Method of manufacturing a piece of material structural composite comprising a double yoke orientee radially

摘要

The present invention relates to a method of manufacture of a balance of aircraft landing gear, comprising a body provided with a double yoke (24) comprising two wings (19, 21) parallel to a radial direction with respect to the body, comprising the steps of: - form a first core; - apply a or of the first layers of braided fibers (11) on the first core; - report on the assembly thus formed, a second element of the mandrel extending between the two wings (19, 21) of the yoke (24) to form; - apply a and second layers of braided fibers (17) on the assembly thus formed; - injecting the resin in the different layers (11, 17) and polymerize the resin; - machining the blank thus formed, in order to form a notch passes through the second layers woven (17) in order to separate the two wings (19, 21) of the double yoke (24).