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公开(公告)号：US08622343B2
公开(公告)日：2014-01-07
申请号：US13478560
申请日：2012-05-23
申请人： Christopher E. Fisher , John Peter Zwaan , David R. Thompson , Marc L. Schmalzel , Karl R. Klingebiel , Tyson R. Jensen , Pavel Belik , Eric James Aagaard
发明人： Christopher E. Fisher , John Peter Zwaan , David R. Thompson , Marc L. Schmalzel , Karl R. Klingebiel , Tyson R. Jensen , Pavel Belik , Eric James Aagaard
CPC分类号： B64F1/12 , B05B1/02 , B29C65/48 , B29L2031/3076 , B64C39/024 , B64F1/16 , Y10T156/10 , Y10T156/1788
摘要： Liquid dispensing assemblies including adhesive anchoring assemblies configured to adhere to a support surface external to a device such as a vehicle. An air vehicle includes (a) a fluid adhesive container assembly detachably attached to the air vehicle, wherein the fluid adhesive container assembly comprises: (i) an adhesive container comprising fluid adhesive; and (ii) one or more fibers, wherein the one or more fibers are configured, or a brush of fibers, or a fabric of fibers, is configured to conduct the fluid adhesive and to structurally support an adhesive bond between the one or more fibers and a surface; and (b) means for dispensing the fluid adhesive from the fluid adhesive container, to the one or more fibers.
摘要翻译： 液体分配组件包括被配置为粘附到诸如车辆的装置外部的支撑表面的粘合剂锚固组件。 一种空中交通工具包括（a）可拆卸地附接到空中交通工具的流体粘合剂容器组件，其中流体粘合剂容器组件包括：（i）包含流体粘合剂的粘合剂容器; 和（ii）一种或多种纤维，其中所述一种或多种纤维构成，或纤维刷或纤维织物构造成导电流体粘合剂，并且在结构上支撑所述一种或多种纤维之间的粘合剂结合 和表面; 和（b）用于将流体粘合剂从流体粘合剂容器分配到一个或多个纤维的装置。
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公开(公告)号：US20120251092A1
公开(公告)日：2012-10-04
申请号：US13478764
申请日：2012-05-23
CPC分类号： B64C39/024 , B64C2201/127 , B64D47/08 , G03B15/006 , G03B17/561
摘要： Embodiments include an assembly comprising: (a) a camera support structure comprising: a masthead disposed on the distal end of a mast wherein the masthead is configured to receive an imaging element; where a proximal end of the mast rotatably engaging an azimuth-elevation joint assembly wherein the azimuth-elevation joint assembly comprises a first angular actuator of a first rotational degree-of-freedom and a second angular actuator of a second rotational degree of freedom; and (b) a camera support structure housing comprising an aperture and a hatch wherein the hatch is resiliently biased to close the aperture; and wherein the camera support structure is configured to overcome the hatch resilient bias by at least one of: the release of a pin restraining a loaded spring and a rotational actuation of the mast via at least one of the first angular actuator and the second angular actuator.
摘要翻译： 实施例包括一种组件，包括：（a）照相机支撑结构，包括：桅杆，其设置在桅杆的远端上，其中桅顶被构造成接收成像元件; 其中所述桅杆的近端可旋转地接合方位角接头组件，其中所述方位角接头组件包括第一旋转自由度的第一角度致动器和第二旋转自由度的第二角度致动器; 和（b）相机支撑结构外壳，其包括孔和舱口，其中所述舱口被弹性偏压以关闭所述孔; 并且其中所述照相机支撑结构被配置为通过以下至少一个来克服所述舱口弹性偏压：释放限制装载的弹簧的销和通过所述第一角度致动器和所述第二角致动器中的至少一个的所述桅杆的旋转致动 。
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公开(公告)号：US08548314B2
公开(公告)日：2013-10-01
申请号：US13478764
申请日：2012-05-23
CPC分类号： B64C39/024 , B64C2201/127 , B64D47/08 , G03B15/006 , G03B17/561
摘要： Embodiments include an assembly comprising: (a) a camera support structure comprising: a masthead disposed on the distal end of a mast wherein the masthead is configured to receive an imaging element; where a proximal end of the mast rotatably engaging an azimuth-elevation joint assembly wherein the azimuth-elevation joint assembly comprises a first angular actuator of a first rotational degree-of-freedom and a second angular actuator of a second rotational degree of freedom; and (b) a camera support structure housing comprising an aperture and a hatch wherein the hatch is resiliently biased to close the aperture; and wherein the camera support structure is configured to overcome the hatch resilient bias by at least one of: the release of a pin restraining a loaded spring and a rotational actuation of the mast via at least one of the first angular actuator and the second angular actuator.
