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
2023-09-27
Patent
Electronic Resource
English
Assembly for nacelle of aircraft, nacelle and aircraft comprising such assembly
European Patent Office | 2023
|AIRCRAFT JET ENGINE NACELLE, PROPULSION ASSEMBLY AND AIRCRAFT COMPRISING SUCH A NACELLE
European Patent Office | 2019
|Aircraft jet engine nacelle, propulsion assembly and aircraft comprising such a nacelle
European Patent Office | 2022
|Aircraft nacelle section and aircraft having aircraft nacelle section
European Patent Office | 2022
|