Electrically conductive laminate for temperature control of airc

Details Electrically conductive laminate for temperature control of airc Electrically conductive laminate for temperature control of airc

1992-03-12

1994-09-06

Ryan, Patrick J.

Stock material or miscellaneous articles

Structurally defined web or sheet

Physical dimension specified

428212, 428213, 428246, 428332, 428336, 428373, 428374, 428408, 428418, 428902, 428926, 219529, 219548, 244134D, 427318, 427446, B64D 1516, B32S 500

Patent

active

053446968

ABSTRACT:
A laminate coating comprising a durable outer ply which is resistant to abrasion and impermeable to water, bonded to and through a conductive layer of fibers and an integrally enveloping adhesive layer which is disposed on a vehicle component surface, such that the laminate coating upon curing is bonded to the vehicle component surface such as the surface of an aircraft part especially the fuselage, wing parts or tail section. The conductive layer is connected to a source of electrical energy and control means adapted to control the temperature of the coated surface of the aircraft part.

REFERENCES:
patent: 4021008 (1977-05-01), Eichenauer
patent: 4737618 (1988-04-01), Barbier et al.
patent: 4808481 (1989-02-01), Luxon
patent: 4942078 (1990-07-01), Newman et al.
patent: 4972197 (1990-11-01), McCauley et al.
patent: 5248116 (1993-10-01), Rauckhorst

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