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公开(公告)号：US20230242271A1
公开(公告)日：2023-08-03
申请号：US18295215
申请日：2023-04-03
CPC分类号： B64D39/06 , B67D7/04 , B67D7/40 , B64C39/024 , B64D5/00 , B64D1/06 , B64D1/22 , B64D1/16 , B64U30/10
摘要： A stabilizing system for a cable has a cable deployed and suspended from a helicopter, a cargo support attached at a deployed end of the cable, an end effector attached to the cable, the end effector comprising thrusters directed in a plurality of directions orthogonal to a vertical axis of the cable, first control circuitry in the helicopter, and second control circuitry in the end effector. Thrust of individual thrusters is controlled through the first and second control circuitry maintaining the axis of the cable vertical, damping swinging of the cable.
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公开(公告)号：US11702221B2
公开(公告)日：2023-07-18
申请号：US17093218
申请日：2020-11-09
IPC分类号： B64D39/06 , B67D7/04 , B67D7/40 , B64C39/02 , B64D5/00 , B64D1/06 , B64D1/22 , B64D1/16 , B64U30/10 , B64U50/12 , B64U50/34 , B64U80/82
CPC分类号： B64D39/06 , B64C39/024 , B64D1/06 , B64D1/16 , B64D1/22 , B64D5/00 , B67D7/04 , B67D7/40 , B64U30/10 , B64U50/12 , B64U50/34 , B64U80/82
摘要： A system for fighting fires has a source of fire-retardant material, a delivery hose connected to the source has a delivery nozzle at an end, and an end effector carrying the delivery hose proximate the nozzle. The end effector has controllable thrusters, an imaging device, and control circuitry including a display monitor, the control circuitry providing commands controlling actuators varying thrust and direction of the thrusters, and a valve in the delivery nozzle. With the delivery hose deployed, images from the end effector are transmitted to the control circuitry and displayed on the display monitor, and an operator viewing the images on the display monitor uses the command inputs to maneuver the end effector, carrying the nozzle at the end of the delivery hose to a position proximate an active fire, and opens the valve on the nozzle, delivering fire retardant material from the nozzle onto the fire.
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公开(公告)号：US11702220B2
公开(公告)日：2023-07-18
申请号：US17093137
申请日：2020-11-09
IPC分类号： B64D39/06 , B64C39/02 , B67D7/04 , B67D7/40 , B64D5/00 , B64D1/06 , B64D1/22 , B64D1/16 , B64U30/10 , B64U50/12 , B64U50/34 , B64U80/82
CPC分类号： B64D39/06 , B64C39/024 , B64D1/06 , B64D1/16 , B64D1/22 , B64D5/00 , B67D7/04 , B67D7/40 , B64U30/10 , B64U50/12 , B64U50/34 , B64U80/82
摘要： A system for refueling has a boom having a rigid portion and, extendible portion and a fuel nozzle at an end of the extendible portion, the fuel nozzle mates with a port on an aircraft. Control circuitry in the tanker aircraft has input elements by which an operator controls actuators moving the boom left, right and up and down, and a first imaging device proximate the end of the extendible portion of the boom, capturing images and transmitting the captured images to the control circuitry, where the images are displayed on a monitor visible to the operator. The operator controls extension and attitude of the fuel nozzle at the end of the extendible portion, according to the images displayed, mating the fuel nozzle with the refueling port, and transferring fuel from the tanker aircraft to the aircraft to be refueled.
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公开(公告)号：US20210253265A1
公开(公告)日：2021-08-19
申请号：US17093061
申请日：2020-11-09
摘要： A stabilizing system for a winch cable has a winch cable deployed and suspended from a helicopter, a cargo support attached at a deployed end of the winch cable, an end effector attached to the winch cable, the end effector comprising thrusters directed in a plurality of directions orthogonal to a vertical axis of the winch cable, first control circuitry in the helicopter, and second control circuitry in the end effector. Thrust of individual thrusters is controlled through the first and second control circuitry maintaining the axis of the winch cable vertical, damping swinging of the cable.
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公开(公告)号：US20210163149A1
公开(公告)日：2021-06-03
申请号：US17093197
申请日：2020-11-09
摘要： A refueling system has a first vehicle having a fuel tank connected to a deployable fuel hose with a nozzle on the deployable end, a second vehicle carrying a supply of fuel, having a refueling panel with a refueling port adapted to connect to the nozzle on the deployed end of the fuel hose, an end effector joined to the fuel hose proximate the nozzle, the end effector having a plurality of thrusters providing thrust in a plurality of directions; and control circuitry in the first vehicle and in the end effector enabling an operative to vary direction and thrust of the thrusters. The operative controls the thrusters through the control circuitry to direct the nozzle toward and to connect the nozzle to the refueling port on the refueling panel of the second vehicle.
