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公开(公告)号：US09926084B2
公开(公告)日：2018-03-27
申请号：US15291878
申请日：2016-10-12
IPC分类号： B64F1/02 , B64C39/02 , G05D1/10 , B60L11/18 , B64F1/36 , B64C25/68 , B64D47/04 , B64D47/08 , G06K9/00
CPC分类号： B64F1/02 , B60L11/1816 , B60L11/1838 , B60L2200/10 , B64C25/68 , B64C39/024 , B64C2201/028 , B64C2201/042 , B64C2201/06 , B64C2201/066 , B64C2201/123 , B64C2201/127 , B64C2201/141 , B64C2201/182 , B64D47/04 , B64D47/08 , B64F1/362 , G05D1/101 , G06K9/0063
摘要： An aerial vehicle landing station comprising a first post and a second post, wherein the second post is spaced apart from the first post and a cable to capture an aerial vehicle, wherein the cable is stretched between the first post and the second post and configured to support the weight of the aerial vehicle once captured and the cable may provide a charging current to the aerial vehicle once captured. One or more markers may be further positioned on the cable to designate a landing point, wherein the one or more markers are configured to be visually tracked by the aerial vehicle. A cable management device coupled to the cable via one or more pulleys may regulate tension of the cable. A communications transceiver at the aerial vehicle landing station may wirelessly communicate data with the aerial vehicle.
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公开(公告)号：US09896222B2
公开(公告)日：2018-02-20
申请号：US14939893
申请日：2015-11-12
申请人： Insitu, Inc.
CPC分类号： B64F1/02 , B64C25/68 , B64C39/024 , B64C2201/182
摘要： Capture devices for unmanned aerial vehicles, including track borne capture lines, and associated systems and methods are disclosed. A representative system includes at least one support having an upright portion and at least one boom portion, a carriage track carried by the at least one boom portion, and a carriage carried by, and movable along, the carriage track. The system can further include a capture line carried by and extending downwardly from the at least one boom portion, or the carriage, or both the at least one boom portion and the carriage.
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公开(公告)号：US09067675B2
公开(公告)日：2015-06-30
申请号：US13736632
申请日：2013-01-08
申请人： The Boeing Company
摘要： A system, an apparatus, and a method for an aerospace vehicle braking system for decelerating an aerospace vehicle on a landing surface. An arm is provided having a first portion connected to the aerospace vehicle and a second portion generally distal to the first portion. The second portion of the arm includes an engagement portion configured to engage the landing surface. The arm is movable between a first position, wherein the engagement portion is substantially disengaged from the landing surface, and a second position, wherein the engagement portion engages the landing surface with a force sufficient to significantly decelerate the aerospace vehicle. The engagement portion is configured to pivot with respect to the arm in response to the direction of travel of the aerospace vehicle upon the landing surface. An actuator is connected to the arm to selectively move the arm between the first position and the second position.
摘要翻译： 一种用于航空航天车辆制动系统的系统，装置和方法，用于使航空航天器在着陆面上减速。 臂被设置有具有连接到航空航天车辆的第一部分和大致远离第一部分的第二部分。 臂的第二部分包括被配置为接合着陆表面的接合部分。 臂可在第一位置和第二位置之间移动，第一位置与接合部分基本上脱离接合表面;第二位置，其中接合部分以足以使航空航天车辆显着减速的力与着陆面接合。 接合部分构造成响应于航空航天器在着陆表面上的行进方向相对于臂枢转。 致动器连接到臂以选择性地在第一位置和第二位置之间移动臂。
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4.发明申请公开(公告)号：US20140203140A1
公开(公告)日：2014-07-24
申请号：US14247807
申请日：2014-04-08
申请人： Aerovel Corporation
CPC分类号： B64F1/12 , B64C25/68 , B64C39/024 , B64C2201/024 , B64C2201/084 , B64C2201/182 , B64F1/02 , B64F1/04 , B64F1/06 , B64F1/125 , B64F1/28 , B64F5/00
摘要： Various embodiments of the present disclosure provide an apparatus configured to automatically retrieve, service, and launch an aircraft. For retrieval, the aircraft drops a weighted cable, and pulls it at low relative speed into a broad aperture of the apparatus. In certain instances, the cable is dragged along guiding surfaces of the apparatus into and through a slot until its free end is captured. The aircraft becomes anchored to the apparatus, and is pulled downward by the cable into a receptacle. Guiding surfaces of the receptacle adjust the position and orientation of a probe on the aircraft, directing the probe to mate with a docking fixture of the apparatus. Once mated, the aircraft is automatically shut down and serviced. When desired, the aircraft is automatically started and tested in preparation for launch, and then released into free flight. A full ground-handling cycle is thus accomplished with a simple, economical apparatus.