摘要翻译： 实施例包括一种组件，包括：（a）照相机支撑结构，包括：桅杆，其设置在桅杆的远端上，其中桅顶被构造成接收成像元件; 其中所述桅杆的近端可旋转地接合方位角接头组件，其中所述方位角接头组件包括第一旋转自由度的第一角度致动器和第二旋转自由度的第二角度致动器; 和（b）相机支撑结构外壳，其包括孔和舱口，其中所述舱口被弹性偏压以关闭所述孔; 并且其中所述照相机支撑结构被配置为通过以下至少一个来克服所述舱口弹性偏压：释放限制装载的弹簧的销和通过所述第一角度致动器和所述第二角致动器中的至少一个的所述桅杆的旋转致动 。
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公开(公告)号：US08761967B2
公开(公告)日：2014-06-24
申请号：US13478520
申请日：2012-05-23
CPC分类号： B64C39/024 , B64C29/0033 , B64C2201/027 , B64C2201/042 , B64C2201/102
摘要： Methods, systems, and devices for determining system/device configuration and setting a mode of operation based on the determined configuration. An air vehicle processor: (a) receives a component information set of at least one external component; (b) determine a mode of operation, by the processor having a current mode of operation setting, based on the received component information and at least one of: an initial mode of operation setting and the current mode of operation setting; (c) determines whether all of the one or more received component information sets match a configuration requirement; (d) transitions to a flight-ready status if the determination is a conjunctive match; and (e) transition to a reset status if the determination is not a conjunctive match.
摘要翻译： 用于确定系统/设备配置并基于所确定的配置来设置操作模式的方法，系统和设备。 一种飞行器处理器：（a）接收至少一个外部部件的部件信息组; （b）基于接收到的分量信息和至少一个操作设置模式和当前操作模式设置中的至少一个来确定具有当前操作模式设置的处理器的操作模式; （c）确定所述一个或多个接收到的分量信息集合是否匹配配置要求; （d）如果确定是联合匹配，则转换到飞行就绪状态; 和（e）如果确定不是联合匹配，则转换到复位状态。
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公开(公告)号：US20120232722A1
公开(公告)日：2012-09-13
申请号：US13478520
申请日：2012-05-23
IPC分类号： G05D1/00
CPC分类号： B64C39/024 , B64C29/0033 , B64C2201/027 , B64C2201/042 , B64C2201/102
摘要： Methods, systems, and devices for determining system/device configuration and setting a mode of operation based on the determined configuration. An air vehicle processor: (a) receives a component information 14 set of at least one external component; (b) determine a mode of operation, by the processor having a current mode of operation setting, based on the received component information and at least one of: an initial mode of operation setting and the current mode of operation setting; (c) determines whether all of the one or more received component information sets match a configuration requirement; (d) transitions to a flight-ready status if the determination is a conjunctive match; and (e) transition to a reset status if the determination is not a conjunctive match.
摘要翻译： 用于确定系统/设备配置并基于所确定的配置来设置操作模式的方法，系统和设备。 一种飞行器处理器：（a）接收至少一个外部部件的部件信息14组; （b）基于接收到的分量信息和至少一个操作设置模式和当前操作模式设置中的至少一个来确定具有当前操作模式设置的处理器的操作模式; （c）确定所述一个或多个接收到的分量信息集合是否匹配配置要求; （d）如果确定是联合匹配，则转换到飞行就绪状态; 和（e）如果确定不是联合匹配，则转换到复位状态。
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公开(公告)号：US09208689B2
公开(公告)日：2015-12-08
申请号：US13261814
申请日：2012-08-16
CPC分类号： G08G5/02 , B64C39/024 , B64C2201/021 , B64C2201/042 , B64C2201/104 , B64C2201/127 , B64C2201/14 , B64C2201/146 , B64C2201/165 , B64C2201/18 , B64D31/00 , G05D1/0011 , G05D1/0676
摘要： An aircraft defining an upright orientation and an inverted orientation, a ground station; and a control system for remotely controlling the flight of the aircraft. The ground station has an auto-land function that causes the aircraft to invert, stall, and controllably land in the inverted orientation to protect a payload and a rudder extending down from the aircraft. In the upright orientation, the ground station depicts the view from a first aircraft camera. When switching to the inverted orientation: (1) the ground station depicts the view from a second aircraft camera, (2) the aircraft switches the colors of red and green wing lights, extends the ailerons to act as inverted flaps, and (3) the control system adapts a ground station controller for the inverted orientation. The aircraft landing gear is an expanded polypropylene pad located above the wing when the aircraft is in the upright orientation.
