Patent ID: 8961140
Filing Date: 2015-02-24
Classification: B64C,F01D,Y10S,Y10T

Abstract:
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: