The invention relates to the technical field of multidirectional die
forging, in particular to a multidirectional die
forging forming process and method for an all-
fiber piston rod of an
aircraft landing gear. The invention discloses a multi-directional die
forging forming process and method for an all-
fiber piston rod of an
aircraft landing gear. The multi-directional die forging forming process is characterized by comprising the specific steps of
raw material detection, wherein size and performance detection is conducted on raw materials meeting
purchasing requirements and specifications; preparing a blank: preparing the raw materials into the blank according to requirements; blank heating is conducted, specifically, the blank is heated; all-
fiber multi-directional die forging is conducted, specifically, the heated blank is placed on a special press, die forging forming is conducted on the
piston rod forging rod through a special die, and the drawing size is achieved;
punching is conducted, specifically, the
forge piece is subjected to
punching treatment through a multi-directional die forging technology; and heat treatment after forging: heat treatment is performed according to heat treatment specifications to meet the technical requirements of drawings. Compared with the prior art, the multi-directional die forging forming process and method for the all-fiber
piston rod of the
aircraft landing gear break through barriers in the prior art, and manufacturing of the all-fiber hollow
piston rod is achieved.