Apparatus and method for providing a pneumatic de-icer with a re

Aeronautics and astronautics – Aircraft structure – Ice prevention

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244121, B64D 1500

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active

054491347

ABSTRACT:
Apparatus and method for providing a pneumatic de-icer structure having a replaceable environment resistant surface are disclosed. A separable adhesive impermanently bonds the environment resistant surface to the de-icer structure. The environment resistant layer can be repeatedly replaced until the cycle life of the pneumatic de-icer structure is depleted.

REFERENCES:
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patent: 3423225 (1969-01-01), Coney et al.
patent: 3559928 (1971-02-01), Dohmeyer
patent: 3604666 (1971-09-01), Achberger
patent: 3642567 (1972-02-01), Rogers, Jr.
Estane.RTM. Erosion Material Installation Procedure, #90-30-075, Jun. 20, 1990, BFG Aerospace De-Icing Systems.
Report 75-23-062E, Aug. 2, 1993, BF Goodrich Aerospace De-Icing Systems.
Report 80-32-036C, Nov. 1, 1989, BF Goodrich Aerospace De-Icing Systems.
Report 82-32-003, Jan. 25, 1982, BF Goodrich Engineered Products Group.
Report 82-32-030, May 11, 1982, BF Goodrich Engineered Products Group.

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