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
11.02.2020
Patent
Elektronische Ressource
Englisch
MANUFACTURING METHOD OF POLYMER COMPOSITE/METAL LOAD TRANSFER JOINT FOR LANDING GEAR
Europäisches Patentamt | 2020
|MANUFACTURING METHOD OF POLYMER COMPOSITE/METAL LOAD TRANSFER JOINT FOR LANDING GEAR
Europäisches Patentamt | 2017
|POLYMER COMPOSITE/METAL LOAD TRANSFER JOINT FOR LANDING GEAR
Europäisches Patentamt | 2022
|Landing gear, aircraft comprising landing gear and method of distributing load of landing gear
Europäisches Patentamt | 2023
|