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公开(公告)号：US20180319476A1
公开(公告)日：2018-11-08
申请号：US15774266
申请日：2016-11-04
Inventor： Luciano da Silveira Araujo
CPC classification number: B64B1/34 , B64C27/08 , B64C39/024 , B64C2201/022 , B64C2201/101 , B64C2201/108 , B64C2201/146 , G05D1/00
Abstract: Unmanned and remotely controlled airship constituted from system of multirotor combined with inflatable envelope. The airship may be lifted/powered by a power system comprising three or more rotors. In some embodiments, the airship may be constructed using rods, connectors, the main system/control box and the rotors. The airship system may have a systemic symmetry for weight distribution and flight control and may be, for example, a symmetric ellipsoid envelope/blimp.
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公开(公告)号：US20180079479A1
公开(公告)日：2018-03-22
申请号：US15824748
申请日：2017-11-28
Applicant: EGAN AIRSHIPS, INC.
Inventor： James C. Egan , Joel D. Egan
IPC: B64B1/20 , B64C39/02 , B64B1/14 , B64B1/34 , B64B1/70 , B64B1/58 , B64B1/38 , B64B1/30 , B64B1/28 , B64B1/22 , B64B1/60
CPC classification number: B64B1/20 , B64B1/14 , B64B1/22 , B64B1/28 , B64B1/30 , B64B1/34 , B64B1/38 , B64B1/58 , B64B1/60 , B64B1/70 , B64B2201/00 , B64C39/024 , B64C2201/022 , B64C2201/101 , B64C2201/104
Abstract: A hybrid VTOL vehicle having an envelope configured to provide hydrostatic buoyancy, a fuselage attached to the envelope and having at least one pair of wings extending from opposing sides thereof to produce dynamic lift through movement, and a thrust generation device on each wing and configured to rotate with each wing about an axis that is lateral to a longitudinal axis of the envelope to provide vertical takeoff or landing capabilities. Ideally, the envelope provides negative hydrostatic lift to enhance low-speed and on-the-ground stability. A vehicle comprising a first lift device capable of providing hydrostatic lift; a second lift device capable of providing dynamic lift through movement; and a system structured to generate thrust coupled to the second lift device, the second lift device and the thrust generation system capable of rotating together about an axis that is lateral to a longitudinal axis of the vehicle at angles at least in the range of 90 degrees to and including 180 degrees.
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公开(公告)号：US09856007B2
公开(公告)日：2018-01-02
申请号：US14898708
申请日：2014-06-26
Applicant: Egan Airships, Inc.
Inventor： James C. Egan , Joel D. Egan
IPC: B64B1/20 , B64B1/14 , B64B1/22 , B64B1/28 , B64B1/30 , B64B1/38 , B64B1/58 , B64B1/70 , B64C39/02 , B64B1/34 , B64B1/60
CPC classification number: B64B1/20 , B64B1/14 , B64B1/22 , B64B1/28 , B64B1/30 , B64B1/34 , B64B1/38 , B64B1/58 , B64B1/60 , B64B1/70 , B64B2201/00 , B64C39/024 , B64C2201/022 , B64C2201/101 , B64C2201/104
Abstract: A hybrid VTOL vehicle having an envelope configured to provide hydrostatic buoyancy, a fuselage attached to the envelope and having at least one pair of wings extending from opposing sides thereof to produce dynamic lift through movement, and a thrust generation device on each wing and configured to rotate with each wing about an axis that is lateral to a longitudinal axis of the envelope to provide vertical takeoff or landing capabilities. Ideally, the envelope provides negative hydrostatic lift to enhance low-speed and on-the-ground stability.
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公开(公告)号：US20170029097A1
公开(公告)日：2017-02-02
申请号：US15062871
申请日：2016-03-07
Inventor： Hiroyuki MATSUMOTO , Shigenori ICHIMURA , Tatsuya IYOBE , Mizuki TAKITA
CPC classification number: B64C27/006 , B64B1/14 , B64B1/26 , B64B1/40 , B64B1/58 , B64C27/20 , B64C39/024 , B64C2201/022 , B64C2201/027 , B64C2201/042 , B64C2201/101 , B64C2201/108 , B64C2201/127 , B64D47/04 , B64D47/08 , B64D2203/00
Abstract: An aircraft includes: a plurality of rotor units each including a propeller and a motor that drives the propeller; and a shock absorber covering the entire vertical length of lateral sides of the plurality of rotor units.
Abstract translation: 飞机包括：多个转子单元，每个转子单元包括驱动推进器的螺旋桨和马达; 以及覆盖所述多个转子单元的横向侧的整个垂直长度的减震器。
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公开(公告)号：US20160200235A1
公开(公告)日：2016-07-14
申请号：US14912474
申请日：2014-09-11
Applicant: SILICIS TECHNOLOGIES, INC.
