| 发明名称 |
TWO-STAGE ROCKET SEPARATOR |
| 摘要 |
FIELD: transport.SUBSTANCE: proposed devise is composed of rudder control mechanism and includes two links articulated with aerodynamic and gas rudders. Link coupled with aerodynamic rudder comprises bracket with groove, rocker with opening, link connected with gas rudder and rocker with pin. Rockers are articulated with two tie-rods.EFFECT: higher reliability of separation.3 dwg |
| 申请公布号 |
RU2548261(C1) |
申请公布日期 |
2015.04.20 |
| 申请号 |
RU20140107991 |
申请日期 |
2014.03.04 |
| 申请人 |
OTKRYTOE AKTSIONERNOE OBSHCHESTVO "VOENNO-PROMYSHLENNAJA KORPORATSIJA "NAUCHNO-PROIZVODSTVENNOE OB"EDINENIE MASHINOSTROENIJA" |
发明人 |
SHESTAKOV SERGEJ ALEKSANDROVICH;ZEMSKOV VJACHESLAV ALEKSANDROVICH;DERGACHEV ALEKSANDR ANATOL'EVICH |
| 分类号 |
B64G1/64 |
主分类号 |
B64G1/64 |
| 代理机构 |
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