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1. 发明公开

EP0060726A2 Gas thruster systems 失效
标题翻译： Strahltrieb-Schubsysteme。
公开(公告)号：EP0060726A2
公开(公告)日：1982-09-22
申请号：EP82301351.1
申请日：1982-03-16
申请人： NORMALAIR-GARRETT (HOLDINGS) LIMITED
发明人： Young, Robert William
IPC分类号： F42B15/18 , F02K9/88
CPC分类号： F42B10/663 , F02K9/88
摘要： A gas thruster system particularly suited for use in controlling the flight of an aerial projectile, has self-centering valve means controlling the exhaust of gas from a pair of oppositely directed exhaust nozzles. Actuating means, which may comprise a pair of solenoids, are adapted for cooperation with the valve means and, in operation, shift the valve means to either side of a null central position towards closing one or the other of the pair of nozzles to provide differential gas flow from the pair of nozzles whilst maintaining a substantially constant area vent from a gas source.
摘要翻译：特别适用于控制空中弹药飞行的气体推进器系统具有自动对中阀装置，其控制来自一对相反方向的排气喷嘴的气体排气。可以包括一对螺线管的致动装置适于与阀装置协作，并且在操作中，将阀装置移动到零中心位置的任一侧以朝向闭合一对或另一个喷嘴以提供差分气体从一对喷嘴流出，同时保持与气体源基本恒定的区域通气口。

2. 发明公开

EP0069440A3 Gas thruster device 失效
标题翻译：气体脉动装置
公开(公告)号：EP0069440A3
公开(公告)日：1983-03-16
申请号：EP82301896
申请日：1982-04-08
申请人： NORMALAIR-GARRETT (HOLDINGS) LIMITED
发明人： Young, Robert William
IPC分类号： F02K09/88 , F42B15/18
CPC分类号： F42B10/666 , F02K9/80 , F02K9/84
摘要： A gas thruster device has a body portion housing at least one pair of rotatable nozzle assemblies for discharging gas to control, for example, the flight of a small calibre aerial body. Each nozzle assembly comprises a duct member extending substantially parallel with the longitudinal axis of the body portion and a thrust nozzle connected with one end of the duct so as to extend substantially normal thereto. The duct member is adapted at its other end to receive gas from a gas source and is mounted in the body portion for rotation about its own axis. Means are provided for rotating each nozzle assembly about the axis of its duct member to vary the direction of gas discharged from its thrust nozzle.
摘要翻译：气体推进器装置具有容纳至少一对可旋转喷嘴组件的主体部分，用于排放气体以控制例如小口径天体的飞行。每个喷嘴组件包括基本上平行于主体部分的纵向轴线延伸的管道部件和与管道的一端连接的推力喷嘴，以便与其基本正交地延伸。管道构件在其另一端适于接收来自气源的气体，并且安装在主体部分中以围绕其自身的轴线旋转。提供了用于使每个喷嘴组件围绕其管道构件的轴线旋转以改变从其推力喷嘴排出的气体的方向的装置。

3. 发明公开

EP0069440A2 Gas thruster device 失效
标题翻译： Einrichtung zum Erzeugen eines Gas-Schubkraft。
公开(公告)号：EP0069440A2
公开(公告)日：1983-01-12
申请号：EP82301896.5
申请日：1982-04-08
申请人： NORMALAIR-GARRETT (HOLDINGS) LIMITED
发明人： Young, Robert William
IPC分类号： F02K9/88 , F42B15/18
CPC分类号： F42B10/666 , F02K9/80 , F02K9/84
摘要： A gas thruster device has a body portion housing at least one pair of rotatable nozzle assemblies for discharging gas to control, for example, the flight of a small calibre aerial body. Each nozzle assembly comprises a duct member extending substantially parallel with the longitudinal axis of the body portion and a thrust nozzle connected with one end of the duct so as to extend substantially normal thereto. The duct member is adapted at its other end to receive gas from a gas source and is mounted in the body portion for rotation about its own axis. Means are provided for rotating each nozzle assembly about the axis of its duct member to vary the direction of gas discharged from its thrust nozzle.
摘要翻译：气体推进器装置具有容纳至少一对可旋转喷嘴组件的主体部分，用于排放气体以控制例如小口径天体的飞行。每个喷嘴组件包括基本上平行于主体部分的纵向轴线延伸的管道部件和与管道的一端连接的推力喷嘴，以便与其基本正交地延伸。管道构件在其另一端适于接收来自气源的气体，并且安装在主体部分中以围绕其自身的轴线旋转。提供了用于使每个喷嘴组件围绕其管道构件的轴线旋转以改变从其推力喷嘴排出的气体的方向的装置。

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