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1. 发明授权

US08303239B2 Percussive shovel for robotic applications 有权
标题翻译：用于机器人应用的敲击铲
公开(公告)号：US08303239B2
公开(公告)日：2012-11-06
申请号：US12861710
申请日：2010-08-23
申请人： Philip Chu , Jack Wilson , Jack Craft , Kiel Davis
发明人： Philip Chu , Jack Wilson , Jack Craft , Kiel Davis
IPC分类号： E02F3/02 , A01B1/00
CPC分类号： E02F3/966 , B25J15/0019
摘要： A percussive digging tool attachment for a small robotic platform employs a percussor module for applying percussive impulses of relatively low impact at relatively high frequency to an attached digging tool to dig into or break up soil and rocks. By using low-impact, high-frequency percussive forces, it reduces the reaction loads on the small robotic platform while providing increased capability.
摘要翻译：用于小机器人平台的敲击式挖掘工具附件采用冲击模块，用于以相对高的频率将相对低的冲击冲击脉冲施加到附接的挖掘工具以挖掘或分解土壤和岩石。通过使用低冲击，高频冲击力，它可以降低小型机器人平台上的反作用力，同时提供更高的功能。

2. 发明申请

US20120111587A1 PERCUSSIVE SHOVEL FOR ROBOTIC APPLICATIONS 有权
公开(公告)号：US20120111587A1
公开(公告)日：2012-05-10
申请号：US12861710
申请日：2010-08-23
申请人： Philip CHU , Jack Wilson , Jack Craft , Kiel Davis
发明人： Philip CHU , Jack Wilson , Jack Craft , Kiel Davis
IPC分类号： E02F3/42 , A01B35/02
CPC分类号： E02F3/966 , B25J15/0019
摘要： A percussive digging tool attachment for a small robotic platform employs a percussor module for applying percussive impulses of relatively low impact at relatively high frequency to an attached digging tool to dig into or break up soil and rocks. By using low-impact, high-frequency percussive forces, it reduces the reaction loads on the small robotic platform while providing increased capability.
摘要翻译：用于小机器人平台的敲击式挖掘工具附件采用冲击模块，用于以相对高的频率将相对低的冲击冲击脉冲施加到附接的挖掘工具以挖掘或分解土壤和岩石。通过使用低冲击，高频冲击力，它可以降低小型机器人平台上的反作用力，同时提供更高的功能。

3. 发明申请

US20060120869A1 COOLED TURBINE SPAR SHELL BLADE CONSTRUCTION 失效
标题翻译：冷却涡轮叶片叶片结构
公开(公告)号：US20060120869A1
公开(公告)日：2006-06-08
申请号：US10793641
申请日：2004-03-04
申请人： Jack Wilson , Wesley Brown
发明人： Jack Wilson , Wesley Brown
IPC分类号： F01D5/18
CPC分类号： F01D5/147 , F01D5/189 , F01D5/20 , Y10T29/49327 , Y10T29/49339 , Y10T29/49341
摘要： A blade for a rotor of a gas turbine engine is constructed with a spar and shell configuration. The spar is constructed in an integral unit or multi-portions and includes a first wall adjacent to the pressure side and a second wall adjacent to the suction side, a tip portion extending in the spanwise direction and extending beyond the first wall and the second wall and a root portion extending longitudinally, an attachment portion having a central opening for receiving the root portion and a platform portion. The root portion fits into the central opening and is secured therein by a pin extending transversely through the attachment and the root portion. The shell fits over the spar and is supported thereto by a plurality of complementary hooks extending from the spar and shell. The ends of the shell fit into grooves formed on the tip portion and the platform.
摘要翻译：用于燃气涡轮发动机的转子的叶片由翼梁和壳体构造构成。翼梁构造成整体单元或多部分，并且包括邻近压力侧的第一壁和邻近吸力侧的第二壁，尖端部分沿翼展方向延伸并且延伸超出第一壁和第二壁和根部，其纵向延伸，具有用于接收根部的中心开口和平台部分的附接部分。根部装配到中央开口中并且通过横向穿过附件和根部部分的销固定在其中。壳体装配在翼梁上，并由多个从翼梁和壳体延伸的互补钩支撑在其上。壳体的端部装配到形成在尖端部分和平台上的凹槽中。

