Aircraft supplemental liquid cooler and method

Aircraft supplemental liquid cooler and method

  • CN 102,923,310 A
  • Filed: 08/07/2012
  • Published: 02/13/2013
  • Est. Priority Date: 08/08/2011
  • Status: Active Application
First Claim
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1. aircraft 10, it comprises:

  • Deployable liquid cooler 150 with H Exch 154, described H Exch 154 fluids are coupled at least one thermal source 108 of described aircraft 10, and be configured to receive cooling system fluid 104 from described thermal source 108, in order to cycle through described H Exch 154;

    Described H Exch 154 can motion between the expanded position 174 in the stowed position 172 of described aircraft inside and the described aircraft outside;

    AndWhen described H Exch was in described expanded position 174, described H Exch 154 was configured to the heat of described cooling system fluid 104 is transferred to the environment 64 in the described aircraft outside.

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