Method for manufacturing a composite material connecting rod having reinforced ends
AssigneeMessier-Bugatti-Dowty
InventorsRichard Masson, Patrick Dunleavy
Life of this patent
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AssigneeMessier-Bugatti-Dowty
InventorsRichard Masson, Patrick Dunleavy
Estimating the term…
In the field of aviation, a method of fabricating a composite-material rod. The method comprises a first step of fabricating a mandrel comprising a sleeve of composite material and solid inserts of composite material secured to the ends of said sleeve to constitute a rigid whole. Then, one or more layers of braided fibers are applied around the mandrel by using a fiber-braiding machine. Next, a resin is injected into the layers of braided fibers so as to establish cohesion rigidly bonding the braided fiber layers and at least the ends of the mandrel in order to form a rod body out of composite material having reinforced ends. Finally, respective holes are drilled at each end of the rod body, each hole passing through the layers of braided fibers and also through the corresponding insert.
A method of fabricating a composite-material rod having reinforced ends, the method comprising the steps of:
Dependencies are inferred from the claim text.