4. 发明授权

US4249141A Laser systems using pentaphosphate active mediums 失效
标题翻译：使用五磷酸盐活性介质的激光系统
公开(公告)号：US4249141A
公开(公告)日：1981-02-03
申请号：US913920
申请日：1978-06-08
申请人： David C. Brown , Jack Wilson
发明人： David C. Brown , Jack Wilson
IPC分类号： H01S3/16
CPC分类号： H01S3/16
摘要： Laser systems in which efficiency and high repetition rate operation are obtained utilize an active laser medium consisting of pentaphosphate with high concentration doping of a rare earth such as neodymium and a pumping means in optical contact with the active medium which produces pump radiation confined to a band which essentially overlaps the absorption band of the laser medium. An active mirror configuration is described with thin layer of pentaphosphate active medium on one side of a substrate which is transmissive to the pump radiation. The pump radiation is provided by an excimer laser or by a semiconductor converter layer which is excited by flash lamps. The laser medium may be segmented with the space between segments occupied by material absorptive of amplified spontaneous emission wavelengths. The laser system is especially useful in laser fusion systems.
摘要翻译：获得效率和高重复率操作的激光系统利用由五磷酸盐组成的活性激光介质，其中高浓度掺杂稀土如钕，以及与活性介质光学接触的泵送装置，该活性介质产生限制在带其基本上与激光介质的吸收带重叠。在衬底的一侧上用磷光体活性介质的薄层描述有源反射镜结构，其对泵浦辐射是透射的。泵浦辐射由准分子激光器或被闪光灯激发的半导体转换器层提供。激光介质可以被被放大的自发发射波长吸收的材料所占据的部分之间的空间分段。激光系统在激光融合系统中特别有用。

5. 发明授权

US09835171B2 Vane carrier assembly 有权
公开(公告)号：US09835171B2
公开(公告)日：2017-12-05
申请号：US12859904
申请日：2010-08-20
申请人： Keith D. Kimmel , Jack Wilson
发明人： Keith D. Kimmel , Jack Wilson
IPC分类号： F01D9/04 , F01D25/26 , F04D29/54 , F01D11/18 , F01D25/24
CPC分类号： F04D29/541 , F01D9/041 , F01D11/18 , F01D25/246 , F01D25/26 , F04D29/542
摘要： A vane carrier assembly is provided for supporting vanes within a main engine casing of a gas turbine engine. The vane carrier assembly comprises a plurality of vane support panels positioned adjacent to one another so as to define a vane support assembly. The support panels are assembled such that the support panels expand circumferentially to minimize radial expansion of the vane support assembly during operation of the gas turbine engine. A control ring is coupled to the main engine casing, and the vane support assembly is coupled to the control ring. The control ring may be formed from a material having a coefficient of thermal expansion less than that of the material from which the vane support assembly is formed.

6. 发明申请

US20060249912A1 Segmented air floating seal 审中-公开
标题翻译：分段空气浮动密封
公开(公告)号：US20060249912A1
公开(公告)日：2006-11-09
申请号：US11183275
申请日：2005-07-15
申请人： Jack Wilson
发明人： Jack Wilson
IPC分类号： F16J15/44
CPC分类号： F16J15/442
摘要： A segmented floating seal assembly used in a gas turbine engine to seal a rotary shaft. The segmented seal is made from a fiber reinforced ceramic matrix composite (FRCMC) material having a polymer-derived pre-ceramic resin in its ceramic state, fibers of Nextel, and a filler material. The seal segments are secured to respective support plates, and the support plates are each biased by a spring member secured to a support ring mounted in the engine. The material in the seal segments are resistive to very high temperatures, are not brittle, allow little flow across the seal face, and durable.
摘要翻译：用于燃气涡轮发动机以密封旋转轴的分段浮动密封组件。分段密封由具有其陶瓷状态的聚合物衍生的预陶瓷树脂，Nextel的纤维和填充材料的纤维增强陶瓷基复合材料（FRCMC）材料制成。密封段被固定到相应的支撑板上，并且支撑板各自被固定到安装在发动机中的支撑环上的弹簧构件偏压。密封段中的材料对非常高的温度具有阻力，不易脆，允许几乎没有流过密封面的流动并且耐用。

7. 再颁专利

USRE29103E Nitrogen laser action with supersonic flow 失效
标题翻译：激素激光作用与超音速流动
公开(公告)号：USRE29103E
公开(公告)日：1977-01-04
申请号：US309126
申请日：1972-11-24
申请人： Jack Wilson , Arthur R. Kantrowitz
发明人： Jack Wilson , Arthur R. Kantrowitz
IPC分类号： H01S3/0979
CPC分类号： H01S3/0979
摘要： Lasing action is electrically induced in a supersonic flow of nitrogen gas, resulting in an increase in pulse repetition rate to a new order.

