发明名称 |
METHOD OF CONTROL OF HELICOPTER THRUSTER AND HELICOPTER THRUSTER FOR REALIZATION OF THIS METHOD |
摘要 |
aviation. SUBSTANCE: proposed thruster is mounted at rear end section of tail boom 16 helicopter. Two sets of blades deflect air flow passing longitudinal along tail boom to opposite sides of tail boom respectively. Two flaps (46 and 48) are mounted for partial rotation around sets of blades forming two holes on respective lateral sides of tail boom. Flats turn incomplete agreement in way towards each other and from each other for opening/closing respective holes symmetrically and simultaneously, thus keeping the geometric center of each hole stationary irrespective of state of adjustment of hole. EFFECT: reduced power of steering rotor actuator. 11 cl, 5 dwg
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申请公布号 |
RU2155703(C2) |
申请公布日期 |
2000.09.10 |
申请号 |
RU19980102122 |
申请日期 |
1996.07.23 |
申请人 |
DENEL (PROPRIETARI) LIMITED |
发明人 |
EHKSTER POL BRAJEN |
分类号 |
B64C27/82;(IPC1-7):B64C27/82 |
主分类号 |
B64C27/82 |
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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