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1. 发明授权

US4813496A Drill ahead tool 失效
标题翻译：向前钻工具
公开(公告)号：US4813496A
公开(公告)日：1989-03-21
申请号：US200890
申请日：1988-06-01
申请人： David J. Rohweller , Joseph W. Pallini, Jr.
发明人： David J. Rohweller , Joseph W. Pallini, Jr.
IPC分类号： E21B7/128 , E21B7/20 , E21B7/124
CPC分类号： E21B7/128 , E21B7/208
摘要： A drill ahead tool for drilling the initial portion of a subsea well allows an operator to drill ahead after running conductor pipe. The running tool locates in the wellhead housing secured to the upper end of the string of conductor pipe. The running tool has a mandrel that connects into the string of drill pipe. The mandrel locates in a sleeve. The sleeve locates in a body of the running tool. The body has dogs which engage a groove in the wellhead housing to secure the running tool to the wellhead housing while the conductor pipe is being run. The sleeve has a cam on its exterior for maintaining the dogs in the extended position. The drill pipe rotates the sleeve to advance the cam to allow the dogs to be retracted. The mandrel and sleeve have a J-slot and pin that allow the mandrel to be released from the sleeve to continue drilling ahead.
摘要翻译：用于钻探海底井的初始部分的钻头工具允许操作者在运行导管之后向前钻。运行工具位于固定到导线管的上端的井口外壳中。运行工具具有连接到钻杆系列中的心轴。心轴位于套筒中。套管位于运行工具的主体内。主体具有在井口壳体中接合凹槽的狗，以在导管正在运行时将运行的工具固定到井口壳体。套筒在其外部具有凸轮，用于将狗保持在延伸位置。钻杆旋转套筒以推进凸轮以允许狗缩回。心轴和套筒具有J形槽和销，其允许心轴从套筒释放以继续向前钻孔。

2. 发明授权

US4603886A Snap type pipe connector 失效
标题翻译：卡扣型管接头
公开(公告)号：US4603886A
公开(公告)日：1986-08-05
申请号：US592508
申请日：1984-03-26
申请人： Joseph W. Pallini, Jr. , David J. Rohweller
发明人： Joseph W. Pallini, Jr. , David J. Rohweller
IPC分类号： E21B17/08 , F16L37/088 , F16L55/00
CPC分类号： E21B17/085 , F16L37/088
摘要： A snap type pin and box connector. A plurality of box diameters 24, 28, 32 interact with a plurality of pin diameters 36, 40, 44, 48 and 50 to produce a minimum clearance at an intermediate location 28, 44. The box load shoulder 56 is chamfered 54, as is a portion K of the split lock ring 14 adjacent to the split.
摘要翻译：卡扣式销和盒式连接器。多个盒直径24,28,32与多个销直径36,40,44,48和50相互作用，以在中间位置28,44处产生最小间隙。盒装载肩56被倒角54 分裂锁定环14的与分割相邻的部分K.

3. 发明授权

US08970447B2 Deployable helical antenna for nano-satellites 有权
标题翻译：用于纳米卫星的可部署螺旋天线
公开(公告)号：US08970447B2
公开(公告)日：2015-03-03
申请号：US13564393
申请日：2012-08-01
申请人： Daniel J. Ochoa , Geoffrey W. Marks , David J. Rohweller
发明人： Daniel J. Ochoa , Geoffrey W. Marks , David J. Rohweller
IPC分类号： H01Q11/08 , H01Q1/28 , H01Q1/12 , H01Q1/36
CPC分类号： H01Q1/1235 , H01Q1/288 , H01Q1/362 , H01Q11/086
摘要： A helical antenna operable to be stowed on and deployed from a cubesat. The antenna includes two helical elements wound in opposite directions and defining an antenna column, where one of the helical elements is a conductive antenna element. The antenna also includes a plurality of circumferentially disposed vertical stiffeners extending along a length of the column and being coupled to the helical elements at each location where the vertical stiffeners and the helical elements cross. The helical elements and the vertical stiffeners are formed of a flexible material, such as a fiber glass, so that the antenna can be collapsed and stowed into a relatively small space. To position the antenna in the stowed configuration, the vertical stiffeners are folded on each other in a radial direction, and then the folded antenna is rolled in an axial direction from one end of the column to the other end.
摘要翻译：螺旋天线可操作地被存放在立方体上并展开。天线包括沿相反方向缠绕的两个螺旋形元件，并且限定天线柱，其中一个螺旋元件是导电天线元件。天线还包括沿着柱的长度延伸的多个周向设置的垂直加强件，并且在垂直加强件和螺旋元件交叉的每个位置处联接到螺旋元件。螺旋元件和垂直加强件由柔性材料（例如玻璃纤维）形成，使得天线能够收缩并收纳在较小的空间中。为了将天线放置在收起的构造中，垂直扶强件在径向方向上彼此折叠，然后折叠的天线在从柱的一端到另一端的轴向方向上滚动。

