Structural skin construction materials and method

Aeronautics and astronautics – Aircraft structure – Airfoil construction

Patent

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Details

46 76R, 156 85, 264342R, 264DIG71, 428411, 428913, B64C 326

Patent

active

040957608

ABSTRACT:
A structural cover skin for components of a fluid-medium craft, especially the foil components of the craft, wherein a layer of heat shrinkable, polymeric film, preferably of polyvinyl fluoride is bonded to a layer of heat-shrinkable polymeric film and/or fabric, preferably of polyester, to form a special laminated heat shrink covering material particularly useful for man-flown airplanes. A method for covering the frame portions includes an encapsulating envelope of the noted material or an overlapped wrapping which is heat shrunk tautly to the contours of the frame.

REFERENCES:
patent: 3186866 (1965-06-01), Claeys
patent: 3228823 (1966-01-01), Usala et al.
patent: 3388651 (1968-06-01), Axelrod
patent: 3488249 (1970-01-01), Wolinski
patent: 3578521 (1971-05-01), Evans
patent: 3900653 (1975-08-01), Riboulet

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