Asymmetrical pneumatic deicer

Details Asymmetrical pneumatic deicer Asymmetrical pneumatic deicer

1989-09-01

1990-10-09

Barefoot, Galen

Aeronautics and astronautics

Aircraft structure

Ice prevention

B64D 1518

Patent

active

049615491

ABSTRACT:
A pneumatic deicer for a strut or airfoil having a knife-edge or wedge leading edge wherein one spanwise tube of the deicer envelopes the leading edge and is positioned with at least 55% but not more than about 75% of the width of the spanwise deicer tube positioned on one surface of the wedge, the remaining portion of the width being positioned on the remaining surface of the wedge.

REFERENCES:
patent: 1890286 (1932-12-01), Geer
patent: 2320017 (1943-05-01), Spicer
patent: 2418262 (1947-04-01), Hunter
patent: 2567804 (1951-09-01), Davies
patent: 2937826 (1960-05-01), Johnson
patent: 4516745 (1985-05-01), Ely et al.
Kermod, A. C., Mechanics of Flight, Eighth edition, Pitman, pp. 96-101.
Anderson, Jr., J. D., Introduction to Flight Its Engineering & History, McGraw-Hill Book Company, New York, pp. 165-179.

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