Inventor： Michael J. Stigler , Nicholas James Setar
CPC classification number: B60P3/11 , B60P7/06 , B60P7/0876 , B64B1/10 , B64B1/50 , B64B1/58 , B64B1/66 , B64C39/022 , B64C39/024 , B64C2201/022 , B64C2201/06 , B64C2201/101 , B64C2201/12 , B64C2201/121 , B64C2201/125 , B64C2201/127 , B64C2201/148 , B64C2201/208 , B64F1/14 , B64F3/02 , G08C17/02
Abstract: The disclosed embodiments include a trailer for an autonomous vehicle controlled by a command and control interface. The trailer includes a trailer body configured to retain the autonomous vehicle in an undeployed configuration. The trailer also anchors the autonomous vehicle in a deployed configuration. A tether is provided having a first end coupled to the trailer body and a second end that is configured to couple to the autonomous vehicle. A winch is utilized to adjust a length of the tether to move the autonomous vehicle between the undeployed configuration and deployed configuration. Further, a communication system communicates with the command and control interface and the autonomous vehicle to control movement of the autonomous vehicle between the undeployed configuration and deployed configuration.
Abstract translation: 所公开的实施例包括用于由命令和控制接口控制的自主车辆的拖车。 拖车包括拖车主体，其构造成将自主车辆保持在未部署的构造中。 拖车还以部署的配置锚定自主车辆。 提供了系绳，其具有联接到拖车主体的第一端和被配置为联接到自主车辆的第二端。 使用绞盘来调节系绳的长度以在未部署的配置和部署配置之间移动自主车辆。 此外，通信系统与命令和控制界面以及自主车辆进行通信，以控制自动车辆在未部署配置和部署配置之间的移动。
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Patent Agency Ranking
16.发明申请SYSTEM AND METHOD FOR GAS AND, OPTIONALLY, LIQUID CARGO TRANSPORTATION BY AIR 审中-公开用于气体的方法和方法，空气中的液体运输公开(公告)号：US20160075422A1
公开(公告)日：2016-03-17
申请号：US14833159
申请日：2015-08-24
Applicant: Leonid Goldstein
Inventor： Leonid Goldstein
CPC classification number: B64B1/00 , B64B1/66 , B64B1/70 , B64C39/024 , B64C2201/022 , B64C2201/101 , B64C2201/128 , B64F1/14
Abstract: A system and a method for gas transportation by air, in which the transported gas also creates at least some of the lift for the airship, transporting it. In the same time, a fluid cargo, which also serves as ballast, is loaded. One of the options is that some of the transported gas is carried in a compressed form within a strong vessel on the airship. Among other options for the fluid cargo is the same gas in liquefied form, sea water, fresh or brackish water, LPG and oil. Yet another option is carrying easily liquefied gas, which is evaporated and fills in the airship envelope on its way back. Other embodiments are disclosed, such as cooling the transported gas or using heated air or steam when the transported gas is unloaded. A network of airships, terminals and control stations for natural gas transportation by air and more can be used with multiple airships of this kind.
Abstract translation: 一种用于通过空气进行气体输送的系统和方法，其中所运送的气体还至少产生一部分用于飞艇的升降机运送。 同时，也装载了也用作镇流器的流体货物。 其中一个选择是，一些运输的气体以压缩的形式运载在飞艇上的强大的船只内。 流体货物的其他选择是液化形式的相同气体，海水，新鲜或微咸水，液化石油气和油。 另一种选择是携带容易的液化气体，其被蒸发并在其返回的路上填充飞艇信封。 公开了其它实施例，例如当运输的气体被卸载时冷却所输送的气体或使用加热的空气或蒸汽。 航空天然气运输飞艇，码头和控制站网络可与多台此类飞艇配合使用。
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公开(公告)号：US20140284422A1
公开(公告)日：2014-09-25
申请号：US13848443
申请日：2013-03-21
Applicant: Itzhak Sapir
Inventor： Itzhak Sapir
IPC: B64B1/00
CPC classification number: B64B1/24 , B64B1/40 , B64B1/62 , B64C2201/022 , B64C2201/101 , B64C2201/121 , B64C2201/123
Abstract: A hovering surveillance device. An electronic imaging device is disposed on a housing having a primary lift element, at least one compressed lighter-than-air gas element, a pitch adjustment element, and, a steering element. The compressed lighter-than-air gas is channeled to the primary lift element and the pitch adjustment element to selectively vary the altitude and angle for the housing such that scene of interest may be imaged. The lighter-than-air gas may be selected from the group of helium, hydrogen, heated air, neon, ammonia, and methane.
