GAS TURBINE ENGINES

  • US 3,820,719 A
  • Filed: 04/30/1973
  • Issued: 06/28/1974
  • Est. Priority Date: 05/09/1972
  • Status: Expired due to Term
First Claim
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1. A nozzle for a ducted fan gas turbine engine having fan cowl means defining the nozzle area, means for relatively axially separating an upstream portion and a downstream portion of the fan cowl means to define an opening therebetween, means for directing a portion of the nozzle flow through said opening and for promoting attachment of the nozzle flow to the outer surface of the said dowNstream portion.

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