$\require{mediawiki-texvc}$
  • 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

Bleed air systems for use with aircraft and related methods

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02C-009/18    F02C-003/10    F02C-007/047    F02C-007/27    F02C-007/32    B64D-013/06   
출원번호 US-0242570 (2014-04-01)
등록번호 US-9810158 (2017-11-07)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Henley, Flight & Zimmerman, LLC
인용정보 피인용 횟수 : 0  인용 특허 : 38
초록
▼

Bleed air systems for use with aircraft and related methods are disclosed. An example apparatus includes a compressor having a compressor inlet, a compressor outlet, and a first drive shaft. The compressor outlet is to be fluidly coupled to a system of an aircraft that receives pressurized air, and the compressor inlet is to receive bleed air from a low-pressure compressor of an engine of the aircraft. The example apparatus includes a gearbox operatively coupled to the first drive shaft to drive the compressor. The gearbox is to be operatively coupled to...

대표
청구항
▼

1. A bleed air system for an aircraft comprising: a turbo-compressor comprising a compressor, a turbine, and a first drive shaft coupled between the compressor and the turbine, the first drive shaft to enable the turbine to selectively drive the compressor, the compressor having a compressor inlet and a compressor outlet, the compressor outlet to be fluidly coupled to a system of the aircraft that receives pressurized air, the compressor inlet to receive bleed air from a low-pressure compressor of an engine of the aircraft;a gearbox operatively coupled t...

이 특허에 인용된 특허 (38)

  1. Kinsell Robert C. (Los Angeles CA) Noe James C. (Canoga Park CA) Byrne John P. (Westminster CA). Air cycle air conditioning system for vehicles. USP1977044015438.
  2. Zywiak, Thomas M.. Air cycle air conditioning with adaptive ram heat exchanger. USP2005096942183.
  3. Scherer, Thomas; Schmidt, Ruediger; Solntsev, Alexander. Air supply for an aircraft. USP2009117618008.
  4. Brutscher,Norbert; Haas,Joachim. Air-conditioning system and a method for the preparation of air for the air-conditioning of a space. USP2008127467524.
  5. Casey Y. K. Ng ; Warren Andrew Atkey ; Gregg Grant LaVoy ; Leigh M. Sedgwick. Aircraft air conditioning system and method. USP2002066401473.
  6. Glickstein Marvin R. (North Palm Beach FL). Aircraft cooling method. USP1995055414992.
  7. Christoff William J. (Thousand Oaks CA). Aircraft environmental control system with auxiliary power output. USP1985034503666.
  8. Rudolph Peter K. C. (Seattle WA) Georgefalvy Dezso (Mercer Island WA). Anti-icing system for aircraft. USP1992055114100.
  9. Renninger, Stanton W.; Giffin, III, Rollin G.. Auxiliary refrigerated air system employing mixture of air bled from turbine engine compressor and air recirculated within auxiliary system. USP1991085036678.
  10. Mackin, Steve G.; Foutch, David W.. Bleed air systems for use with aircrafts and related methods. USP2015028955794.
  11. Gupta Alankar (Renton WA) Runnels Joe N. (Bellevue WA). Cabin-air recirculation system powered by cabin-to-ambient pressure differential. USP1981044262495.
  12. Suciu, Gabriel L.; Merry, Brian D.; Glahn, Jorn A.; Dye, Christopher M.. Constant speed pump system for engine ECS loss elimination. USP2015109163562.
  13. Jones,Philip E.. Cooling system for an on-board inert gas generating system. USP2006026997013.
  14. Beier, Jens; Klimpel, Frank. Device and process for heating an aircraft cabin. USP2010067727057.
  15. Dowd Peter J. ; Greenberg Michael D.. Distribution damper valve. USP1999055899805.
  16. Critchley, Ian L.; Kingery, Barry J.; Frost, Cristopher; Walhood, David G.; Sumegi, Robert B.. Dual mode power unit having a combustor bypass system. USP2005126971241.
  17. 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.
  18. 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.
  19. Lents, Charles E.; Squier, Steven E.; Thresher, Wayne A.. Electrically driven aircraft cabin ventilation and environmental control system. USP2004016681592.
  20. Cronin Michael J. (Sherman Oaks CA) Seid Gordon (Los Angeles CA). Energy-efficient all-electric ECS for aircraft. USP1984124487034.
  21. Douglas S. Walkinshaw CA; Gintautas P. Mitalas CA; Campbell S. L. McNeil CA; Keith F. Preston CA. Environment control system for aircraft having interior condensation problem reduction, cabin air quality improvement, fire suppression and fire venting functions. USP2002126491254.
  22. Williams Samuel B. ; Jones John F. ; Thompson ; Jr. Robert S.. Environment control unit for turbine engine. USP2001026189324.
  23. Sampson, Bernard Francis. Environmental control system. USP2004096796131.
  24. Finney, Adam M.. Gas turbine bleed energy recovery via counter rotating generator. USP2011118063501.
  25. Mahoney,Timothy D.; Laidlaw,Mitchell J.; Libera,Anthony C.. Gas turbine engine bleed air power assist system and method. USP2007077246482.
  26. Coffinberry George A. (West Chester OH). Gas turbine engine powered aircraft environmental control system and boundary layer bleed. USP1992095143329.
  27. Farrington Franklin D.. High efficiency environmental control systems and methods. USP1999105967461.
  28. Ellsworth Scott P. (4365 S. Maidie La. West Valley City UT 84119). Humidification process and apparatus. USP1996065524848.
  29. Dixon James T. (Jupiter FL) Glickstein Marvin R. (North Palm Beach FL). Integrated auxiliary power system. USP1994115363641.
  30. Lui Clarence. Integrated bleed air and engine starting system. USP2001106305156.
  31. Lui, Clarence W. T.; Derouineau, Jean Luc; Claeys, Henry M.. Integrated environmental control and auxiliary power system for an aircraft. USP2009107607318.
  32. Brown, Ryan; Olivarez, Jason; Roberts, Kenneth. Linear quadratic regulator control for bleed air system fan air valve. USP2013098529189.
  33. Breer, Marlin D.; Olsen, Ronald F.; Kunze, Jr., Robert K.; Riedel, Brian L.. Method and apparatus for aircraft inlet ice protection. USP2004026688558.
  34. Murry, Roger P.. Method of heating for an aircraft electric environmental control system. USP2003106629428.
  35. Williams Kenneth R.. Multi-mode secondary power unit. USP1998095813630.
  36. Cronin Michael J. (Sherman Oaks CA). Multifunction power system for an aircraft. USP1987084684081.
  37. Porte, Alain. System for deicing an air inlet cowl for a turbine engine. USP2011118047470.
  38. 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.

IPC 상위 출원인