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1. 发明专利

BR7000033U 未知
公开(公告)号：BR7000033U
公开(公告)日：1991-08-06
申请号：BR7000033
申请日：1990-01-04
申请人： THOMAS MICHAEL LEAL
发明人： LEAL THOMAS MICHAEL
IPC分类号： A63H15/00

2. 发明专利

NL7909014A Sand salt content reduction system - delivers water with low salt concentration into mass after which draining takes place 未知
公开(公告)号：NL7909014A
公开(公告)日：1980-06-17
申请号：NL7909014
申请日：1979-12-14
申请人： JOHN MICHAEL LEAL UREN
IPC分类号： B01D11/02 , B03B5/00 , C04B14/06
摘要： The system reduces the salt content of sand by adding water with a relatively low concn. of dissolved salts. The water is delivered into the spaces in a mass of sand contg. soluble salts so as to fill them almost completely, after which they are emptied by draining the water away, this taking the salt in the sand with it. The water can be delivered as a layer onto the top of the sand, so as to sink through it. The system is partic. for use when dredging from the seabed.

3. 发明申请

US20060284006A1 MISSILE CONTROL SYSTEM AND METHOD 有权
标题翻译： MISSILE控制系统和方法
公开(公告)号：US20060284006A1
公开(公告)日：2006-12-21
申请号：US11113511
申请日：2005-04-25
申请人： Daniel Chasman , Michael Leal , Stephen Haight
发明人： Daniel Chasman , Michael Leal , Stephen Haight
IPC分类号： B64B1/36
CPC分类号： F42B10/666 , F02K9/30 , F02K9/805 , F02K9/86 , F05D2240/128 , F05D2250/323 , F05D2250/324 , F05D2250/41 , F05D2260/60 , F16K3/085 , F42B10/663
摘要： A missile includes a control system having divert and attitude control system thrusters with control valves. Each of the control valves has a nozzle plate having a plurality of small nozzles therein. The nozzle plate includes a pair of portions, one of which is rotatable relative to the other. Control of flow through the nozzle plate may be effected by relative positioning of the portions of the nozzle plate. An upstream convergent portion of the nozzle plate may be fixed relative to the missile, with a downstream throat and/or divergent portion of the nozzle plate moveable. Movement of the movable portion of the nozzle plate may be accomplished by use of an actuator that is external to the missile body. The control valve provides a simple, lightweight and compact way of controlling flow from a divert thruster.
摘要翻译：导弹包括具有转向和姿态控制系统推进器的控制系统，其具有控制阀。每个控制阀具有在其中具有多个小喷嘴的喷嘴板。喷嘴板包括一对部分，其中一个部分可相对于另一个部分旋转。通过喷嘴板的流动的控制可以通过喷嘴板的部分的相对定位来实现。喷嘴板的上游收敛部分可以相对于导弹固定，喷嘴板的下游喉部和/或发散部分可移动。可以通过使用在导弹体外部的致动器来实现喷嘴板的可移动部分的移动。控制阀提供了一种控制来自转向推进器的流量的简单，轻便和紧凑的方式。

4. 发明申请

US20080093498A1 Multiple Kill Vehicle (MKV) Interceptor with Autonomous Kill Vehicles 有权
标题翻译：具有自主杀伤车辆的多重杀伤车辆（MKV）拦截器
公开(公告)号：US20080093498A1
公开(公告)日：2008-04-24
申请号：US11678456
申请日：2007-02-23
申请人： Michael Leal , Todd Baker , Kent Pflibsen
发明人： Michael Leal , Todd Baker , Kent Pflibsen
IPC分类号： F41G7/20
CPC分类号： F41G7/2233 , F41G3/04 , F41G7/2206 , F41G7/308 , F42B12/58
摘要： The present invention provides a MKV interceptor including multiple kill vehicles with autonomous management capability and kinematic reach to prosecute a large threat extent. Each KV can self-manage its own KV deployment and target engagement for a determined target volume assigned by a designated master KV. At least one KV is master capable of managing the post-separation of all of the KVs without requiring updates to the mission plan post-separation. The autonomous capability and increased kinematic reach provides for a more efficient use of boosters and more effective engagement of the threat.
摘要翻译：本发明提供一种MKV拦截器，包括具有自主管理能力和运动触觉的多个杀伤车辆，以起诉较大的威胁程度。每个KV可以自行管理自己的KV部署，并针对由指定的主KV分配的确定的目标卷进行目标参与。至少有一名KV是能够管理所有KV的分离后的主人，而不需要更新任务计划后分离。自主能力和增加的运动能力达到更有效地使用助推器并更有效地参与威胁。

5. 发明授权

US07287725B2 Missile control system and method 有权
标题翻译：导弹控制系统及方法
公开(公告)号：US07287725B2
公开(公告)日：2007-10-30
申请号：US11113511
申请日：2005-04-25
申请人： Daniel B. Chasman , Michael Leal , Stephen D. Haight
发明人： Daniel B. Chasman , Michael Leal , Stephen D. Haight
IPC分类号： B64C1/24
CPC分类号： F42B10/666 , F02K9/30 , F02K9/805 , F02K9/86 , F05D2240/128 , F05D2250/323 , F05D2250/324 , F05D2250/41 , F05D2260/60 , F16K3/085 , F42B10/663
摘要： A missile includes a control system having divert and attitude control system thrusters with control valves. Each of the control valves has a nozzle plate having a plurality of small nozzles therein. The nozzle plate includes a pair of portions, one of which is rotatable relative to the other. Control of flow through the nozzle plate may be effected by relative positioning of the portions of the nozzle plate. An upstream convergent portion of the nozzle plate may be fixed relative to the missile, with a downstream throat and/or divergent portion of the nozzle plate moveable. Movement of the movable portion of the nozzle plate may be accomplished by use of an actuator that is external to the missile body. The control valve provides a simple, lightweight and compact way of controlling flow from a divert thruster.
摘要翻译：导弹包括具有转向和姿态控制系统推进器的控制系统，其具有控制阀。每个控制阀具有在其中具有多个小喷嘴的喷嘴板。喷嘴板包括一对部分，其中一个部分可相对于另一个部分旋转。通过喷嘴板的流动的控制可以通过喷嘴板的部分的相对定位来实现。喷嘴板的上游收敛部分可以相对于导弹固定，喷嘴板的下游喉部和/或发散部分可移动。可以通过使用在导弹体外部的致动器来实现喷嘴板的可移动部分的移动。控制阀提供了一种控制来自转向推进器的流量的简单，轻便和紧凑的方式。

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