发明名称 |
Automatically closable line valve for rocket |
摘要 |
The line valve has a valve body (10) in which a control mechanism for a flap (18) is mounted by holding arms (22,24). This mechanism has a central body (34) containing a cylindrical chamber (32) with control piston (30). The control piston can be fixed in one of two settings by a locking mechanism which has at least one cylinder device (66,68) which releases the locking ball (44,46) from its engagement with a ring (48) by acting on a cylindrical collar (50).
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申请公布号 |
DE19633074(A1) |
申请公布日期 |
1997.02.27 |
申请号 |
DE19961033074 |
申请日期 |
1996.08.16 |
申请人 |
SOCIETE EUROPEENNE DE PROPULSION, SURESNES, FR |
发明人 |
SCHERRER, NORBERT, ST JUST, FR |
分类号 |
F16K1/12;F16K37/00;(IPC1-7):F16K1/18 |
主分类号 |
F16K1/12 |
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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