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1. 发明申请

US20090272840A1 AIRCRAFT FLIGHT TERMINATION SYSTEM AND METHOD 有权
标题翻译：飞机飞行终止系统和方法
公开(公告)号：US20090272840A1
公开(公告)日：2009-11-05
申请号：US12112047
申请日：2008-04-30
申请人： Mark C. Dietrich , Charles N. Trepanier , Timothy R. Werch
发明人： Mark C. Dietrich , Charles N. Trepanier , Timothy R. Werch
IPC分类号： B64C31/02 , F42B3/00 , B64C3/00
CPC分类号： B64C39/024 , B64C1/32 , B64C3/56 , B64C19/00 , F41H11/02 , F42B10/48 , F42B15/36
摘要： An aircraft has a flight termination system that allows flight of an unmanned aircraft to be quickly and efficiently terminated. The flight termination system separates one of the control surfaces of the aircraft, such as a wing, from a fuselage of the aircraft, while one or more other control surfaces connected to the fuselage. The separation may be accomplished by firing one or more explosive bolts to release a clamp that connects the control surface to the fuselage. The separation causes an asymmetry in configuration that results in a rapid crash of the aircraft. The flight termination system causes termination to be effected in small flight footprint, without use of powerful explosives, and without a large cost in weight or volume. The flight termination system may be used in unpowered or powered aircraft.
摘要翻译：一架飞机有一个飞行终端系统，允许无人机的飞行快速有效地终止。飞行终端系统将飞机的诸如机翼的控制表面之一与飞行器的机身分离，同时连接到机身的一个或多个其他控制表面。分离可以通过点火一个或多个爆炸螺栓来释放将控制表面连接到机身的夹具来实现。分离导致配置的不对称性，导致飞机迅速崩溃。飞行终点系统导致终止在小飞行足迹中实现，而不使用强大的爆炸物，并且在重量或体积上没有大的成本。飞行终点系统可用于无动力或动力飞行器。

2. 发明授权

US5785543A High voltage flashlamp connector method and apparatus 失效
标题翻译：高压闪光灯连接器的方法和装置
公开(公告)号：US5785543A
公开(公告)日：1998-07-28
申请号：US566685
申请日：1995-12-04
申请人： Mark C. Dietrich
发明人： Mark C. Dietrich
IPC分类号： H01R13/53 , H01R33/965 , H01R13/52
CPC分类号： H01R13/53 , H01R33/965 , Y10S439/936 , Y10T29/49171 , Y10T29/49176
摘要： A high voltage flashlamp connector includes a housing having a well formed therein intersecting a flashlamp supporting opening and having a female connector positioned in the well and aligned with the intersecting flashlamp opening. An electrical conductor is attached through the well to the female connector and the well is filled with an encapsulate forming a seat for the housing. The method includes forming the outer shell of the apparatus of a glass-filled polyphenylene oxide having a well and a flashlamp insert opening having an annular groove formed therein and attaching a high voltage electrical conductor to the female connector which is placed in the outer shell well positioned within the flashlamp opening, and cleaning the shell surfaces, and filling the shell with an encapsulate with a mold pin positioned in the flashlamp opening, and then inserting an O-ring seal and attaching a flashlamp.
摘要翻译：高压闪光灯连接器包括具有良好形成在其中的壳体，该壳体与闪光灯支撑开口相交并且具有定位在井中并与相交闪光灯开口对准的阴连接器。电导体通过孔连接到阴连接器，并且阱被填充形成用于壳体的座的封装。该方法包括：形成具有孔的装有玻璃的聚苯醚的装置的外壳以及形成有环形槽的闪光灯插入口，并将高压电导体连接到放置在外壳阱中的阴连接器定位在闪光灯开口内，并且清洁壳体表面，并且用封装件填充壳体，模具销定位在闪光灯开口中，然后插入O形密封圈并附接闪光灯。

3. 发明授权

US08037821B2 Methods and apparatus for reducing the transmission of mechanical waves 有权
标题翻译：降低机械波传播的方法和装置
公开(公告)号：US08037821B2
公开(公告)日：2011-10-18
申请号：US12392268
申请日：2009-02-25
申请人： Mark C. Dietrich
发明人： Mark C. Dietrich
IPC分类号： F42D1/055
CPC分类号： F16F15/08 , F16F3/093 , F16F2230/007 , F41H7/042 , F42C19/02
摘要： Methods and apparatus for reducing transmission of mechanical waves according to various aspects of the present invention comprise a set of isolators and a series of stops configured to isolate a piece of equipment in a projectile. The stops serve to limit the amount of stress loading placed on the isolators during transient events where loads associated with launch of the projectile or deployment of flight control surface might damage the isolators or cause the equipment to fail.
摘要翻译：根据本发明的各个方面的用于减少机械波传播的方法和装置包括一组隔离器和一系列停止件，其构造成隔离射弹中的一件设备。这些挡块用于限制在瞬态事件期间放置在隔离器上的应力负载量，其中与发射的弹丸或部署飞行控制表面有关的负载可能会损坏隔离器或导致设备失效。

