Method and mold for fabricating an aerodynamic airframe structur

Plastic and nonmetallic article shaping or treating: processes – Pore forming in situ – Composite article making

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264 469, 2643286, 26432812, 264DIG83, 425543, 425573, B29D 2700, B29F 103, B29F 106

Patent

active

045213542

ABSTRACT:
A method and a mold for fabricating an aerodynamic airframe structure or the like. The method using foam material introduced into the mold having split halves. The mold constructed for receiving a prefabricated stiffener skin. The mold acts as a backup restraint for the airframe structure or any other part being produced. The foam injected into the cavity adheres to the stiffener skin thereby forming an elastic foundation of continuous support for the stiffening element.

REFERENCES:
patent: 4268571 (1981-05-01), McCarthy
patent: 4303728 (1981-12-01), Houdek et al.
Wirtz, H. "Progress in RIM Technology for Automobile Components" in Plastics and Rubbers Processing, vol. 1, No. 4, Dec. 1976, pp. 167-170.

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