A nozzle assembly for an ejection seat may comprise a servo valve assembly, a reservoir a cylinder, a nozzle manifold housing comprising a monolithic body having internal manifold structures integral to the body configured to communicate a gas between a pressure source and the reservoir, and configured to communicate a hydraulic fluid between, the reservoir, the servo valve assembly, and the cylinder, a rack piston disposed within the cylinder and configured to translate axially therein between a base end and a head end of the cylinder, and a linear nozzle coupled to the rack piston and configured to rotate in response to an axial translation of the rack piston.
Hydraulic thrust vector pitch control nozzle for rocket catapult
2022-05-03
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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