发明名称 |
METHOD FOR INSTALLATION OF EMPENNAGE BLADES OF MISSILE STABILISING DEVICE |
摘要 |
FIELD: weapons and ammunition. ^ SUBSTANCE: method for installation of missile stabilising device empennage blades includes assembly of empennage with rigidly fixed blades on vessel at the specified working angle of blade inclination, measurement and calculation of actual working angle of inclination of each installed blade. Discrepancy of actual and specified working angles of missile stabilising device empennage blades inclination is compensated due to arrangement of levelling site with specified width at surface of each blade, and its determining linear size is calculated according to the given formula. ^ EFFECT: invention maintains specified mode of missile rotation. ^ 2 cl, 2 dwg |
申请公布号 |
RU2403530(C1) |
申请公布日期 |
2010.11.10 |
申请号 |
RU20090132446 |
申请日期 |
2009.08.27 |
申请人 |
GOSUDARSTVENNOE UNITARNOE PREDPRIJATIE "KONSTRUKTORSKOE BJURO PRIBOROSTROENIJA" |
发明人 |
MOROZOV VLADIMIR IVANOVICH;GOLOMIDOV BORIS ALEKSANDROVICH;SIMAKOV SERGEJ JUR'EVICH;PETROV VALERIJ BORISOVICH |
分类号 |
F42B10/14 |
主分类号 |
F42B10/14 |
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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