Abstract translation: 悬停监视装置。 电子成像装置设置在具有主提升元件的壳体上，至少一个压缩的轻质空气气体元件，俯仰调节元件和转向元件。 压缩的轻型空气气体被引导到主提升元件和俯仰调节元件以选择性地改变壳体的高度和角度，使得可以对感兴趣的场景进行成像。 轻于空气的气体可以选自氦气，氢气，加热空气，氖气，氨气和甲烷。
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公开(公告)号：US08536501B2
公开(公告)日：2013-09-17
申请号：US10692039
申请日：2003-10-22
Applicant: Minas Tanielian
Inventor： Minas Tanielian
CPC classification number: B64C39/024 , B64C2201/022 , B64C2201/027 , B64C2201/042 , B64C2201/084 , B64C2201/101 , B64C2201/108 , B64C2201/127 , B64C2201/128 , B64C2201/146 , B64C2201/162 , B64C2201/208 , B64D2211/00 , G05D1/0022 , H02J7/025 , H02J17/00 , H02J50/30 , H02J50/50 , H02J50/90 , Y02T50/55
Abstract: The present invention provides a position control system for a remote-controlled vehicle, a vehicle operated by the control system, and a method for operating a remote-controlled vehicle. An electromagnetic energy receiver is configured to receive an electromagnetic beam. The electromagnetic energy receiver is further configured to determine a position of the remote-controlled vehicle relative to a position of the electromagnetic beam. The vehicle is directed to maneuver to track the position of the electromagnetic beam.
Abstract translation: 本发明提供了一种用于遥控车辆的位置控制系统，由控制系统操作的车辆以及用于操作遥控车辆的方法。 电磁能量接收器被配置为接收电磁波束。 电磁能量接收器还被配置为确定遥控车辆相对于电磁波束的位置的位置。 车辆被引导以操纵以跟踪电磁波束的位置。
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19.发明授权公开(公告)号：US07776295B2
公开(公告)日：2010-08-17
申请号：US12380729
申请日：2009-03-02
Applicant: Detlev Konigorski
Inventor： Detlev Konigorski
CPC classification number: B64B1/20 , B01D53/002 , B01D2257/2025 , B01D2257/2064 , B01D2259/4558 , B64B2201/00 , B64C2201/022 , B64C2201/101 , B64C2201/125 , Y10S244/90
Abstract: An apparatus for removing harmful gas components out of the earth's atmosphere is a free-flying autonomous lightweight aircraft with an onboard gas processing system including gas separation or extraction devices, and inlets and outlets connected to the devices. Solar cells and/or thermoelectric generators provided on the craft produce electrical energy to operate the individual devices. The system may include a cryogenic closed-loop circulation system that participates in liquefying the extracted gas components. The apparatus is preferably a lighter-than-air craft like a dirigible. A method of extracting harmful gas components from the atmosphere involves flying the apparatus at a prescribed altitude level and operating the gas processing system to remove the harmful gas component from the atmosphere, then returning the apparatus to earth to offload the liquefied stored harmful gas component.
Abstract translation: 用于将有害气体成分从地球大气中除去的装置是一种自由飞行的自主轻型飞机，其具有包括气体分离或提取装置在内的气体处理系统以及连接到装置的入口和出口。 设在船上的太阳能电池和/或热电发电机产生电能来操作各个装置。 该系统可以包括参与液化提取的气体组分的低温闭环循环系统。 该装置优选地是比较轻便的轻型飞行器。 从大气中提取有害气体成分的方法包括使设备以规定的高度水平飞行，并操作气体处理系统以从大气中除去有害气体成分，然后使设备返回到地面以卸载液化的存储的有害气体成分。
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公开(公告)号：US20090045284A1
公开(公告)日：2009-02-19
申请号：US11840607
申请日：2007-08-17
Applicant: Adam N. Chu
Inventor： Adam N. Chu
IPC: B64B1/00
CPC classification number: B64C39/024 , B64B1/02 , B64C2201/022 , B64C2201/101 , B64C2201/105 , B64C2201/107 , B64C2201/127 , B64C2201/165
Abstract: An orientation system is disclosed for a lighter-than-air aircraft having a lower stage suspended from an envelope. The orientation system includes cords interconnecting the envelope and the lower stage and means for adjusting the length of at least one of the cords between the lower stage and the envelope. Adjusting the length produces a shift in the angle of attack of the envelope with respect to the lower stage.
Abstract translation: 公开了一种具有从信封悬挂的较低级的轻型飞机的定向系统。 定向系统包括将信封和下层相互连接的绳索和用于调节下层和包封之间的至少一根帘线长度的装置。 调整长度会导致信封相对于下层的迎角发生偏移。
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