发明名称 |
TORQUE SPLIT GEARBOX FOR ROTARY WING AIRCRAFT |
摘要 |
A gearbox system for a dual coaxial counter rotating rotor assembly includes an input shaft to input a first torque into the gearbox system and a transfer shaft operably connected to the input shaft to transfer the first torque therethrough. Two gear sets are operably connected to the transfer shaft. Each gear set includes a first output gear to transfer a second torque acting in a first direction to a first rotor of a rotor assembly and a second output gear to transfer the second torque acting in a second direction opposite the first direction to a second rotor of the rotor assembly. The second torque transferred by each gear set of the two gear sets is substantially equal. |
申请公布号 |
WO2015034732(A1) |
申请公布日期 |
2015.03.12 |
申请号 |
WO2014US53058 |
申请日期 |
2014.08.28 |
申请人 |
SIKORSKY AIRCRAFT CORPORATION |
发明人 |
GARCIA, TODD A. |
分类号 |
B64C27/12;F16H1/06;F16H1/22 |
主分类号 |
B64C27/12 |
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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