发明名称 |
НЕСУЩИЙ ВИНТ САМОЛЕТА С ИЗМЕНЕНИЕМ УГЛА РАБОЧИХ ЛОПАСТЕЙ |
摘要 |
FIELD: aeronautical engineering. ^ SUBSTANCE: aircraft lifting propeller has drive for synchronous turn of blades at free motion along drive shaft and rotating unit with rods mounted in it according to number of lifting propeller blades. Rods are articulated with levers. Blade synchronous turn mechanism is moved along drive shaft by means of hydraulic cylinder rod which is articulated with lug mounted in blade synchronous turn mechanism body. ^ EFFECT: enhanced reliability. ^ 1 dwg |
申请公布号 |
RU2004117275(A) |
申请公布日期 |
2006.01.10 |
申请号 |
RU20040117275 |
申请日期 |
2004.06.07 |
申请人 |
Камышников Сергей Андреевич (RU) |
发明人 |
Камышников Сергей Андреевич (RU) |
分类号 |
B64C11/30;B64C27/32 |
主分类号 |
B64C11/30 |
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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