| 发明名称 |
METHOD OF CONTROL OF THRUST VECTOR IN ANNULAR SUPERSONIC NOZZLE AND ANNULAR SUPERSONIC NOZZLE USED FOR REALIZATION OF THIS METHOD |
| 摘要 |
FIELD: aeronautical engineering and rocketry; short takeoff and landing aeroplanes. SUBSTANCE: annular nozzle includes shroud and central body. For control of magnitude and direction of thrust, central body and/or shroud are rotated around axis of nozzle and are shifted axially; shroud and/or central body are provided with stepped cut or with combined stepped and bevel cuts. EFFECT: enhanced reliability. 3 cl, 3 dwg
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| 申请公布号 |
RU2111374(C1) |
申请公布日期 |
1998.05.20 |
| 申请号 |
SU19925062474 |
申请日期 |
1992.09.21 |
| 申请人 |
TSENTRAL'NYJ AEHROGIDRODINAMICHESKIJ INSTITUT IM.P;TSENTRAL NYJ AEHROGIDRODINAMIC |
发明人 |
KEKHVAJANTS V.G.;KEKHVAJANTS V.G. |
| 分类号 |
F02K9/80;(IPC1-7):F02K9/80 |
主分类号 |
F02K9/80 |
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