发明名称 |
COLLECTIVE TO ELEVATOR MIXING OF A ROTARY WING AIRCRAFT |
摘要 |
An aircraft is provided including an airframe, an extending tail, and a counter rotating, coaxial main rotor assembly including an upper rotor assembly and a lower rotor assembly. A translational thrust system positioned at the extending tail, the translational thrust system providing translational thrust to the airframe. A horizontal stabilizer with a left elevator and right elevator positioned at the extending tail. A flight control computer to independently control one or more of the main rotor assembly and the elevator through a fly-by-wire control system. The flight control computer is configured to mix a collective pitch of the main rotor assembly and a deflection of the elevator. |
申请公布号 |
WO2016053958(A2) |
申请公布日期 |
2016.04.07 |
申请号 |
WO2015US52820 |
申请日期 |
2015.09.29 |
申请人 |
SIKORSKY AIRCRAFT CORPORATION |
发明人 |
ELLER, EREZ;WHITE, MATTHEW A.;LUSZCZ, MATTHEW T. |
分类号 |
B64C27/04;G06F19/00 |
主分类号 |
B64C27/04 |
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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