发明名称 |
ASYMMETRICAL SINGLE MAIN ROTOR UNMANNED AERIAL VEHICLE |
摘要 |
A single engine rotary wing aircraft is provided including a fuselage having a longitudinal first axis. A main rotor assembly is mounted to the fuselage for rotation about a second axis, perpendicular to the first axis. A tailboom is connected to an empennage. The tailboom is mounted to an end of the fuselage such that the tailboom is laterally offset from the first axis in a first direction. The rotary wing aircraft also includes a propulsion system. The single engine of the propulsion system is laterally offset from the first axis in a second direction opposite the first direction. |
申请公布号 |
US2014008486(A1) |
申请公布日期 |
2014.01.09 |
申请号 |
US201213532212 |
申请日期 |
2012.06.25 |
申请人 |
ALBER MARK R.;NEWMAN JESSICA;SIKORSKY AIRCRAFT CORPORATION |
发明人 |
ALBER MARK R.;NEWMAN JESSICA |
分类号 |
B64C27/12;B64C27/06;B64C27/82 |
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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