Systems and methods for landing gear arrangements are provided. In various embodiments, a landing gear arrangement may comprise a first composite layer, the first composite layer having a cylindrical geometry, a metallic ring comprising an inner surface and an outer surface, the metallic ring perimetrically surrounding at least a portion of the first composite layer, the inner surface being in contact with the first composite layer, a metallic connecting tab extending away from the outer surface, and a second composite layer at least partially perimetrically surrounding the metallic ring and at least partially perimetrically surrounding the first composite layer, the outer surface being in contact with the second composite layer.
MANUFACTURING METHOD OF POLYMER COMPOSITE/METAL LOAD TRANSFER JOINT FOR LANDING GEAR
2017-12-28
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
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