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).
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 代理人
主权项
地址