-
公开(公告)号：US09908608B2
公开(公告)日：2018-03-06
申请号：US15351441
申请日：2016-11-14
IPC分类号： H04W4/02 , B64B1/40 , G05D1/04 , B64B1/64 , B64B1/70 , G01S19/42 , G01S19/24 , H04Q9/02 , B64B1/44 , G01S5/06 , G01S5/12 , H04B7/185
CPC分类号： B64B1/40 , B64B1/44 , B64B1/64 , B64B1/70 , G01S5/06 , G01S5/12 , G01S19/24 , G01S19/39 , G01S19/42 , G05D1/042 , H04B7/18502 , H04B7/18504 , H04B7/18576 , H04Q9/02 , H04W4/023 , H04W4/027
摘要： Innovative new systems and method of operating the systems, wherein the system comprises an airborne platform comprising an unmanned balloon; a payload that is separate from the unmanned balloon; a transceiver; first and second flight termination devices; at least two separate power sources for the first and second flight termination devices; a sensor; a processor; a pump; a valve; and a tether that when broken separates the unmanned balloon and the payload, are disclosed herein.
-
公开(公告)号：US09632503B2
公开(公告)日：2017-04-25
申请号：US15366020
申请日：2016-12-01
CPC分类号： G05D1/0055 , B64B1/40 , B64B1/44 , B64B1/46 , B64B1/62 , B64B1/64 , B64B1/70 , B64C39/024 , B64C2201/022 , B64C2201/125 , B64C2201/145 , G01S5/02 , G07C5/0808 , H04B7/18502 , H04B7/18504 , H04B7/18576 , H04W4/023 , H04W4/027
摘要： Innovative new systems and method of operating the systems, wherein the system comprises an airborne platform comprising an unmanned balloon; a payload that is separate from the unmanned balloon; a transceiver; first and second flight termination devices; at least two separate power sources for the first and second flight termination devices; a sensor; a processor; a pump; a valve; and a tether that when broken separates the unmanned balloon and the payload, are disclosed herein.
-
公开(公告)号：US10710695B2
公开(公告)日：2020-07-14
申请号：US15912599
申请日：2018-03-06
IPC分类号： B64B1/40 , G05D1/04 , B64B1/64 , B64B1/70 , G01S19/42 , G01S19/24 , H04Q9/02 , B64B1/44 , G01S5/06 , G01S5/12 , H04B7/185 , H04W4/02 , G01S19/39
摘要： Innovative new systems and method of operating the systems, wherein the system comprises an airborne platform comprising an unmanned balloon comprising a gas enclosure; a geographic locator or tracking system configured to determine geographical coordinates of the unmanned balloon; a payload comprising a transceiver, wherein the transceiver is capable of communicating with communication devices that are separate from the unmanned balloon; first and second flight-termination devices each configured to cause termination of a flight of the unmanned balloon; and at least two power sources each configured to provide power to at least one of the first and second flight-termination devices.
-
公开(公告)号：US09519045B2
公开(公告)日：2016-12-13
申请号：US14473691
申请日：2014-08-29
IPC分类号： B64B1/40 , G01S5/06 , B64B1/44 , B64B1/64 , B64B1/70 , H04B7/185 , B64C19/00 , B64B1/62 , G05D1/04 , G01S5/12 , G01S19/42 , H04W4/02
CPC分类号： G01S5/06 , B64B1/40 , B64B1/44 , B64B1/62 , B64B1/64 , B64B1/70 , B64C19/00 , G01S5/12 , G01S19/42 , G05D1/042 , H04B7/18502 , H04B7/18504 , H04B7/18576 , H04W4/023 , H04W4/027
摘要： Innovative new methods in connection with lighter-than-air (LTA) free floating platforms, of facilitating legal transmitter operation, platform flight termination when appropriate, environmentally acceptable landing, and recovery of these devices are provided. The new systems and methods relate to rise rate control, geo-location from a LTA platform including landed payload and ground-based vehicle locations, and steerable recovery systems.
摘要翻译： 提供了与轻于空气（LTA）自由浮动平台相关的创新新方法，便于合法的变送器操作，适当的平台飞行终止，环境可接受的着陆和这些设备的恢复。 新的系统和方法涉及上升速率控制，LTA平台的地理位置，包括着陆有效载荷和地面车辆位置以及可操纵的恢复系统。
-
公开(公告)号：US09964629B2
公开(公告)日：2018-05-08
申请号：US15343190
申请日：2016-11-03
IPC分类号： G01S5/06 , H04W4/02 , H04B7/185 , B64B1/70 , B64B1/62 , B64B1/44 , G01S19/42 , G01S5/12 , B64B1/64
CPC分类号： G01S5/06 , B64B1/40 , B64B1/44 , B64B1/62 , B64B1/64 , B64B1/70 , B64C19/00 , G01S5/12 , G01S19/42 , G05D1/042 , H04B7/18502 , H04B7/18504 , H04B7/18576 , H04W4/023 , H04W4/027
摘要： Innovative new methods in connection with lighter-than-air (LTA) free floating platforms, of facilitating legal transmitter operation, platform flight termination when appropriate, environmentally acceptable landing, and recovery of these devices are provided. The new systems and methods relate to rise rate control, geo-location from a LTA platform including landed payload and ground-based vehicle locations, and steerable recovery systems.
