; Mackin, Steve G.; Bowman, Michael D.. Bleed air systems for use with aircraft and related methods. USP20180810054051.
  6. Mackin, Steve G.; Foutch, David W.. Bleed air systems for use with aircrafts and related methods. USP2015028955794.
  7. Mackin, Steve G.; Ludlow, George A.. Bleed air systems for use with aircrafts and related methods. USP2015038967528.
  8. Mackin, Steve G.; Ludlow, George A.. Bleed air systems for use with aircrafts and related methods. USP2017099765700.
  9. Holt, Christopher G.; Martin, William L.. Dual end gear fluid drive starter. USP2013028381617.
  10. 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.
  11. DeRoy, Robert M.. Electric compressor for use with a wing anti-ice system. USP20181210144521.
  12. Bruno, Louis J.; Lents, Charles E.; Sahm, Michael K.; Thresher, Wayne A.. Electric power and cooling system for an aircraft. USP2005016845630.
  13. 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.
  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. Kimura Shigeaki (2-120 ; 35-1 ; Oshitate-cho 1-chome ; Fuchu-shi Tokyo JPX). Energy supply system utilizing gas and steam turbines. USP1997105678401.
  17. Suciu, Gabriel L.. Gas turbine engine thermal management system for heat exchanger using bypass flow. USP20180710036329.
  18. Wright E. Scott (Mesa AZ). High performance turbine engine. USP1991024991394.
  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. Munoz, Jules Ricardo; Bertuccioli, Luca; Sahm, Michael K.; Fletcher, Jay; Lents, Charles E.; Squier, Steve; Welch, Richard; Becker, Arthur Curtis. Integrated air turbine driven system for providing aircraft environmental control. USP2004096796527.
  22. Lui, Clarence W. T.; Derouineau, Jean Luc; Claeys, Henry M.. Integrated environmental control and auxiliary power system for an aircraft. USP2009107607318.
  23. Derouineau, Jean Luc; Schenk, Bjoern; Lui, Clarence. Integrated power and pressurization system. USP2009087578136.
  24. Munoz, Jules Ricardo; Bertuccioli, Luca; Sahm, Michael K.; Fletcher, Jay; Lents, Charles E.; Squier, Steven E.; Welch, Richard; Becker, Arthur Curtis. Integrated system for providing aircraft environmental control. USP2004116817575.
  25. Biess, Lawrence J; Gotmalm, Christer T. Locomotive and auxiliary power unit engine controller. USP2005086928972.
  26. Biess, Lawrence J; Stewart, Ted E.. Locomotive emission reduction kit and method of earning emission credits. USP2003106636798.
  27. Ho, Yu-Hang. Magnetically coupled integrated power and cooling unit. USP2004086776002.
  28. Houssaye, Laurent. Method and architecture for recovery of energy in an aircraft. USP2016049302775.
  29. Murry, Roger P.. Method of heating for an aircraft electric environmental control system. USP2003106629428.
  30. Martin, William L.; Holt, Christopher G.. Multi-compressor string with multiple variable speed fluid drives. USP2013088517693.
  31. Sites, Omar Angus. Parallel dynamic compressor arrangement and methods related thereto. USP2016039284964.
  32. Stolte, Ralf-Henning. Power distribution system. USP2014038672263.
  33. Manabe, So; Fujii, Kentaro. Power generation system, driving method for power generation system, and combustor. USP20181010107190.
  34. Army, Jr., Donald E.; Zywiak, Thomas M.; Anderson, Jr., David. Primary heat exchanger crossover bypass manifold. USP2018019873511.
  35. Pal, Debabrata. Ram air fan and power electronics cooling systems. USP2017119832910.
  36. Atkey, Warren A.; Mackin, Steve G.; Millar, Rod. System and method for improved cooling efficiency of an aircraft during both ground and flight operation. USP2015038973393.
  37. Biess, Lawrence J; Gotmalm, Christer. System and method for supplying auxiliary power to a large diesel engine. USP2005096945207.
  38. Biess,Lawrence J.; Gotmalm,Christer T.. System and method for supplying auxiliary power to a large diesel engine. USP200805RE40286.
  39. Lawrence J Biess. System and method for supplying auxiliary power to a large diesel engine. USP2002106470844.
  40. Kelnhofer, Juergen. System for cooling a heat exchanger on board an aircraft. USP2016039284057.
  41. 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.
  42. 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.
  43. Niggemann Richard E. ; Nguyen Dam. Thermal and energy management method and apparatus for an aircraft. USP2001026182435.
  44. Wolfe, David; Minh, Nguyen Q.; Meister, Kurt; Matulich, Dan S.. Turbomachine-driven environmental control system. USP2004056735953.
  45. Karimi, Kamiar J.; Liu, Shengyi; Liffring, Mark E.; Helton, Steven B.; Fu, Sheau-Wei (Johnny). Vehicle electrical power management and distribution. USP2014058738268.

IPC 상위 출원인