Aircraft engine propulsor blade deicing

Details Aircraft engine propulsor blade deicing Aircraft engine propulsor blade deicing

1991-04-01

1992-07-21

Look, Edward K.

Fluid reaction surfaces (i.e., impellers)

With heating, cooling or thermal insulation means

244134D, B64D 1500

Patent

active

051318121

ABSTRACT:
A blade heater (10) for an aircraft engine propulsor blade (14) has a foil pattern (18) which is comprised of a plurality of elements (25-56). The resistance of the elements (25-56) varies according to the distance between the elements (25-56) and the leading edge (12) of the blade (14).

REFERENCES:
patent: 2084556 (1957-06-01), Hamilton
patent: 2496279 (1950-02-01), Ely et al.
patent: 2503457 (1950-04-01), Speir et al.
patent: 2552075 (1951-05-01), Van Daam
patent: 2599059 (1952-06-01), Jones
patent: 2743890 (1956-05-01), LaRue
patent: 4386749 (1983-06-01), Sweet et al.

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