| 发明名称 |
SERVO UNIT FOR FLYING VEHICLE CONTROL SYSTEM |
| 摘要 |
FIELD: aeronautical engineering. ^ SUBSTANCE: proposed servo unit has pump station, hydraulic mixer, hydraulic compensator and actuating cylinder with rod, locking mechanism and cross-feed valve. Locking mechanism is made in form of spring-loaded plunger with longitudinal slot where two rollers are fitted; these rollers are engageable with bevels available on rod. ^ EFFECT: enhanced reliability. ^ 3 dwg |
| 申请公布号 |
RU1840185(C) |
申请公布日期 |
2006.06.27 |
| 申请号 |
SU19731563062 |
申请日期 |
1973.04.06 |
| 申请人 |
Открытое акционерное общество Павловский машиностроительный завод " Восход " |
发明人 |
KUPRIJANOV FEDOR FEDOROVICH;PARMENOV JURIJ ALEKSEEVICH;TYCHKIN VJACHESLAV IVANOVICH;RJABOV VJACHESLAV MOISEEVICH |
| 分类号 |
B64C13/36 |
主分类号 |
B64C13/36 |
| 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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