Thrust reversing system for counter rotating propellers

Fluid reaction surfaces (i.e. – impellers) – Method of operation

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Details

416129, 244 69, 244110B, B64C 1148

Patent

active

050549987

ABSTRACT:
A method of creating thrust reversal for an engine having counter-rotating forward and rear propeller blades. The forward blades are set at a positive angle of attack to produce an orderly flow of air toward the rear blades. The rear blades are set at a negative angle of attack to produce reverse thrust. The net effect is that the thrust produced by the rear blades overbalances that of the forward blades to produce net thrust reversal.

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`Power Flow in a Differential`, Machine Design, Apr. 8, 1976 Fred A. Shen, pp. 77-79.

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