Turbine and compressor employing tubercle leading edge rotor...

Details Turbine and compressor employing tubercle leading edge rotor... Turbine and compressor employing tubercle leading edge rotor...

F - Mech Eng,Light,Heat,Weapons

03

B

F03B 3/12 (2006.01) F03D 3/06 (2006.01) F03D 11/00 (2006.01) H02K 7/18 (2006.01)

Patent

CA 2587946

A turbine/compressor comprises at least one magneto-electric device and a drive train coupled to the magneto-electric device. At least one rotor blade is coupled to the drive train. The rotor blade has a shaped leading edge with a series of spaced tubercles formed therealong.

L'invention concerne un ensemble turbine/compresseur qui comprend au moins un dispositif magnétoélectrique et une transmission couplée au dispositif magnétoélectrique. Au moins une pale de rotor est couplée à la transmission. La pale de rotor présente un bord avant profilé muni d'une série de tubercules espacés le long dudit bord avant.

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