4. 发明授权

US06505561B1 Method and apparatus for inducing rotation of a dispensed payload from non-spin projectiles 失效
标题翻译：用于从非旋转抛射体引起分配的有效载荷的旋转的方法和装置
公开(公告)号：US06505561B1
公开(公告)日：2003-01-14
申请号：US09843011
申请日：2001-04-25
申请人： Mark C. Dietrich
发明人： Mark C. Dietrich
IPC分类号： F42B1236
CPC分类号： F42B12/62
摘要： A method an apparatus for inducing spin, or rotation, in a dispersed payload of a non-spin guided projectile is taught. Rifling is applied to a cylindrical surface of a projectile casing. The rifling engages a member on a payload, which may be a bulkhead, as the payload is expelled from the projectile casing. The rotation imparted to the payload causes the dispersed projectile, grenades in the preferred embodiment, to form a spiral pattern that provides a more uniform coverage of the target area as compared to the prior art.
摘要翻译：教导了一种用于在非旋转引导射弹的分散载荷中诱导旋转或旋转的装置的方法。步枪应用于射弹套管的圆柱形表面。该膛线与有效载荷上的一个成员接合，有效载荷可能是舱壁，因为有效载荷被从射弹套管排出。与现有技术相比，赋予有效载荷的旋转使得在优选实施例中的分散弹丸，手榴弹形成螺旋图案，其提供目标区域的更均匀的覆盖。

5. 发明授权

US08256716B2 Aircraft flight termination system and method 有权
标题翻译：飞机飞行终止系统及方法
公开(公告)号：US08256716B2
公开(公告)日：2012-09-04
申请号：US12112047
申请日：2008-04-30
申请人： Mark C. Dietrich , Charles N. Trepanier , Timothy R. Werch
发明人： Mark C. Dietrich , Charles N. Trepanier , Timothy R. Werch
IPC分类号： B64C1/06
CPC分类号： B64C39/024 , B64C1/32 , B64C3/56 , B64C19/00 , F41H11/02 , F42B10/48 , F42B15/36
摘要： An aircraft has a flight termination system that allows flight of an unmanned aircraft to be quickly and efficiently terminated. The flight termination system separates one of the control surfaces of the aircraft, such as a wing, from a fuselage of the aircraft, while one or more other control surfaces connected to the fuselage. The separation may be accomplished by firing one or more explosive bolts to release a clamp that connects the control surface to the fuselage. The separation causes an asymmetry in configuration that results in a rapid crash of the aircraft. The flight termination system causes termination to be effected in small flight footprint, without use of powerful explosives, and without a large cost in weight or volume. The flight termination system may be used in unpowered or powered aircraft.
摘要翻译：一架飞机有一个飞行终端系统，允许无人机的飞行快速有效地终止。飞行终端系统将飞机的诸如机翼的控制表面之一与飞行器的机身分离，同时连接到机身的一个或多个其他控制表面。分离可以通过点火一个或多个爆炸螺栓来释放将控制表面连接到机身的夹具来实现。分离导致配置的不对称性，导致飞机迅速崩溃。飞行终点系统导致终止在小飞行足迹中实现，而不使用强大的爆炸物，并且在重量或体积上没有大的成本。飞行终点系统可用于无动力或动力飞行器。

6. 发明申请

US20090289400A1 METHODS AND APPARATUS FOR REDUCING THE TRANSMISSION OF MECHANICAL WAVES 有权
标题翻译：减少机械波传播的方法和装置
公开(公告)号：US20090289400A1
公开(公告)日：2009-11-26
申请号：US12392268
申请日：2009-02-25
申请人： Mark C. Dietrich
发明人： Mark C. Dietrich
IPC分类号： F16F7/00
CPC分类号： F16F15/08 , F16F3/093 , F16F2230/007 , F41H7/042 , F42C19/02
摘要： Methods and apparatus for reducing transmission of mechanical waves according to various aspects of the present invention comprise a set of isolators and a series of stops configured to isolate a piece of equipment in a projectile. The stops serve to limit the amount of stress loading placed on the isolators during transient events where loads associated with launch of the projectile or deployment of flight control surface might damage the isolators or cause the equipment to fail.
摘要翻译：根据本发明的各个方面的用于减少机械波传播的方法和装置包括一组隔离器和一系列停止件，其构造成隔离射弹中的一件设备。这些挡块用于限制在瞬态事件期间放置在隔离器上的应力负载量，其中与发射的弹丸或部署飞行控制表面有关的负载可能会损坏隔离器或导致设备失效。

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