초록 ▼

A propeller engine system with means for generating electric power within a rotatable hub is disclosed. The means include a shaft extending into the hub so that the hub and shaft are differentially rotatable. Magnetic means are fixed to the shaft and winding means are fixed to the hub so that either

A propeller engine system with means for generating electric power within a rotatable hub is disclosed. The means include a shaft extending into the hub so that the hub and shaft are differentially rotatable. Magnetic means are fixed to the shaft and winding means are fixed to the hub so that either rotation of the rotor shaft or hub induces an electric current in the winding means.

대표청구항 ▼

1. In a propeller engine system having a rotatable hub including propeller blades, means for generating electric power within said hub for use with said blades comprising: a rotor shaft extending into said hub, wherein said hub and said rotor shaft are differentially rotatable; and generator mea

1. In a propeller engine system having a rotatable hub including propeller blades, means for generating electric power within said hub for use with said blades comprising: a rotor shaft extending into said hub, wherein said hub and said rotor shaft are differentially rotatable; and generator means including magnetic means fixed to said rotor shaft and winding means fixed to said hub for rotation therewith; wherein said differential rotation induces an electric current in said winding means. 2. In a propeller engine system having a rotatable hub with variable pitch propeller blades, said hub being operatively connected to the engine drive shaft through gearing means, means for generating electric power within said hub for actuating said blades comprising: a high speed rotor shaft driven by said engine drive shaft extending through said gearing means into said hub; magnetic means fixed to said rotor shaft and rotatable therewith; and winding means fixed to said hub for rotation therewith, wherein the rotation of said rotor shaft or said hub induces an electric current in said winding means. 3. In a propeller engine system having a static frame and a rotatable hub with variable pitch propeller blades, said hub being operatively connected to the engine drive shaft through gearing means, an actuation system for said blades comprising: an electric actuator motor, mounted within said hub for rotation with said hub, with output shaft operatively connected to said blades for pitch control; a high speed rotor shaft extending through said gearing means into said hub; and generator means including magnetic field-producing means fixed to said rotor shaft and rotatable therewith, and winding means magnetically coupled to said magnetic means, fixed to said hub for rotation therewith and electrically connectable to said motor; wherein the rotation of said rotor shaft or said hub induces an electric current in said winding means. 4. An actuation system, as recited in claim 3, further comprising control means for regulating the pitch of said propeller blades; said control means including: motor control means located within said hub for controlling the electrical energy to said motor; engine control means located within said static frame for generating pitch control signals in response to engine parameters; and signaling means for transmitting said signals from said engine control means to said motor control means. 5. An actuation system, as recited in claim 4, wherein said control means further includes a speed sensor for measuring the rotational speed of said hub; said motor control means being adapted to receive hub speed signals from said speed sensor and regulate said blade pitch independently of said engine control means so as to maintain a relatively constant hub speed. 6. An actuation system, as recited in claim 4, wherein said signaling means includes a fibre optic rotary coupler. 7. An actuation system, as recited in claim 3, further comprising gear reduction means for operatively connecting said actuator motor to said variable blades. 8. An actuation system, as recited in claim 7, wherein said rotor shaft penetrates said gear reduction means. 9. An actuation system, as recited in claim 7, wherein said generator means is located between said gearing means and said gear reduction means. 10. An acutation system, as recited in claim 7, wherein said generator means is located forward of said gear reduction means.