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1. 发明授权

US06536350B2 Stagnation pressure activated fuel release mechanism for hypersonic projectiles 有权
公开(公告)号：US06536350B2
公开(公告)日：2003-03-25
申请号：US09799572
申请日：2001-03-07
申请人： Harry E. Cartland , John W. Hunter
发明人： Harry E. Cartland , John W. Hunter
IPC分类号： F42B1500
CPC分类号： F42B15/10 , F02K7/10
摘要： A propulsion-assisted projectile has a body, a cowl forming a combustion section and a nozzle section. The body has a fuel reservoir within a central portion of the body, and a fuel activation system located along the central axis of the body and having a portion of the fuel activation system within the fuel reservoir. The fuel activation system has a fuel release piston with a forward sealing member where the fuel release piston is adapted to be moved when the forward sealing member is impacted with an air flow, and an air-flow channel adapted to conduct ambient air during flight to the fuel release piston.

2. 外观设计

USD476533S1 Insulated container 失效
公开(公告)号：USD476533S1
公开(公告)日：2003-07-01
申请号：US29165988
申请日：2002-08-20
申请人： John W. Hunter
设计人： John W. Hunter

3. 发明授权

US5970970A Ring airfoil launcher 失效
标题翻译：环形翼型发射器
公开(公告)号：US5970970A
公开(公告)日：1999-10-26
申请号：US10431
申请日：1998-01-21
申请人： Chester F. Vanek , John W. Hunter , Abraham Flatau , Thomas H. Grimm , Sung H. Kim , Robert B. Brownell, Jr. , William S. Law , Mark C. Sorensen
发明人： Chester F. Vanek , John W. Hunter , Abraham Flatau , Thomas H. Grimm , Sung H. Kim , Robert B. Brownell, Jr. , William S. Law , Mark C. Sorensen
IPC分类号： F41B7/00 , F42B10/36
CPC分类号： F42B10/36 , F41B7/003
摘要： Toys and methods for safely and reproducibly launching ring airfoils in a flying orientation. The toys generally comprise a member, a ring airfoil support mounted on the member, and a propelling element configured to move the ring airfoil support along the member from a first to a second position. Contact between the ring airfoil and the ring airfoil support causes the ring airfoil to move with the ring airfoil support as the ring airfoil support moves; this contact is overcome as the ring airfoil support decelerates at the second position, causing the ring airfoil to be launched with forward or both forward and spinning motion. The toys further may comprise a housing to protect the toy and user, a return element to place the toy in an engaged, launch-ready configuration, and a trigger to hold the toy in the engaged configuration until launching. As an additional aspect of the invention, components of the device may be chosen so that the characteristics of the ring airfoil at launch are within certain safety limitations.
摘要翻译：用于安全和可重复地以飞行方向发射环形翼型的玩具和方法。玩具通常包括构件，安装在构件上的环形翼型件支撑件和构造成沿着构件将环形翼型件支撑件从第一位置移动到第二位置的推进元件。环形翼型件和环形翼片支架之间的接触使得环形翼型件随着环形翼型件支撑件移动而与环形翼片支撑件一起移动; 当环形翼型件支撑在第二位置减速时，克服了这种接触，导致环形翼片向前或向前或向前和旋转运动。玩具还可以包括用于保护玩具和使用者的壳体，用于将玩具置于接合的发射准备配置中的返回元件以及将玩具保持在接合配置中直到发射的触发器。作为本发明的另一方面，可以选择装置的部件，使得发射时的环形翼型件的特性在某些安全限制之内。

4. 外观设计

USD513018S1 Refrigerant package 失效
标题翻译：制冷剂包装
公开(公告)号：USD513018S1
公开(公告)日：2005-12-20
申请号：US29201738
申请日：2004-03-19
申请人： John W. Hunter
设计人： John W. Hunter

5. 外观设计

USD427490S Surface configuration for an insulated container 失效
公开(公告)号：USD427490S
公开(公告)日：2000-07-04
申请号：US99784
申请日：1999-01-27
申请人： John W. Hunter
设计人： John W. Hunter

