发明名称 |
SYSTEM OF TWO COAXIAL MAIN ROTORS OF FLYING VEHICLE |
摘要 |
aeronautical engineering; main rotors of flying vehicle. SUBSTANCE: proposed system includes reduction gear with two coaxial shafts, main rotor hubs, main rotor control circuits, two wobble plates and main rotor collective and differential pitch control mechanism. Shaft of upper main rotor is made axial downward motion bringing the lifting system to initial position without any adjustment. EFFECT: reduced overall size in height of coaxial helicopter both in parking position and in transportation. 2 dwg
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申请公布号 |
RU2155702(C1) |
申请公布日期 |
2000.09.10 |
申请号 |
RU19990108371 |
申请日期 |
1999.04.15 |
申请人 |
KUMERTAUSKOE AVIATSIONNOE PROIZVODSTVENNOE PREDPRI;JATIE |
发明人 |
MALYSHEV B.S.;SOLOV'EV A.I.;ZEVIG G.V.;BELJAEV V.V.;KHRIBKOV V.K.;VLASOV A.A.;PONOMAREV N.N.;PODNEBESNOV B.JA. |
分类号 |
B64C27/10;B64C27/32;(IPC1-7):B64C27/10 |
主分类号 |
B64C27/10 |
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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