$\require{mediawiki-texvc}$
  • 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"

특허 상세정보

System for cooling a heat exchanger on board an aircraft

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64D-013/08    B64D-013/06   
출원번호 US-0125728 (2009-10-26)
등록번호 US-9284057 (2016-03-15)
우선권정보 DE-10 2008 055 888 (2008-11-05)
국제출원번호 PCT/EP2009/007647 (2009-10-26)
§371/§102 date 20110725 (20110725)
국제공개번호 WO2010/051919 (2010-05-14)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Wood, Herron & Evans, LLP
인용정보 피인용 횟수 : 1  인용 특허 : 16
초록

A system for cooling a heat exchanger on board an aircraft includes an engine bleed air line connected to an engine of the aircraft and adapted to supply engine bleed air to the heat exchanger. The system further includes a process air line branching off from the engine bleed air line such that the engine bleed air is supplied to the process air line and connecting to an input side of a turbine. The system also includes a cooling air line connected to an output side of the turbine such that cooling air produced by an expansion of the engine bleed air sup...

대표
청구항

1. A system for cooling a heat exchanger on board an aircraft comprising: an engine bleed air line including a first end and a second end, the first end of the engine bleed air line being connected by a plurality of engine bleed air line branches to an engine of the aircraft at a plurality of positions such that engine bleed air is supplied to the engine bleed air line, the engine of the aircraft generating propulsion force to move the aircraft, wherein the heat exchanger is attached to the engine bleed air line between the first end and the second end o...

이 특허에 인용된 특허 (16)

  1. Cowell Wiley M. (Fountain Valley CA) Malmberg Quentin C. (Hermosa Beach CA) Edgar Jon M. (Long Beach CA). Advanced hybrid air/vapor cycle ECS. USP1990104966005.
  2. Ostersetzer Shlomo (Ramat Chen ILX) Lior David (Herzliya ILX). Air conditioning system. USP1994125373707.
  3. Masanao Ando JP; Osamu Satoh JP; Shoji Uryu JP; Koichi Ohara JP. Air cycle machine and air conditioning system using the same. USP2002086427471.
  4. Glickstein Marvin R. (North Palm Beach FL). Aircraft cooling method. USP1995055414992.
  5. Christoff William J. (Thousand Oaks CA). Aircraft environmental control system with auxiliary power output. USP1985034503666.
  6. 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.
  7. Bruno, Louis J.; Lents, Charles E.; Sahm, Michael K.; Thresher, Wayne A.. Electric power and cooling system for an aircraft. USP2005016845630.
  8. Glickstein Marvin R. (North Palm Beach FL) Coons Leland L. (Marlborough CT). Endothermic fuel energy management system. USP1995025392595.
  9. Schiff,Peter. Environmental control system and method for an aircraft. USP2007127305842.
  10. Sanger Roger Reed. Environmental control system no condenser high pressure water separation system. USP2000116148622.
  11. Wright E. Scott (Mesa AZ). High performance turbine engine. USP1991024991394.
  12. Glickstein Marvin R. (North Palm Beach FL) Dixon James T. (Jupiter FL) Podolsky Donald M. (Jupiter FL). High pressure air source for aircraft and engine requirements. USP1995095452573.
  13. Glickstein Marvin R. (North Palm Beach FL) Dixon James T. (Jupiter FL) Podolsky Donald M. (Jupiter FL). High pressure air source for aircraft and engine requirements. USP1996045511374.
  14. Dixon James T. (Jupiter FL) Glickstein Marvin R. (North Palm Beach FL). Integrated auxiliary power system. USP1994115363641.
  15. George E. Wilmot, Jr. ; Gregory M. Ott. Integrated thermal management and coolant system for an aircraft. USP2002076415595.
  16. Schwalm,Gregory; Surawski,Eric; Schwemmer,John; Dion,Mark. On-board inert gas generation system with compressor surge protection. USP2007117300494.