Aircraft propeller balancing system

摘要

An aircraft with at least a first propeller system (3') with a first rotation axis (48) and at least a second propeller system (3') with a second rotation axis (48) is provided. The aircraft (1) includes a first means (520') for actively balancing said first propeller system (3') during aircraft flight with a first control system controller (20'), said first control system controller (20') disposed proximate said first propeller system (3') wherein said first control system controller (20') controls said first means (520') for actively balancing said first propeller system (3'). The aircraft (1) also includes a second means (520") for actively balancing said second propeller system (3') during aircraft flight with a second control system controller (20"), said second control system controller (20") disposed proximate said second propeller system (3') wherein said second control system controller (20") controls said second means (520') for actively balancing said second propeller system (3'). A method of balancing aircraft propeller systems is also provided.