Insulated propeller blade

Fluid reaction surfaces (i.e. – impellers) – With heating – cooling or thermal insulation means

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Details

416224, 416226, 416230, B64C 1126

Patent

active

047893044

ABSTRACT:
A propeller blade is insulated to withstand the high temperature exhaust of a gas turbine engine. The blade has a spar, a skin covering the spar and forming a contour of the blade, and an insulating layer disposed between the spar and the skin along the portion of the blade operating within the high temperature exhaust of an engine.

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