-
公开(公告)号：US09658618B1
公开(公告)日：2017-05-23
申请号：US15434036
申请日：2017-02-15
CPC分类号： G05D1/0055 , B64B1/40 , B64B1/44 , B64B1/46 , B64B1/62 , B64B1/64 , B64B1/70 , B64C39/024 , B64C2201/022 , B64C2201/125 , B64C2201/145 , G01S5/02 , G07C5/0808 , H04B7/18502 , H04B7/18504 , H04B7/18576 , H04W4/023 , H04W4/027
摘要： Innovative new systems and method of operating the systems, wherein the system comprises an airborne platform comprising an unmanned balloon; a payload that is separate from the unmanned balloon; a transceiver; a flight termination device; at least two separate power sources; a sensor; a processor; a pump; a valve; and an object that when broken separates the unmanned balloon and the payload, are disclosed herein.
-
公开(公告)号：US10894592B2
公开(公告)日：2021-01-19
申请号：US16886870
申请日：2020-05-29
IPC分类号： B64B1/40 , H04W4/02 , B64B1/64 , B64B1/70 , G01S19/42 , G01S19/24 , H04Q9/02 , B64B1/44 , G01S5/06 , G01S5/12 , H04B7/185 , G05D1/04
摘要： Innovative new systems and method of operating the systems, wherein the system comprises an airborne platform comprising an unmanned balloon comprising a gas enclosure; a geographic locator or tracking system configured to determine geographical coordinates of the unmanned balloon; a payload comprising a transceiver, wherein the transceiver is capable of communicating with communication devices that are separate from the unmanned balloon; first and second flight-termination devices each configured to cause termination of a flight of the unmanned balloon; and at least two power sources each configured to provide power to at least one of the first and second flight-termination devices.
-
公开(公告)号：US20180194449A1
公开(公告)日：2018-07-12
申请号：US15912599
申请日：2018-03-06
IPC分类号： B64B1/40 , G05D1/04 , H04B7/185 , H04Q9/02 , H04W4/02 , G01S19/42 , B64B1/44 , B64B1/64 , B64B1/70 , G01S5/06 , G01S5/12 , G01S19/24
摘要： Innovative new systems and method of operating the systems, wherein the system comprises an airborne platform comprising an unmanned balloon comprising a gas enclosure; a geographic locator or tracking system configured to determine geographical coordinates of the unmanned balloon; a payload comprising a transceiver, wherein the transceiver is capable of communicating with communication devices that are separate from the unmanned balloon; first and second flight-termination devices each configured to cause termination of a flight of the unmanned balloon; and at least two power sources each configured to provide power to at least one of the first and second flight-termination devices.
-
公开(公告)号：US09678193B2
公开(公告)日：2017-06-13
申请号：US14328331
申请日：2014-07-10
IPC分类号： G01C3/00 , G01S5/06 , B64B1/40 , B64B1/44 , B64B1/64 , B64B1/70 , H04B7/185 , B64C19/00 , B64B1/62 , G05D1/04 , G01S5/12 , G01S19/42 , H04W4/02
CPC分类号： G01S5/06 , B64B1/40 , B64B1/44 , B64B1/62 , B64B1/64 , B64B1/70 , B64C19/00 , G01S5/12 , G01S19/42 , G05D1/042 , H04B7/18502 , H04B7/18504 , H04B7/18576 , H04W4/023 , H04W4/027
摘要： Innovative new methods in connection with lighter-than-air (LTA) free floating platforms, of facilitating legal transmitter operation, platform flight termination when appropriate, environmentally acceptable landing, and recovery of these devices are provided. The new systems and methods relate to rise rate control, geo-location from a LTA platform including landed payload and ground-based vehicle locations, and steerable recovery systems.
-
公开(公告)号：US09643706B2
公开(公告)日：2017-05-09
申请号：US15351438
申请日：2016-11-14
CPC分类号： B64B1/40 , B64B1/44 , B64B1/62 , B64B1/64 , B64B1/70 , B64C2201/022 , G01S19/24 , G01S19/39 , G01S19/42 , G05D1/042 , H04B7/18502 , H04B7/18504 , H04B7/18576 , H04W4/023 , H04W4/027
摘要： Innovative new systems and method of operating the systems, wherein the system comprises an airborne platform comprising an unmanned balloon; a payload that is separate from the unmanned balloon; a transceiver; first and second flight termination devices; at least two separate power sources for the first and second flight termination devices; a sensor; a processor; a pump; a valve; and a tether that when broken separates the unmanned balloon and the payload, are disclosed herein.
-
-
-
-
-
-
-
-
-
搜索结果
10 条记录 (耗时 0.02 秒)
