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公开(公告)号：WO2017069331A1
公开(公告)日：2017-04-27
申请号：PCT/KR2015/013121
申请日：2015-12-03
Applicant: 서울시립대학교 산학협력단
IPC: B64B1/00 , B64B1/06 , B64B1/24 , B64B1/58 , B64B1/40 , C01B3/04 , B64D41/00 , B64D47/00 , F17C5/00 , B64B1/36
CPC classification number: B64B1/00 , B64B1/06 , B64B1/24 , B64B1/36 , B64B1/40 , B64B1/58 , B64D41/00 , B64D47/00 , C01B3/04 , F17C5/00
Abstract: 본 발명은 수소 리싸이클 비행 시스템 및 비행방법에 관한 것으로, 몸체의 양측에 적어도 한 쌍의 날개를 갖는 비행동체와, 상기 비행동체에 기밀 연결되는 수소가스벌룬과, 상기 수소가스벌룬과 연결되고, 상기 비행동체 외부 또는 내부에 설치되는 수소연료전지와, 상기 수소연료전지로부터 생산된 전기 또는 비행동체 외주부에 구비된 태양전지로부터 생산된 전기 또는 외부 전력망 전기로 충전되는 2차전지를 포함하며, 스위치 전환으로 수소연료전지를 물전기분해장치로 또는 물전기분해장치를 수소연료전지로 전환하고, 상기 수소연료전지로부터 생성된 물을 저장하는 물탱크, 상기 저장된 물을 전기분해하는 상기 물전기분해장치와, 수소연료전지와 물전기분해장치의 기능전환을 위한 스위치 제어장치와, 물전기분해장치에서 생산된 수소가스와 산소가스를 고압저장하기 위한 고압가스통과, 비행체의 부양동력인 상기 수소가스벌룬의 부피가 상기 수소연료전지의 작동 또는 상기 고압가스통에 의해 제어되어 비행하는 것을 특징으로 한다.
Abstract translation:
本发明涉及一种氢气循环飞行系统和飞行方法，和氢气气球是在飞行中，与具有至少在主体的任一侧上的一对翼，气密联接到飞行体的主体，其中 2与氢气气球相连，并充入电或从设置在从氢燃料电池所产生的外周部的电或飞行体的太阳能电池产生的外部电网的电力，氢燃料电池被安装在外部或内部的飞行体的 腿包括是否氢燃料电池的一个开关转换为水电解槽或作为水的电解的氢的燃料电池装置，和水箱，储存的水，电的分解，其存储由所述氢燃料电池所产生的水 一种用于切换氢燃料电池和水电解装置功能的开关控制装置， 其特征在于，所述高压气瓶，车辆到高压储存氢气和氧气飞由操作或氢燃料电池的高压气体流路控制的氢气气球的体积的相关功率。
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公开(公告)号：WO1980000825A1
公开(公告)日：1980-05-01
申请号：PCT/US1979000860
申请日：1979-10-18
Applicant: AIRSHIPS INT INC
Inventor： AIRSHIPS INT INC , PAVLECKA V
IPC: B64B01/26
Abstract: The object of this invention is to provide thruster control for an airship. The use of thrusters (12, 14, 16, 18, 20, 22, 24, 26) at the bow and stem of an airship for control of the direction, attitude, and orientation of such an airship is described. The thruster utilizes an electric motor (50) or a gas turbine (160, 162) for power. In the electric motor (50) embodiment, the motor (50) utilizes two contra-rotating rotors (110, 112) which each drive a separate and contra-rotating propeller (132, 134) to generate the controlling jet of air. Thrusters (12, 14, 16, 18, 20, 22, 24, 26) are arranged in pairs at the top, bottom, and each side of the bow and stem of the airship. Lifting thrusters (152, 154) directed downwardly and located above the longitudinal extent of the hull are provided to augment the static lift capability of the airship when under heavy load.
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公开(公告)号：WO2009023114A2
公开(公告)日：2009-02-19
申请号：PCT/US2008009453
申请日：2008-08-07
Applicant: LTA CORP , BALASKOVIC PIERRE
Inventor： BALASKOVIC PIERRE
Abstract: A system for controlling yaw associated with an airship may include one or more vertical control surfaces associated with the airship, a first power source and a second power source, each configured to provide a thrust associated with the airship, and a yaw control configured to receive an input indicative of a desired yaw angle. The system may further include a controller communicatively connected to the yaw control, the one or more vertical control surfaces, and the first and second power sources. The controller may be configured to receive an output signal from the yaw control corresponding to the desired yaw angle and to generate a control signal configured to modify a state associated with at least one of the one or more vertical control surfaces, the first power source, and the second power source, such that the airship substantially attains the desired yaw angle.
