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특허 상세정보

Cooling means

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64D-033/08    F02K-003/04   
미국특허분류(USC) 244/57 ; 60/3983 ; 244/117A ; 361/384
출원번호 US-0447361 (1982-12-06)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 20  인용 특허 : 5
초록

Cooling for an electronic package mounted on an aircraft engine housed in a nacelle is achieved by connecting the package to the inlet of the engine and overboard of the nacelle so that substantially continuous air flow over the electronic package will ensue from either direction depending on the varying pressure gradients adjacent the points where connections are made and the conditions exists during the flight envelope. This negates the necessity of providing positive pumping devices for effectuating the flow of the cooling air.

대표
청구항

Cooling means for an electronic package mounted on a gas turbine engine housed in a nacelle of an aircraft consisting of a first connection means for interconnecting the electronic package and the inlet of the engine, a second connection means interconnecting said electronic package, said first connection means and the ambient overboard of said nacelle, the opening of said first connection means relative to said engine inlet and the opening of said second connection means relative to said ambient overboard being located relative to pressure gradients act...

이 특허를 인용한 특허 피인용횟수: 20

  1. Wilmot, Theodore Steven; Kelbey, Ryan Gilbert. Air cooled core mounted ignition system. USP2011118046987.
  2. Negulescu Dimitrie,DEX. Aircraft gas turbine engine with a liquid-air heat exchanger. USP1999126000210.
  3. Ream Jeffrey L. (Tolland CT) Bubello Robert (North Meriden CT). Buffer region for the nacelle of a gas turbine engine. USP1991055012639.
  4. Voorhis Roger (Liverpool NY) Erbs Daryl G. (Canastota NY) Palmer John M. (Syracuse NY) Marris Derrick A. (Blossvale NY). Control module cooling. USP1987124709560.
  5. Lepage, Thomas; Gaully, Bruno Robert. Device for ventilating and supplying electrical power to an aircraft engine computer. USP2017119821736.
  6. Altoz Frank E. (Catonsville MD) Buckley John J. (Catonsville MD). Direct air cooling system for airborne electronics. USP1987064674704.
  7. Dearman,Peter Thomas. Engines driven by liquified or compressed gas. USP2006016983598.
  8. Rotta, Phillip R.; MacDuff, Jr., John G.; Roll, Phillip E.. Fixture and method for quick installation and removal of mobile platform electronic modules. USP2005076914781.
  9. Colman Michael E. (Wakefield MA) Goeller Robert E. (Beverly MA). Gas turbine engine component cooling system. USP1986094608819.
  10. Colman Michael E. (Wakefield MA) Goeller Robert E. (Beverly MA). Gas turbine engine component cooling system. USP1986074601202.
  11. Laborie, Daniel Jean-Louis. Gas turbine engine having a cooling-air nacelle-cowl duct integral with a nacelle cowl. USP2010027665310.
  12. Jain, Ashok K.. Gas turbine engine systems involving integrated fluid conduits. USP2017049611758.
  13. Bowers,John L.; Hariram,Sham S.; Patel,Jayant D.; Sikand,Sharanpal S.. Hingeless flapper valve for flow control. USP2008117448219.
  14. Zysman, Steven H.; Lord, Wesley K.; Miller, Robert M.; Atassi, Oliver V.. Passive boundary layer bleed system for nacelle inlet airflow control. USP2017059644535.
  15. Zysman, Steven H.; Lord, Wesley K.; Miller, Robert M.; Atassi, Oliver V.. Passive boundary layer bleed system for nacelle inlet airflow control. USP2014098839805.
  16. Zysman, Steven H.; Lord, Wesley K.; Miller, Robert M.; Atassi, Oliver V.. Passive boundary layer bleed system for nacelle inlet airflow control. USP2014098844553.
  17. Suciu, Gabriel L.; Sobanski, Kurt J.; Lord, Wesley K.; Ackermann, William K.. System and method for controlling an environmental condition of an engine electronic component. USP20190210196930.
  18. Parsons, John Patrick. Temperature sensing device and method of assembling the same. USP2016099442022.
  19. Coates, Laura Jean. Thermal pneumatic deicing system for an aircraft RAM air heat exchanger. USP2015119187180.
  20. Sommerer, Yannick; Jeanmougin, Stéphanie. Thermal protection device for equipment in a turbomachine engine compartment. USP2018049932900.