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公开(公告)号：US08517306B2
公开(公告)日：2013-08-27
申请号：US11510920
申请日：2006-08-28
CPC分类号： B64F1/02 , B64C25/68 , B64C39/024 , B64C2201/084 , B64C2201/104 , B64C2201/165 , B64C2201/182 , B64C2201/205 , B64D3/00 , B64F1/04 , B64F1/10
摘要： A method of launching and retrieving a UAV (Unmanned Aerial Vehicle) (10). The preferred method of launch involves carrying the UAV (10) up to altitude using a parasail (8) similar to that used to carry tourists aloft. The UAV is dropped and picks up enough airspeed in the dive to perform a pull-up into level controlled flight. The preferred method of recovery is for the UAV to fly into and latch onto the parasail tow line (4) or cables hanging off the tow line and then be winched back down to the boat (2).
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公开(公告)号：US20110011974A1
公开(公告)日：2011-01-20
申请号：US12893407
申请日：2010-09-29
申请人： William R. McDonnell
发明人： William R. McDonnell
IPC分类号： B64F1/02
CPC分类号： B64F1/02 , B64C25/68 , B64C39/024 , B64C2201/084 , B64C2201/104 , B64C2201/165 , B64C2201/182 , B64C2201/205 , B64D3/00 , B64F1/04 , B64F1/10
摘要： A method of launching and retrieving a UAV (Unmanned Aerial Vehicle) (10). The preferred method of launch involves carrying the UAV (10) up to altitude using a parasail (8) similar to that used to carry tourists aloft. The UAV is dropped and picks up enough airspeed in the dive to perform a pull-up into level controlled flight. The preferred method of recovery is for the UAV to fly into and latch onto the parasail tow line (4) or cables hanging off the tow line and then be winched back down to the boat (2).
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公开(公告)号：US07152827B2
公开(公告)日：2006-12-26
申请号：US10759541
申请日：2004-01-16
申请人： Brian T. McGeer
发明人： Brian T. McGeer
IPC分类号： B64C3/56
CPC分类号： B64F1/04 , B64C25/68 , B64C39/024 , B64C2201/021 , B64C2201/042 , B64C2201/044 , B64C2201/048 , B64C2201/084 , B64C2201/102 , B64C2201/146 , B64C2201/165 , B64C2201/182 , B64C2201/201 , B64C2201/205 , B64F1/02 , B64F1/06
摘要： Methods and apparatuses for launching, capturing, and storing unmanned aircraft and other flight devices or projectiles are described. In one embodiment, the aircraft can be assembled from a container with little or no manual engagement by an operator. The container can include a guide structure to control motion of the aircraft components. The aircraft can be launched from an apparatus that includes an extendable boom. The boom can be extended to deploy a recovery line to capture the aircraft in flight. The aircraft can then be returned to its launch platform, disassembled, and stored in the container, again with little or no direct manual contact between the operator and the aircraft.