8. 外观设计

USD711162S1 Cap and armrest cover 有权
标题翻译：盖帽和扶手盖
公开(公告)号：USD711162S1
公开(公告)日：2014-08-19
申请号：US29436250
申请日：2012-11-02
申请人： Jack Wilson , Brian Hall
设计人： Jack Wilson , Brian Hall

9. 发明申请

US20080084030A1 Segmented air floating seal 审中-公开
标题翻译：分段空气浮动密封
公开(公告)号：US20080084030A1
公开(公告)日：2008-04-10
申请号：US11998368
申请日：2007-11-29
申请人： Jack Wilson
发明人： Jack Wilson
IPC分类号： F16J15/40
CPC分类号： F16J15/442 , F01D25/22 , F16J15/445 , F16J15/453
摘要： A segmented floating seal assembly used in a gas turbine engine to seal a rotary shaft. The segmented seal is made from a fiber reinforced ceramic matrix composite (FRCMC) material having a polymer-derived pre-ceramic resin in its ceramic state, fibers of Nextel, and a filler material. The seal segments are secured to respective support plates, and the support plates are each biased by a spring member secured to a support ring mounted in the engine. The material in the seal segments are resistive to very high temperatures, are not brittle, allow little flow across the seal face, and durable. The segmented seal includes holes in either the segments or the rotary shaft in which pressurized air is supplied to the seal interface to form an air cushion on which the seal segments can float.
摘要翻译：用于燃气涡轮发动机以密封旋转轴的分段浮动密封组件。分段密封由具有其陶瓷状态的聚合物衍生的预陶瓷树脂，Nextel的纤维和填充材料的纤维增强陶瓷基复合材料（FRCMC）材料制成。密封段被固定到相应的支撑板上，并且支撑板各自被固定到安装在发动机中的支撑环上的弹簧构件偏压。密封段中的材料对非常高的温度具有阻力，不易脆，允许几乎没有流过密封面的流动并且耐用。分段密封件包括分段或旋转轴中的孔，其中加压空气供应到密封接口以形成气垫，密封段可以浮动在该气垫上。

10. 发明授权

US07174797B2 High temperature and pressure testing facility 有权
标题翻译：高温高压试验设备
公开(公告)号：US07174797B2
公开(公告)日：2007-02-13
申请号：US10685339
申请日：2003-10-14
申请人： Joseph Brostmeyer , Jack Wilson , Todd A. Ebert
发明人： Joseph Brostmeyer , Jack Wilson , Todd A. Ebert
IPC分类号： G01N33/00
CPC分类号： G01N25/00 , G01M15/14 , G01M99/002 , G01N3/18 , G01N17/002 , G01N2203/0042 , G01N2203/0057 , G01N2203/0226 , G01N2203/0232
摘要： A test facility is provided for testing materials under high temperature, pressure, and mechanical loads. The facility provides a physically scaled system that simulates conditions in hot sections of gas turbine engines. A test article is coated with a test material and exposed to a hot combusting flow in a test section housing. The article may be a pipe or conduit member oriented at any direction to the flow. A second cooler flow of fluid is channeled through the test article to create a sharp temperature gradient in the test article and through the test material. A liquid-cooled sleeve is disposed about the test article to create an annular channel of combusting flow over the test article. The downstream end of the second cooler flow is connected to the upstream end of the main hot flow at the combustion chamber.
摘要翻译：提供测试设备用于在高温，高压和机械负载下测试材料。该设施提供了一个物理尺度的系统，可模拟燃气轮机发动机热段的状况。测试物品涂覆有测试材料并暴露于测试部分壳体中的热燃烧流。制品可以是在流动的任何方向上定向的管道或管道构件。流体的第二个较冷的流动通过测试物品，以在测试物品和测试材料中产生尖锐的温度梯度。液体冷却的套筒围绕测试物品设置，以产生在测试物品上燃烧的环形通道。第二冷却器流的下游端连接到燃烧室的主热流的上游端。

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