F - Mech Eng,Light,Heat,Weapons – 01 – D
Patent
F - Mech Eng,Light,Heat,Weapons
01
D
F01D 25/30 (2006.01) F02K 1/00 (2006.01) F02K 1/12 (2006.01)
Patent
CA 2089981
Thrust vectoring variable geometry exhaust nozzle for gas turbines, which includes a convergent section followed, in the direction of the gas stream, by a divergent section, both formed by master and slave petals, whose convergent section defines a throat having variable area. The divergent section has variable geometry in order to orientate the thrust, and includes governing and external radial support means for regulating the throat area, and governing means for regulating the vectoring of the thrust. Both means are formed by a single governing system consisting of three rings, concentric among themselves and with the turbine centerline, and by a plurality of linear actuators. The master petals of the divergent section are transversely subdivided into at least two segments.
Ibarreche Mendia Jose Ignacio
Rivacoba Urruela Jose
Robic
Tobera Vectorial S.l.
LandOfFree
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