Aircraft fuel cell system

Aircraft fuel cell system

  • CN 101,933,187 A
  • Filed: 01/28/2009
  • Published: 12/29/2010
  • Est. Priority Date: 01/30/2008
  • Status: Active Application
First Claim
Patent Images

1. an aircraft fuel cell system (10) has:

  • Have oxidant inlet (14a, 14b, 14c, fuel cell 14d) (12a, 12b, 12c, 12d), this oxidant inlet (14a, 14b, 14c, 14d) be used for oxygen-containing medium supply to described fuel cell (12a, 12b, 12c, 12d);

    Oxidant supply pipeline (16), first end of this oxidant supply pipeline (16) is connected to described fuel cell (12a, 12b, 12c, 12d) described oxidant inlet (14a, 14b, 14c, 14d), and second end of this oxidant supply pipeline (16) can be connected to described airborne vehicle cabin (20) used air outlet slit (18);

    WithBe arranged in heat exchanger in the described oxidant supply pipeline (16) (30a, 30b);

    It is characterized in that (30a 30b) is suitable for and will flows through the described medium and the pipeline that flows through the airborne vehicle air-conditioning unit (32a, medium heat coupling 32b) of described oxidant supply pipeline (16) described heat exchanger.

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