Aircraft propeller balancing system

摘要

An aircraft system and method with a first counterweight rotating balancing rotor mass concentration, and a second counterweight rotating balancing rotor mass concentration to balance a first aircraft propeller. The system includes an inboard electromagnetic coil driver with a first inboard electromagnetic coil, and a second inboard electromagnetic coil, the inboard electromagnetic coil driver and the first counterweight balancing rotor and the second counterweight balancing rotor centered around the aircraft propeller shaft rotating machine member. The system/method utilizes a first control system controller to control the coils and position the mass concentrations to balance the first aircraft propeller. The system/method includes a third counterweight rotating balancing rotor mass concentration, and a fourth counterweight rotating balancing rotor mass concentration to balance a second aircraft propeller which positioned and controlled by a second control system controller.

主权项

1. A method of balancing aircraft propeller systems, said method comprising:
providing an aircraft with at least a first propeller system with a first rotation axis and at least a second propeller system with a second rotation axis, providing a first means for actively balancing said first propeller system during aircraft flight, providing a first control system controller and disposing said first control system controller proximate said first propeller system wherein said first control system controller controls said first means for actively balancing said first propeller system during aircraft flight, providing a second means for actively balancing said second propeller system during aircraft flight, providing a second control system controller and disposing said second control system controller proximate said second propeller system wherein said second control system controller controls said second means for actively balancing said second propeller system during aircraft flight, wherein providing a first means for actively balancing said first propeller system during aircraft flight, further includes:
providing a first counterweight rotating balancing rotor with a first rotor bearing support flange arc oriented with a first mass concentration andproviding a second counterweight rotating balancing rotor with a second rotor bearing support flange arc oriented with a second mass concentration, with said first rotor bearing support flange arc retaining a first rotor outboard rotating bearing support assembly wherein said first counterweight rotating balancing rotor is rotationally supported by said first rotor outboard rotating bearing support assembly, and with said second rotor bearing support flange arc retaining a second rotor outboard rotating bearing support assembly wherein said second counterweight rotating balancing rotor is rotationally supported by said second rotor outboard rotating bearing support assembly.