Methods and apparatus for deicing airfoils or rotor blades

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

Reexamination Certificate

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C416S09600A, C415S905000

Reexamination Certificate

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10895255

ABSTRACT:
A method for deicing a rotor blade having a blade root, a blade tip, and a leading edge in which the rotor blade is operably coupled to a hub of a turbine includes circulating heated air through an outflow channel from the blade root towards the blade tip, recirculating the heated air via a return channel from the blade tip to the blade root, whereupon the recirculated heated air becomes returned air, and reheating the returned air for further circulation.

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patent: 6612810 (2003-09-01), Olsen et al.
patent: 6676122 (2004-01-01), Wobben
patent: 2228145 (2003-11-01), None

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