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公开(公告)号：US20210107675A1
公开(公告)日：2021-04-15
申请号：US17077797
申请日：2020-10-22
摘要： A personnel rescue system has a winch subsystem comprising a first tether deployable and retrievable with a powered winch, a powered and controllable end effector attached at a deployable end of the first tether, a second tether attached by a first end to the end effector, a personnel harness attached at a second end of the second tether; and control apparatus in communication with the end effector, the control apparatus operable to maneuver the end effector vertically and laterally, carrying the personnel harness to a subject to be rescued.
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7.发明授权Visual inspection apparatus, secure one-way data transfer device and methods therefor 有权目视检查装置，安全单向数据传输装置及其方法公开(公告)号：US08983172B2
公开(公告)日：2015-03-17
申请号：US13730377
申请日：2012-12-28
CPC分类号： G06T7/0046 , G06T7/75 , G06T2207/20104 , G06T2207/30108
摘要： A visual inspection system includes a database storing a wireframe model of an object and a portable electronic device equipped with an imaging device and a display. The portable electronic device is in communication with the database. The portable electronic device is configured to show on the display the wireframe model as an overlay to an image of the object taken by the imaging device. The display is configured to accept input of a trace of a defect on the display, and displays the trace on the image. A method of transmitting electronic data from an unsecure device to a secure database is also described.
摘要翻译： 视觉检查系统包括存储物体的线框模型的数据库和配备有成像装置和显示器的便携式电子装置。 便携式电子设备与数据库通信。 便携式电子设备被配置为在显示器上显示线框模型作为由成像设备拍摄的对象的图像的覆盖。 显示器配置为接受显示屏上缺陷痕迹的输入，并在图像上显示轨迹。 还描述了将电子数据从不安全装置发送到安全数据库的方法。
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8.发明申请VISUAL INSPECTION APPARATUS, SECURE ONE-WAY DATA TRANSFER DEVICE AND METHODS THEREFOR 有权视觉检测设备，安全一路数据传输设备及其方法公开(公告)号：US20140185911A1
公开(公告)日：2014-07-03
申请号：US13730377
申请日：2012-12-28
IPC分类号： G06T7/00
CPC分类号： G06T7/0046 , G06T7/75 , G06T2207/20104 , G06T2207/30108
摘要： A visual inspection system includes a database storing a wireframe model of an object and a portable electronic device equipped with an imaging device and a display. The portable electronic device is in communication with the database. The portable electronic device is configured to show on the display the wireframe model as an overlay to an image of the object taken by the imaging device. The display is configured to accept input of a trace of a defect on the display, and displays the trace on the image. A method of transmitting electronic data from an unsecure device to a secure database is also described.
摘要翻译： 视觉检查系统包括存储物体的线框模型的数据库和配备有成像装置和显示器的便携式电子装置。 便携式电子设备与数据库通信。 便携式电子设备被配置为在显示器上显示线框模型作为由成像设备拍摄的对象的图像的覆盖。 显示器配置为接受显示屏上缺陷痕迹的输入，并在图像上显示轨迹。 还描述了将电子数据从不安全装置发送到安全数据库的方法。
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公开(公告)号：US12103701B2
公开(公告)日：2024-10-01
申请号：US18295215
申请日：2023-04-03
IPC分类号： B64D1/06 , B64C39/02 , B64D1/16 , B64D1/22 , B64D5/00 , B64D39/06 , B67D7/04 , B67D7/40 , B64U30/10 , B64U50/12 , B64U50/34 , B64U80/82
CPC分类号： B64D39/06 , B64C39/024 , B64D1/06 , B64D1/16 , B64D1/22 , B64D5/00 , B67D7/04 , B67D7/40 , B64U30/10 , B64U50/12 , B64U50/34 , B64U80/82
摘要： A stabilizing system for a cable has a cable deployed and suspended from a helicopter, a cargo support attached at a deployed end of the cable, an end effector attached to the cable, the end effector comprising thrusters directed in a plurality of directions orthogonal to a vertical axis of the cable, first control circuitry in the helicopter, and second control circuitry in the end effector. Thrust of individual thrusters is controlled through the first and second control circuitry maintaining the axis of the cable vertical, damping swinging of the cable.
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公开(公告)号：US20230391469A1
公开(公告)日：2023-12-07
申请号：US18297826
申请日：2023-04-10
CPC分类号： B64D39/06 , B67D7/04 , B67D7/40 , B64C39/024 , B64D5/00 , B64D1/06 , B64D1/22 , B64D1/16 , B64U30/10
摘要： A satellite refueling system has a refueling satellite carrying fuel, a fuel hose connected to the fuel carried by the refueling satellite, with a maneuverable end effector at a deployed end of the fuel hose, the end effector comprising a fuel supply nozzle connected to the fuel hose, a plurality of thrusters on the end effector providing thrust in a plurality of directions, an imaging device on the end effector capturing images in an immediate environment of the end effector, and computerized circuitry operating individual ones of the plurality of thrusters in response to the images captured by the imaging device. The refueling satellite deploys the fuel hose, and the computerized circuitry operates the thrusters to maneuver the end effector, bringing the fuel supply nozzle to a location to deliver fuel.
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