A hydraulic piston actuator, which may be used for an aircraft nacelle assembly, includes a housing, a piston, an end gland, and a bearing ring. The housing is concentrically disposed along an axis. The piston is adapted to axially reciprocate within the housing. The end gland is disposed radially between the housing and the piston. The bearing ring is disposed radially between the end gland and the piston.
HYDRAULIC PISTON ACTUATOR FOR A DOOR
16.05.2019
Patent
Elektronische Ressource
Englisch
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