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Bypass lip seal

  • US 20080053060A1
  • Filed: 08/29/2006
  • Published: 03/06/2008
  • Est. Priority Date: 08/29/2006
  • Status: Abandoned Application
First Claim
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1. A cooling apparatus for cooling a fluid in a bypass gas turbine engine, said apparatus comprising:

  • a heat exchanger defining a fluid passage, said heat exchanger being disposed within a bypass duct and being exposed to a bypass air flow; and

    a flow divider affixed to an annular wall of said bypass duct, in combination with said wall of said bypass duct forming a sub-passage for accommodating said heat exchanger, said sub-passage defining an open upstream end and an open downstream end to direct a portion of said bypass air flow to pass therethrough.

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