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8.发明授权Methods and apparatuses for launching, capturing, and storing unmanned aircraft, including a container having a guide structure for aircraft components 有权用于发射，捕获和存储无人飞行器的方法和装置，包括具有用于飞行器部件的引导结构的容器公开(公告)号：US07104495B2
公开(公告)日：2006-09-12
申请号：US11269395
申请日：2005-11-08
申请人： Brian T. McGeer
发明人： Brian T. McGeer
IPC分类号： B64F5/00
CPC分类号： B64F1/04 , B64C25/68 , B64C39/024 , B64C2201/021 , B64C2201/042 , B64C2201/044 , B64C2201/048 , B64C2201/084 , B64C2201/102 , B64C2201/146 , B64C2201/165 , B64C2201/182 , B64C2201/201 , B64C2201/205 , B64F1/02 , B64F1/06
摘要： Methods and apparatuses for launching, capturing, and storing unmanned aircraft and other flight devices or projectiles are described. In one embodiment, the aircraft can be assembled from a container with little or no manual engagement by an operator. The container can include a guide structure to control motion of the aircraft components. The aircraft can be launched from an apparatus that includes an extendable boom. The boom can be extended to deploy a recovery line to capture the aircraft in flight. The aircraft can then be returned to its launch platform, disassembled, and stored in the container, again with little or no direct manual contact between the operator and the aircraft.
摘要翻译： 描述了用于发射，捕获和存储无人机和其他飞行装置或射弹的方法和装置。 在一个实施例中，飞行器可以由操作者很少或没有手动接合的容器组装。 容器可以包括用于控制飞机部件的运动的引导结构。 飞机可以从包括可伸缩吊杆的装置发射。 可以扩展繁荣部署一个恢复线，以便在飞行中捕获飞机。 飞机然后可以返回到其发射平台，拆卸并存储在容器中，再次与操作员和飞机之间的很少或没有直接的手动接触。
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公开(公告)号：US07028949B2
公开(公告)日：2006-04-18
申请号：US10860474
申请日：2004-06-03
IPC分类号： B64F1/12
CPC分类号： B64C25/00 , B64C1/062 , B64C25/10 , B64C25/32 , B64C25/68 , B64C27/04 , B64C2025/325 , B64C2211/00
摘要： An aircraft landing assist apparatus is designed to be retrofit to existing aircraft having internal constructions that have been modified to support the apparatus. The apparatus is designed so that on rough landings of the aircraft on a ship deck, the apparatus will collapse in a controlled manner to avoid any damage to ammunition and/or fuel storage areas of the aircraft.
摘要翻译： 飞机着陆辅助装置被设计成对已经被修改以支持该装置的内部结构的现有飞机进行改装。 设备的设计使得在飞机甲板上的飞机粗糙上升时，设备将以受控的方式倒塌，以避免对飞机的弹药和/或燃料储存区域造成任何损坏。
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公开(公告)号：US20050269449A1
公开(公告)日：2005-12-08
申请号：US10860474
申请日：2004-06-03
申请人： Neal Muylaert , Darrin Tebon , Rolland Lahaie , William Lindsay
发明人： Neal Muylaert , Darrin Tebon , Rolland Lahaie , William Lindsay
CPC分类号： B64C25/00 , B64C1/062 , B64C25/10 , B64C25/32 , B64C25/68 , B64C27/04 , B64C2025/325 , B64C2211/00
摘要： An aircraft landing assist apparatus is designed to be retrofit to existing aircraft having internal constructions that have been modified to support the apparatus. The apparatus is designed so that on rough landings of the aircraft on a ship deck, the apparatus will collapse in a controlled manner to avoid any damage to ammunition and/or fuel storage areas of the aircraft.
摘要翻译： 飞机着陆辅助装置被设计成对已经被修改以支持该装置的内部结构的现有飞机进行改装。 设备的设计使得在飞机甲板上的飞机粗糙上升时，设备将以受控的方式倒塌，以避免对飞机的弹药和/或燃料储存区域造成任何损坏。
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