A strut system for a RAT includes a strut body, a strut first end is connected to the aircraft and rotate about a first axis, a strut second end is spaced apart from the strut first end by the strut body and is connected to the RAT turbine generator unit, the strut has a strut conduit extending from the strut first end toward the strut second end; and a damper rod that includes a rod body and disposed within the strut conduit, the damper rod having a rod first end that is fixed within the strut conduit at the strut first end, and a rod second end that is spaced apart from the rod first end by the rod body and is located intermediate the strut first end and the strut second end, wherein the rod second end moves along a second axis that is parallel to the first axis.
STRUT FOR RAM AIR TURBINE WITH INNER DAMPER ROD
STREBE FÜR EINE RAM AIR TURBINE MIT EINER INNEREN DÄMPFERSTANGE
ENTRETOISE POUR TURBINE À AIR DYNAMIQUE AVEC TIGE D'AMORTISSEUR INTERNE
2024-09-18
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
Mounting bracket of vehicle suspension strut, suspension strut, damper assembly and vehicle
European Patent Office | 2023
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