Thrust Reverser/Exhaust Nozzle Assembly for a Gas Turbine Engine.
DEPARTMENT OF THE AIR FORCE WASHINGTON DC
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This patent discloses an improved thrust reverserexhaust nozzle assembly which has a plurality of blocker devices located in the divergent section of the exhaust nozzle and a plurality of deflector devices located in the convergent section of the nozzle. The blocker and deflector devices are linked together such that they move simultaneously and maintain a substantially constant engine between forward and reverse thrust conditions.
- Jet and Gas Turbine Engines