Patents Assigned to Aeronautical Concepts of Exhaust, LLC
  • Cascade reverser without blocker doors
    Patent number: 7484356
    Abstract: A translating cowl composed of two sub-structures forms the thrust reverser for a turbofan engine. The two sub-structures form the rear part of a nacelle, are translatable, and have operative and inoperative modes of operation. The operative mode is used for direct or reverse thrust operation of the engine and the inoperative mode is used for access to the engine.
    Type: Grant
    Filed: July 24, 2006
    Date of Patent: February 3, 2009
    Assignee: Aeronautical Concepts of Exhaust, LLC
    Inventor: Jean-Pierre Lair