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특허 상세정보

Cooling air supply for the cooling of different systems requiring cooling air in an aircraft

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B60H-001/00    F25D-009/00    B64D-033/02    B64D-011/00    B64G-001/48   
미국특허분류(USC) 165/041; 165/044; 062/401; 062/402; 244/053B; 244/117A; 244/118.5
출원번호 US-0582151 (2004-12-30)
등록번호 US-8602088 (2013-12-10)
우선권정보 DE-103 61 657 (2003-12-30)
국제출원번호 PCT/EP2004/014845 (2004-12-30)
§371/§102 date 20060608 (20060608)
국제공개번호 WO2005/063569 (2005-07-14)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Wood, Herron, Evans, LLP
인용정보 피인용 횟수 : 8  인용 특허 : 15
초록

A cooling air supply system for an aircraft is configured to supply cooling air from the surroundings of the aircraft to at least two devices requiring cooling air (38, 44, 56) within the aircraft. The cooling air supply system includes an air inlet, an air channel communicating with the air inlet, and an air distribution device for the distribution of air from the air channel to the at least two devices requiring cooling air. The air inlet is sized to provide sufficient air flow to accommodate a maximum cooling air requirement of the at least two device...

대표
청구항

1. A cooling air supply system configured to supply cooling air from the surroundings of an aircraft to at least two devices requiring cooling air within the aircraft, the cooling air supply system comprising: an air inlet,an air channel communicating with the air inlet,an air distribution device configured to distribute air from the air channel directly to the at least two devices requiring cooling air, the air distribution device being located downstream from the air channel and upstream from the at least two devices requiring cooling air, andat least ...

이 특허에 인용된 특허 (15)

  1. McAuliffe, Christopher; Merritt, Brent J.; Beers, Craig M.. Air cycle machine for an aircraft environmental control system. USP2013018347647.
  2. Merritt, Brent J.; Beers, Craig M.. Air cycle machine integrated rotor and shaft. USP2013048418495.
  3. Horstman Raymond H. (Auburn WA) Monda Damian G. (Seattle WA) Peash Douglas E. (Enumclaw WA) Yorozu Arthur S. (Seattle WA). Aircraft cabin ventilation system. USP1988054742760.
  4. Centofante, Nico; Petrac, Markus; Scherer, Thomas; Buchholz, Uwe. Device and method for temperature control in an aircraft cabin. USP2012128336610.
  5. Altoz Frank E. (Catonsville MD) Buckley John J. (Catonsville MD). Direct air cooling system for airborne electronics. USP1987064674704.
  6. 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.
  7. Williams Samuel B. ; Jones John F. ; Thompson ; Jr. Robert S.. Environment control unit for turbine engine. USP2001026189324.
  8. Lloyd B. Tisdale ; Robert L. Hauck ; Paul T. Tisdale, Jr.. Gas turbine engine modular cooling and heating apparatus. USP2002076422018.
  9. Nordstrm Christer (Hallingstorp S-590 54 Sturefors SEX) Axelsson Tomas (Snickarestigen 4 S-240 13 Genarp SEX) White Thomas (Tryggs vg 2 S-610 55 Stigtomta SEX). Method and means to prevent condensation in monocoque structures. USP1995025386952.
  10. Searle Robin H. J. (Yeovil GB2). Molecular sieve bed containers. USP1988044737170.
  11. Severson Mark H. (Rockford IL). Ram air flow system for aircraft. USP1989094865267.
  12. Janeke, Charl E.. Reversible space plane. USP2013088505852.
  13. Howard Robert W. (Anaheim CA). Skin heat exchanger. USP1989044819720.
  14. Miller Franklin E. (Cincinnati OH). Turbojet cooling system. USP1994105357742.
  15. Laib,Trevor M.. Ventilated seating system with improved low pressure performance. USP2006047029065.

이 특허를 인용한 특허 피인용횟수: 8

  1. Thomassin, Jean; Bolduc, Sebastien; Villeneuve, Bruno; Berube, Stephane; Fontaine, Mike; Gagnon-Martin, David; Bilodeau, Jade; Julien, Andre; Legare, Pierre-Yves; Nichols, Jason. Compound engine assembly with coaxial compressor and offset turbine section. USP2018049932892.
  2. Thomassin, Jean; Bolduc, Sebastien; Villeneuve, Bruno; Berube, Stephane; Fontaine, Mike; Gagnon-Martin, David; Julien, Andre; Cunningham, Mark; Lafortune, Serge; Legare, Pierre-Yves. Compound engine assembly with common inlet. USP2017109797297.
  3. Thomassin, Jean; Bolduc, Sebastien; Villeneuve, Bruno; Berube, Stephane; Fontaine, Mike; Gagnon-Martin, David; Julien, Andre; Cunningham, Mark; Lafortune, Serge; Legare, Pierre-Yves. Compound engine assembly with modulated flow. USP2018029896998.
  4. Thomassin, Jean; Bolduc, Sebastien; Villeneuve, Bruno; Berube, Stephane; Fontaine, Mike; Gagnon-Martin, David; Julien, Andre; Cunningham, Mark; Lafortune, Serge; Legare, Pierre-Yves. Engine intake assembly with selector valve. USP2018019879591.
  5. Kastell, Dirk; Noreiga, Wilson Willy Casas. System and method for ventilating explosive regions of an aircraft. USP2015049011218.
  6. Kelnhofer, Juergen. System for ventilation of an aircraft area. USP2015079085365.
  7. Guering, Bernard; Durand, Yves. Ventilation system, air blowing and extraction circuits of such a system, as well as an aircraft avionics bay. USP2015129216809.
  8. Van Zyl, Louwrens Hermias. Wing control system. USP2016099434468.