| 发明名称 |
METHOD OF CONTROL OF CARRYING SCREW OF HELICOPTER |
| 摘要 |
A method of control of carrying screw of the helicopter, in which due to the change of the damping characteristics during flapping of blades the phase angle shear between the law of variation of acting force on the blade and the law of its flapping changes, which in turn leads to the required change of the tilt of cone of carrying screw in definitedirection.
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| 申请公布号 |
UA24474(U) |
申请公布日期 |
2007.07.10 |
| 申请号 |
UA20060008260 |
申请日期 |
2006.07.24 |
| 申请人 |
IVAN KOZHEDUB KHARKIV UNIVERSITY OF AIR FORCES |
发明人 |
ONYSCHENKO VOLODYMYR MYKHAILOVYCH;MYRHOROD YURII IVANOVYCH;SHLAPATSKYI VIACHESLAV OLEKSANDROVYCH |
| 分类号 |
B64C27/32 |
主分类号 |
B64C27/32 |
| 代理机构 |
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