Accession Number : ADD012390
Title : Thrust Reverser/Exhaust Nozzle Assembly for a Gas Turbine Engine.
Descriptive Note : Patent,
Corporate Author : DEPARTMENT OF THE AIR FORCE WASHINGTON DC
Personal Author(s) : Thayer,Edward B
Report Date : 27 May 1986
Pagination or Media Count : 8
Abstract : This patent discloses an improved thrust reverser/exhaust 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.
Descriptors : *PATENTS, *THRUST CONTROL, *GAS TURBINE NOZZLES, *EXHAUST NOZZLES, CONVERGENT DIVERGENT NOZZLES, FLOW RATE, BLOCKING, TRANSITIONS, CONSTANTS, DEFLECTORS, THRUST, THRUST REVERSAL, CONVERGENCE, GAS TURBINES
Subject Categories : Jet and Gas Turbine Engines
Distribution Statement : APPROVED FOR PUBLIC RELEASE