Engine nacelle of an aircraft comprising a vortex generator arrangement

Engine nacelle of an aircraft comprising a vortex generator arrangement

  • CN 101,687,542 A
  • Filed: 06/16/2008
  • Published: 03/31/2010
  • Est. Priority Date: 06/15/2007
  • Status: Active Application
First Claim
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1. the engine nacelle of an aircraft, described engine nacelle comprise the nacelle housing (19) with first side (S1) and second side (S2) and the vortex generator (21,22,23 of a plurality of fin shapes;

  • 31,32), described vortex generator is arranged on the wherein side in the described both sides (S1, S2) of described nacelle housing (19) and makes under the situation that the angle of attack increases, and the vortex zone that is produced by vortex generator is along extending on the wing zone that spanwise increases on the whole in order to improve maximum lift.

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