发明名称 |
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. |
申请公布号 |
US2012269626(A1) |
申请公布日期 |
2012.10.25 |
申请号 |
US201113273341 |
申请日期 |
2011.10.14 |
申请人 |
WINZENZ WAYNE LEE;BADRE-ALAM ASKARI;BOSWELL DAVID;MORRIS DONALD |
发明人 |
WINZENZ WAYNE LEE;BADRE-ALAM ASKARI;BOSWELL DAVID;MORRIS DONALD |
分类号 |
B64C11/18;B23P17/00;F01D25/04 |
主分类号 |
B64C11/18 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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