FORCE GENERATOR WITH CENTER ATTACHMENT AND/OR REDUNDANT ATTACHMENT POINTS

The present disclosure provides an improved circular force generator having a housing configured to reduce vibrational forces transmitted to an aircraft structure. Additionally, the disclosed configuration provide the necessary safety redundancies required by the aviation industry. The circular forc...

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Bibliographic Details
Main Authors Sheppard, John L, Leicht, Douglas C, Swanson, Douglas A, Coots, Sean A, Whiteford, Gerald P, Janowski, Michael D
Format Patent
LanguageEnglish
Published 22.02.2024
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Summary:The present disclosure provides an improved circular force generator having a housing configured to reduce vibrational forces transmitted to an aircraft structure. Additionally, the disclosed configuration provide the necessary safety redundancies required by the aviation industry. The circular force generator includes mounting point around the exterior of the CFG housing and a central mounting point thereby providing redundant mounting points.
Bibliography:Application Number: US202318116051