4. 发明授权

US08167247B2 Space-based occulter 有权
标题翻译：基于空间的遮罩
公开(公告)号：US08167247B2
公开(公告)日：2012-05-01
申请号：US12754293
申请日：2010-04-05
申请人： Dean R. Daily , David J. Rohweller , Tiffany Glassman
发明人： Dean R. Daily , David J. Rohweller , Tiffany Glassman
IPC分类号： B64G1/22
CPC分类号： G02B26/02 , G02B5/005
摘要： A space-based occulter is selectively movable between stowed and deployed configurations. A base hub has a longitudinally oriented center axis. A plurality of petals are provided, each petal extending radially outward from, and spaced radially apart from, the base hub when in the deployed configuration. Each petal has a hypergaussian edge made up of a plurality of hypergaussian edge panels. Each hypergaussian edge panel defines a portion of the hypergaussian edge of the petal. Each hypergaussian edge panel is made substantially of a material having a near zero coefficient of thermal expansion. A circular central portion is located radially between the base hub and the plurality of petals. A covering skin extends laterally between the hypergaussian edges of each petal and over the circular central portion. The covering skin defines a substantially planar surface oriented substantially perpendicular to the center axis when the occulter is in the deployed configuration.
摘要翻译：基于空间的遮罩可以在收起和展开的配置之间选择性地移动。基座毂具有纵向定向的中心轴线。设置多个花瓣，当处于展开构型时，每个花瓣从基座毂径向向外延伸并与其径向分开。每个花瓣具有由多个超高斯边缘面板组成的超高斯边缘。每个超高斯边缘面板定义花瓣的超高斯边缘的一部分。每个超高斯边缘面板基本上由具有接近零热膨胀系数的材料制成。圆形中心部分径向地位于基座毂和多个花瓣之间。覆盖皮肤横向延伸在每个花瓣的超高边缘之间并且在圆形中心部分上方。覆盖皮肤限定了当遮罩处于展开构型时基本上垂直于中心轴线定向的基本平坦的表面。

5. 发明申请

US20110242663A1 SPACE-BASED OCCULTER 有权
标题翻译：基于空间的分析仪
公开(公告)号：US20110242663A1
公开(公告)日：2011-10-06
申请号：US12754293
申请日：2010-04-05
申请人： Dean R. Daily , David J. Rohweller , Tiffany Glassman
发明人： Dean R. Daily , David J. Rohweller , Tiffany Glassman
IPC分类号： G02B7/00 , G02B27/00
CPC分类号： G02B26/02 , G02B5/005
摘要： A space-based occulter is selectively movable between stowed and deployed configurations. A base hub has a longitudinally oriented center axis. A plurality of petals are provided, each petal extending radially outward from, and spaced radially apart from, the base hub when in the deployed configuration. Each petal has a hypergaussian edge made up of a plurality of hypergaussian edge panels. Each hypergaussian edge panel defines a portion of the hypergaussian edge of the petal. Each hypergaussian edge panel is made substantially of a material having a near zero coefficient of thermal expansion. A circular central portion is located radially between the base hub and the plurality of petals. A covering skin extends laterally between the hypergaussian edges of each petal and over the circular central portion. The covering skin defines a substantially planar surface oriented substantially perpendicular to the center axis when the occulter is in the deployed configuration.
摘要翻译：基于空间的遮罩可以在收起和展开的配置之间选择性地移动。基座毂具有纵向定向的中心轴线。设置多个花瓣，当处于展开构型时，每个花瓣从基座毂径向向外延伸并与其径向分开。每个花瓣具有由多个超高斯边缘面板组成的超高斯边缘。每个超高斯边缘面板定义花瓣的超高斯边缘的一部分。每个超高斯边缘面板基本上由具有接近零热膨胀系数的材料制成。圆形中心部分径向地位于基座毂和多个花瓣之间。覆盖皮肤横向延伸在每个花瓣的超高边缘之间并且在圆形中心部分上方。覆盖皮肤限定了当遮罩处于展开构型时基本上垂直于中心轴线定向的基本平坦的表面。

6. 发明授权

US10005571B2 Deployable solar panel array for spacecraft 有权
公开(公告)号：US10005571B2
公开(公告)日：2018-06-26
申请号：US14964258
申请日：2015-12-09
申请人： Geoffrey W. Marks , David J. Rohweller , Christian J. Pedersen
发明人： Geoffrey W. Marks , David J. Rohweller , Christian J. Pedersen
IPC分类号： B64G1/44 , B64G1/22 , H02S30/20
CPC分类号： B64G1/443 , B64G1/222 , B64G1/44 , H02S30/20
摘要： A solar panel assembly for a spacecraft includes a bracket and first and second booms each having a first end secured to the bracket and a second end extending away from the bracket. Each boom is formed from a plurality of tubes that telescope between a stowed condition nested within one another and a deployed condition aligned end-to-end with one another. A solar panel is secured to the first and second booms for receiving solar energy and converting the solar energy to electrical power. The solar panel has a stowed condition collapsed between the first and second booms and a deployed condition extending in a plane between the first and second booms.

