PURPOSE: To take out a strong rotational force to the outside with a simple structure, by utilizing a ram pressure and a pulse jet engine principle, injecting an explosion gas from an injection pipe to generate a strong propulsion force.Ī gas turbine engine infra-red radiation suppressor comprising an exhaust nozzle which is surrounded by a duct having a plurality of diffuser vanes at its downstream end. PURPOSE: To facilitate the preparation of priming powder and improve ignition performance by constituting priming powder from a molded body which is prepared by uniformly dispersing main charged gunpowder in pellet form into the double-b. PURPOSE: To facilitate preparation and prevent vibration by arranging the block- shaped main charged gunpowder into a holder extending in the direction of axis line of an ignitor case and forming the holder part from the double-base comp. ![]() Eac.Ī gas turbine engine flight maneuverable nozzle for installation within an aircraft wing or the like is provided with pivotably connected convergent and divergent flaps partially defining an exhaust stream flow path. The valve is provided with a pair of back-to-back, mutually facing flow mixers of the daisy variety, each associated with a section of the coannular ducts. The thrust reverser includes a movable aerodynamic flap downstream of the asymmetric nozzle casing which is rotatable about one pivot in.Ī valve for controlling the fluid flow between two generally coannular ducts. A thrust reverser is provided for use with an asymmetric aircraft gas turbine engine exhaust nozzle.
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