6. 发明授权

US09019375B1 Target locator and interceptor imaging and sensing assembly, system and method 有权
标题翻译：目标定位器和拦截器成像和感测装配，系统和方法
公开(公告)号：US09019375B1
公开(公告)日：2015-04-28
申请号：US13545978
申请日：2012-07-10
申请人： David A. Whelan , John W. Hunter
发明人： David A. Whelan , John W. Hunter
IPC分类号： H04N7/18 , G01C23/00 , G01C11/02
CPC分类号： G01C23/00 , F41A1/00 , F41A9/64 , F41A21/16 , F41B11/54 , F41F7/00 , F41G3/02 , F41G3/22 , F41G7/226 , F41G7/2293 , F41G7/30 , F41G7/346 , F42B10/26 , F42B12/365 , F42B15/08 , G01C11/02
摘要： There is provided in one embodiment a target locator and interceptor imaging and sensing assembly. The assembly has a disc shaped aerodynamic member configured to spin and self-position in flight, a plurality of pulsed thrusters positioned on the member, and a plurality of imaging and sensing devices positioned along a perimeter of the member. The assembly further has one or more munitions devices coupled to one or more detonators, both being coupled to the aerodynamic member. The assembly further has one or more antenna devices positioned on the member and in communication with a first processor device on the member. The first processor device receives data obtained by the plurality of imaging and sensing devices and wirelessly transmits the data to a second processor device not positioned on the member. The assembly further has a power supply powering the assembly.
摘要翻译：在一个实施例中提供了目标定位器和拦截器成像和感测组件。组件具有被配置为在飞行中旋转和自动定位的盘形空气动力学构件，定位在构件上的多个脉冲推进器和沿着构件的周边定位的多个成像和感测装置。组件还具有联接到一个或多个雷管的一个或多个弹药装置，二者都联接到空气动力学构件。组件还具有位于构件上并与构件上的第一处理器装置通信的一个或多个天线装置。第一处理器设备接收由多个成像和感测设备获得的数据，并且将数据无线传输到不位于该成员上的第二处理器设备。组件还具有为组件供电的电源。

7. 外观设计

USD466372S1 Insulated container 失效
标题翻译：绝缘容器
公开(公告)号：USD466372S1
公开(公告)日：2002-12-03
申请号：US29150307
申请日：2001-11-20
申请人： John W. Hunter
设计人： John W. Hunter

8. 发明授权

US09204104B1 Imaging and sensing assembly, system and method 有权
标题翻译：成像和感测装配，系统和方法
公开(公告)号：US09204104B1
公开(公告)日：2015-12-01
申请号：US13545973
申请日：2012-07-10
申请人： David A. Whelan , John W. Hunter
发明人： David A. Whelan , John W. Hunter
IPC分类号： H04N7/18
CPC分类号： H04N7/18 , B64D47/08 , H04N7/185
摘要： There is provided in one embodiment an imaging and sensing assembly. The imaging and sensing assembly has a disc shaped aerodynamic member configured to spin and self-position in flight, a plurality of pulsed thrusters positioned on the member, and a plurality of imaging and sensing devices positioned along a perimeter of the member. The imaging and sensing assembly further has one or more antenna devices positioned on the member and in communication with a first processor device on the member. The first processor device receives data obtained by the plurality of imaging and sensing devices and wirelessly transmits the data to a second processor device not positioned on the member. The imaging and sensing assembly further has a power supply powering the imaging and sensing assembly.
摘要翻译：在一个实施例中提供了一种成像和感测组件。成像和感测组件具有被配置为在飞行中旋转和自动定位的盘形空气动力学构件，定位在构件上的多个脉冲推进器和沿着构件的周边定位的多个成像和感测装置。成像和感测组件还具有位于构件上并与构件上的第一处理器装置通信的一个或多个天线装置。第一处理器设备接收由多个成像和感测设备获得的数据，并且将数据无线传输到不位于该成员上的第二处理器设备。成像和感测组件还具有为成像和感测组件供电的电源。

9. 发明授权

US08247685B2 Solar energy harvesting apparatus 有权
标题翻译：太阳能收割机
公开(公告)号：US08247685B2
公开(公告)日：2012-08-21
申请号：US11644674
申请日：2006-12-22
申请人： John W. Hunter , Philip Sluder
发明人： John W. Hunter , Philip Sluder
IPC分类号： H01L31/00 , H01L31/042
CPC分类号： H02S20/00 , F24S30/425 , F24S80/70 , H01L31/0547 , Y02E10/47 , Y02E10/52
摘要： A solar energy harvesting apparatus is disclosed. An illustrative embodiment of the apparatus includes a generally elongated, rectangular body having a bottom portion and sidewalls extending from the bottom portion; at least one trough provided in the bottom portion and having a trough base and trough peaks; at least one mirror strip provided along at least one peak of the at least one trough; and a linear solar cell provided along the trough base of the at least one trough.
摘要翻译：公开了一种太阳能收集装置。该装置的说明性实施例包括大致细长的矩形主体，其具有底部和从底部延伸的侧壁; 至少一个槽设置在底部并具有槽底和槽顶; 至少一个镜带，沿着所述至少一个槽的至少一个峰提供; 以及沿着所述至少一个槽的槽底设置的线性太阳能电池。

10. 外观设计

USD522070S1 Ring airfoil launching system and components thereof 失效
标题翻译：环形翼型发射系统及其部件
公开(公告)号：USD522070S1
公开(公告)日：2006-05-30
申请号：US29186818
申请日：2003-07-22
申请人： John W. Hunter , Robert M. Fryer , Philip J. Sluder , Robert A. Rauch , Steve Sramek
设计人： John W. Hunter , Robert M. Fryer , Philip J. Sluder , Robert A. Rauch , Steve Sramek

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