An actuator rod assembly (106) for a blade pitch control system is provided herein. The actuator rod assembly (106) includes a tubular outer rod (42) and an inner rod (44). The outer rod (42) has a first end (46) and a second end (48). The inner rod (44) has a first end (50) and a second end (52) and extends through the tubular outer rod(42). The inner rod (44) is tensioned against the tubular outer rod (42) so as to place the outer rod (42) in compression.
ACTUATOR ROD ASSEMBLY FOR A BLADE PITCH CONTROL SYSTEM
ENSEMBLE TIGE D'ACTIONNEUR POUR UN SYSTEME DE COMMANDE DE PAS DE PALE
23.11.2019
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
ACTUATOR ROD ASSEMBLY FOR A BLADE PITCH CONTROL SYSTEM
Europäisches Patentamt | 2019
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