A hydraulic piston actuator (24), which may be used for an aircraft nacelle assembly (20), includes a housing (30), a piston (32), an end gland (42), and a bearing ring (44). The housing (30) is concentrically disposed along an axis (A). The piston (32) is adapted to axially reciprocate within the housing (30). The end gland (42) is disposed radially between the housing (30) and the piston (32). The bearing ring (44) is disposed radially between the end gland (42) and the piston (32).
AIRCRAFT NACELLE ASSEMBLY
ANORDNUNG FÜR EINE FLUGZEUGGONDEL
ASSEMBLAGE POUR UNE NACELLE D'AVION
27.09.2023
Patent
Elektronische Ressource
Englisch
Assembly for nacelle of aircraft, nacelle and aircraft comprising such assembly
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