ACTUATION MECHANISM

Number of patents in Portfolio can not be more than 2000

United States of America

APP PUB NO 20250035067A1
SERIAL NO

18768015

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ATTORNEY / AGENT: (SPONSORED)

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Abstract

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The present invention belongs to the technical field of gas turbine engines used as propulsion systems for supersonic aircraft. In particular, the invention relates to thrust vectoring convergent-divergent nozzles and, more in particular, to an actuation mechanism for vectoring said variable geometry nozzle.

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
DIEZ, CELAYA Mikel Vizcaya, ES 2 0
GÓMEZ, GARCÍA Alberto Vizcaya, ES 2 0
ORTIZ, DE ZARATE ETXEANDIA Ibon Vizcaya, ES 2 0

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