摘要翻译： 定义直立方向和倒置方向的飞机，地面站; 以及用于远程控制飞机飞行的控制系统。 地面站具有自动地面功能，使飞机以反方向反转，失速和可控地降落，以保护从飞机向下延伸的有效载荷和舵。 在直立方向，地面站描绘从第一架飞机摄像机的视图。 当切换到倒置方向时：（1）地面站描绘从第二架飞机照相机的视野，（2）飞机切换红色和绿色翼灯的颜色，延伸副翼作为倒转襟翼，（3） 控制系统适应地面站控制器的倒置方向。 飞机起落架是当飞机处于直立方向时位于机翼上方的扩展的聚丙烯垫。
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公开(公告)号：US20140343752A1
公开(公告)日：2014-11-20
申请号：US13261814
申请日：2012-08-16
CPC分类号： G08G5/02 , B64C39/024 , B64C2201/021 , B64C2201/042 , B64C2201/104 , B64C2201/127 , B64C2201/14 , B64C2201/146 , B64C2201/165 , B64C2201/18 , B64D31/00 , G05D1/0011 , G05D1/0676
摘要： An aircraft defining an upright orientation and an inverted orientation, a ground station; and a control system for remotely controlling the flight of the aircraft. The ground station has an auto-land function that causes the aircraft to invert, stall, and controllably land in the inverted orientation to protect a payload and a rudder extending down from the aircraft. In the upright orientation, the ground station depicts the view from a first aircraft camera. When switching to the inverted orientation: (1) the ground station depicts the view from a second aircraft camera, (2) the aircraft switches the colors of red and green wing lights, extends the ailerons to act as inverted flaps, and (3) the control system adapts a ground station controller for the inverted orientation. The aircraft landing gear is an expanded polypropylene pad located above the wing when the aircraft is in the upright orientation.
摘要翻译： 定义直立方向和倒置方向的飞机，地面站; 以及用于远程控制飞机飞行的控制系统。 地面站具有自动地面功能，使飞机以反方向反转，失速和可控地降落，以保护从飞机向下延伸的有效载荷和舵。 在直立方向，地面站描绘从第一架飞机摄像机的视图。 当切换到倒置方向时：（1）地面站描绘从第二架飞机照相机的视图，（2）飞机切换红色和绿色翼灯的颜色，将副翼延伸为反转翼片，（3） 控制系统适应地面站控制器的倒置方向。 飞机起落架是当飞机处于直立方向时位于机翼上方的扩展的聚丙烯垫。
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公开(公告)号：US09511858B2
公开(公告)日：2016-12-06
申请号：US13261813
申请日：2012-08-16
CPC分类号： G01C5/005 , B64C39/024 , B64C2201/021 , B64C2201/104 , B64C2201/127 , B64C2201/146 , B64C2201/165 , B64C2201/18 , B64D47/08 , G05D1/0011 , G05D1/0676 , G05D1/0808 , G05D1/0816
摘要： An aircraft defining an upright orientation and an inverted orientation, a ground station; and a control system for remotely controlling the flight of the aircraft. The ground station has an auto-land function that causes the aircraft to invert, stall, and controllably land in the inverted orientation to protect a payload and a rudder extending down from the aircraft. In the upright orientation, the ground station depicts the view from a first aircraft camera. When switching to the inverted orientation: (1) the ground station depicts the view from a second aircraft camera, (2) the aircraft switches the colors of red and green wing lights, extends the ailerons to act as inverted flaps, and (3) the control system adapts a ground station controller for the inverted orientation. The aircraft landing gear is an expanded polypropylene pad located above the wing when the aircraft is in the upright orientation.