7. 发明申请

US20140232611A1 DEPLOYABLE HELICAL ANTENNA FOR NANO-SATELLITES 有权
标题翻译：纳米卫星的合适的天线
公开(公告)号：US20140232611A1
公开(公告)日：2014-08-21
申请号：US13564393
申请日：2012-08-01
申请人： Daniel J. Ochoa , Geoffrey W. Marks , David J. Rohweller
发明人： Daniel J. Ochoa , Geoffrey W. Marks , David J. Rohweller
IPC分类号： H01Q1/12 , H01Q1/36
CPC分类号： H01Q1/1235 , H01Q1/288 , H01Q1/362 , H01Q11/086
摘要： A helical antenna operable to be stowed on and deployed from a cubesat. The antenna includes two helical elements wound in opposite directions and defining an antenna column, where one of the helical elements is a conductive antenna element. The antenna also includes a plurality of circumferentially disposed vertical stiffeners extending along a length of the column and being coupled to the helical elements at each location where the vertical stiffeners and the helical elements cross. The helical elements and the vertical stiffeners are formed of a flexible material, such as a fiber glass, so that the antenna can be collapsed and stowed into a relatively small space. To position the antenna in the stowed configuration, the vertical stiffeners are folded on each other in a radial direction, and then the folded antenna is rolled in an axial direction from one end of the column to the other end.
摘要翻译：螺旋天线可操作地被存放在立方体上并展开。天线包括沿相反方向缠绕的两个螺旋形元件，并且限定天线柱，其中一个螺旋元件是导电天线元件。天线还包括沿着柱的长度延伸的多个周向设置的垂直加强件，并且在垂直加强件和螺旋元件交叉的每个位置处联接到螺旋元件。螺旋元件和垂直加强件由柔性材料（例如玻璃纤维）形成，使得天线能够收缩并收纳在较小的空间中。为了将天线放置在收起的构造中，垂直扶强件在径向方向上彼此折叠，然后折叠的天线在从柱的一端到另一端的轴向方向上滚动。

8. 发明授权

US5315795A Deployable/retractable telescoping mast assembly and method 失效
标题翻译：可部署/伸缩式伸缩杆总成及方法
公开(公告)号：US5315795A
公开(公告)日：1994-05-31
申请号：US862009
申请日：1992-04-01
申请人： Daniel S. H. Chae , David J. Rohweller , Mark W. Thomson
发明人： Daniel S. H. Chae , David J. Rohweller , Mark W. Thomson
IPC分类号： B66C23/687 , B66F11/00 , E04H12/18 , B66C23/06
CPC分类号： B66F11/00 , E04H12/182 , E04H12/185 , Y10T403/32516
摘要： A deployable and retractable, telescoping style mast assembly and method employs a plurality of tubular sections of differing diameters. The tubular sections are nested one-in-another and are slidable with respect to each other, in a telescoping manner, to provide a deployable/retractable telescoping mast assembly. Retractable pins are provided to retractably extend from a collar coupled to at least one of the tube sections. In their extended state, the retractable pins are adapted to extend through apertures provided in an adjacent tube section. The retractable pins are provided with a head at one end thereof. The head of each pin is adapted to be engaged by a guide coupled to a third tube section upon the third tube section being in a collapsed state. Upon engagement with the pin head, the guide operates to pull the pin into a retracted state so as to retract the pin out of the pin receiving aperture.
摘要翻译：可部署和可伸缩的伸缩式桅杆组件和方法采用不同直径的多个管状部分。管状部分一个接一个地嵌套并且可以以伸缩的方式相对于彼此滑动，以提供可展开/可伸缩的伸缩式桅杆组件。提供伸缩销以从联接到至少一个管段的套环伸缩地延伸。在伸展状态下，伸缩销适于延伸通过设置在相邻管部分中的孔。可伸缩销在其一端设置有头部。每个销的头部适于在第三管部分处于折叠状态时由连接到第三管部分的引导件接合。在与销头接合时，引导件操作以将销拉入缩回状态，以将销从销接收孔缩回。

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