摘要翻译： 定义直立方向和倒置方向的飞机，地面站; 以及用于远程控制飞机飞行的控制系统。 地面站具有自动地面功能，使飞机以反方向反转，失速和可控地降落，以保护从飞机向下延伸的有效载荷和舵。 在直立方向，地面站描绘从第一架飞机摄像机的视图。 当切换到倒置方向时：（1）地面站描绘从第二架飞机照相机的视图，（2）飞机切换红色和绿色翼灯的颜色，将副翼延伸为反转翼片，（3） 控制系统适应地面站控制器的倒置方向。 飞机起落架是当飞机处于直立方向时位于机翼上方的扩展的聚丙烯垫。
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公开(公告)号：US20140350748A1
公开(公告)日：2014-11-27
申请号：US13261813
申请日：2012-08-16
CPC分类号： G01C5/005 , B64C39/024 , B64C2201/021 , B64C2201/104 , B64C2201/127 , B64C2201/146 , B64C2201/165 , B64C2201/18 , B64D47/08 , G05D1/0011 , G05D1/0676 , G05D1/0808 , G05D1/0816
摘要： An aircraft defining an upright orientation and an inverted orientation, a ground station; and a control system for remotely controlling the flight of the aircraft. The ground station has an auto-land function that causes the aircraft to invert, stall, and controllably land in the inverted orientation to protect a payload and a rudder extending down from the aircraft. In the upright orientation, the ground station depicts the view from a first aircraft camera. When switching to the inverted orientation: (1) the ground station depicts the view from a second aircraft camera, (2) the aircraft switches the colors of red and green wing lights, extends the ailerons to act as inverted flaps, and (3) the control system adapts a ground station controller for the inverted orientation. The aircraft landing gear is an expanded polypropylene pad located above the wing when the aircraft is in the upright orientation.
摘要翻译： 定义直立方向和倒置方向的飞机，地面站; 以及用于远程控制飞机飞行的控制系统。 地面站具有自动地面功能，使飞机以反方向反转，失速和可控地降落，以保护从飞机向下延伸的有效载荷和舵。 在直立方向，地面站描绘从第一架飞机摄像机的视图。 当切换到倒置方向时：（1）地面站描绘从第二架飞机照相机的视图，（2）飞机切换红色和绿色翼灯的颜色，将副翼延伸为反转翼片，（3） 控制系统适应地面站控制器的倒置方向。 飞机起落架是当飞机处于直立方向时位于机翼上方的扩展的聚丙烯垫。
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10.发明授权Ultraviolet curable coatings for optical glass fiber based on a polyfunctional core 失效基于多功能核心的光学玻璃纤维紫外线固化涂层
公开(公告)号：US4806574A
公开(公告)日：1989-02-21
申请号：US757249
申请日：1985-07-22
申请人： John J. Krajewski , Timothy E. Bishop , Clive J. Coady , John M. Zimmerman , Gerry K. Noren , Christopher E. Fisher
发明人： John J. Krajewski , Timothy E. Bishop , Clive J. Coady , John M. Zimmerman , Gerry K. Noren , Christopher E. Fisher
IPC分类号： C03C25/24 , C03C25/10 , C08F2/48 , C08F2/50 , C08F290/00 , C08F299/00 , C08F299/06 , C08G18/50 , C08G18/67 , C08G18/78 , C08G18/79 , C08G18/81 , C09D5/00 , C09D175/14 , G02B6/44 , C08F20/58 , C08F20/60 , G02B6/16
CPC分类号： C08G18/672 , C03C25/106 , C03C25/1065 , C08G18/5024 , C08G18/7831 , C08G18/792 , C08G18/8175
摘要： An ultraviolet curing liquid coating composition which, when cured with ultraviolet light in the presence of an appropriate photoinitiator, provides a coating adapted for the coating of optical glass fiber. This coating composition comprises as the essential component, an acrylate-terminated polyurethane oligomer based on a polyfunctional core which is at least trifunctional and which supports one branch for each functionality in the core. Each of the branches leads to an acrylate-functional terminal group, with there being from about 150 to about 2500 units of molecular weight in each branch between the trifunctional core and the acrylate-functional terminal group. Depending primarily upon the molecular weight of the branches, one can provide coating compositions for buffer coat, single coat or topcoat use.
摘要翻译： 一种紫外线固化液体涂料组合物，其在适当的光引发剂存在下用紫外线固化时，提供适于涂覆光学玻璃纤维的涂层。 该涂料组合物包含基于至少三官能的多官能核心的丙烯酸酯封端的聚氨酯低聚物，并且其对核心中的每个官能团支持一个分支。 每个支链通过丙烯酸酯官能的末端基团，在三官能核心和丙烯酸酯官能的末端基团之间的每个分支中分子量为约150至约2500单位。 主要取决于分支的分子量，可以提供缓冲涂层，单涂层或面漆使用的涂料组合物。
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