Abstract translation: 用于控制与飞艇相关联的偏航的系统可以包括与飞艇相关联的一个或多个垂直控制表面，第一电源和第二电源，每个被配置为提供与飞艇相关联的推力，以及偏航控制，被配置为接收 指示期望的偏航角的输入。 系统还可以包括通信地连接到偏航控制器，一个或多个垂直控制表面以及第一和第二电源的控制器。 控制器可以被配置为从对应于期望的偏航角的偏航控制接收输出信号，并且产生控制信号，该控制信号被配置为修改与一个或多个垂直控制表面，第一电源， 和第二动力源，使得飞艇基本上达到所需的偏航角。
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公开(公告)号：WO2008025139A1
公开(公告)日：2008-03-06
申请号：PCT/CA2007/001505
申请日：2007-08-27
Applicant: SKYHOOK INTERNATIONAL INC. , JESS, Peter, E.
Inventor： JESS, Peter, E.
Abstract: A hybrid lift air vehicle for lifting and transporting a payload to a delivery location, which comprises a helium or other lighter-than-air gas filled envelope mounted on an airframe. Variable and reversible vertical thrusters are positioned on the airframe, and at least two variable and reversible lateral thrusters are mounted on the envelope or mounted on truss arms attached and extending out from the airframe, wherein, when the vehicle is connected to the payload for transport, the helium or other lighter-than-air gas supports or substantially supports the weight of the vehicle and the vertical thrusters are then continuously engaged to support the weight of the payload and to provide lift to the payload, wherein the lateral thrusters are then engaged to effect lateral movement of the vehicle to the delivery location, whereby, once at the delivery location, the lift provided by the variable and reversible vertical thrusters is reduced or reversed so as to allow the air vehicle to descend and the payload to again engage the ground surface, and where necessary, the variable and reversible vertical thrusters may be reversed to facilitate the unloading of the payload from the vehicle, the vehicle continuing to be kept aloft, once unloaded, by the helium or other lighter than air gas. In this manner, the vehicle utilizes the helium or lighter than air gas to offset or substantially offset the weight of the vehicle, the vertical thrusters providing the power to lift the payload.
Abstract translation: 一种用于将有效载荷提升和运送到输送位置的混合式提升空气车辆，其包括安装在机身上的氦气或其他轻于空气的气体填充的信封。 可变和可逆的垂直推进器定位在机身上，并且至少两个可变和可逆的侧向推进器安装在信封上或安装在从机身附接和延伸出的桁架臂上，其中，当车辆连接到有效载荷以用于运输 ，氦气或其他轻型空气气体支撑或基本上支撑车辆的重量，然后连续地接合垂直推进器以支撑有效载荷的重量并且向有效载荷提供升力，其中侧向推进器然后接合 以实现车辆向输送位置的横向移动，由此，一旦在输送位置处，由可变和可逆的垂直推进器提供的升力被减小或反转，以便允许空中客车下降并且有效载荷再次接合 地面，并且在必要时，可变和可逆的垂直推进器可以反向以便于有效载荷的卸载 从车辆起，车辆继续高空，一旦卸载，氦气或其他比空气更轻的轻型车辆。 以这种方式，车辆利用比空气气体的氦气或轻质气体来抵消或基本上抵消车辆的重量，垂直推进器提供提升有效载荷的动力。
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公开(公告)号：WO2008097136A1
公开(公告)日：2008-08-14
申请号：PCT/RU2008/000068
申请日：2008-02-05
Applicant: ХАКИМОВ Борис Васильевич , ЧЕРНИКОВ Александр Николаевич , ДЕМИДОВ Герман Викторович , ХАМИТОВ Рустем Закиевич
Inventor： ХАКИМОВ Борис Васильевич , ЧЕРНИКОВ Александр Николаевич , ДЕМИДОВ Герман Викторович , ХАМИТОВ Рустем Закиевич
CPC classification number: A62C29/00 , A62B5/00 , B64B1/20 , B64B1/36 , B64B2201/00
Abstract: Изобретение относится к летательным аппаратам легче воздуха. Летательный аппарат имеет жесткий корпус, внутри которого расположены оболочки с несущим газом, движители внутри аэродинамических модулей в виде тел вращения тороидальной формы с аэродинамическим профилем. В нижней части корпуса выполнен сквозной продольный проход, соединяющий кабину экипажа, грузопассажирский салон, топливные баки и агрегаты, оборудованный выходными люками и устройствами для причаливания к внешним объектам, выдвижным трапом с перилами и съемной тележкой. Имеется поперечный проход с выходами на крылья и вертикальный проход, оборудованный лебедкой и устройствами для спуска-подъема. Нижняя часть корпуса и полые крылья заполнены пенопластом, обеспечивающим плавучесть и прочность летательного аппарата. Изобретение направлено на расширение арсенала технических средств.
Abstract translation: 本发明涉及轻型轻型车辆。 本发明的飞行器包括具有载气包壳的刚体和布置在空气动力学模块内部的推进器，其以空气动力学形式的环形旋转体形式体现。 身体的下部具有纵向通道，以使其与乘员舱，货物和乘客舱，燃料箱和附件通信，并且设置有用于对接到外部物体的出口舱口和设备， 带有栅栏和可拆卸车厢的可延伸楼梯。 该飞机还包括一个具有俯仰出口的横向通道和一个设有电缆葫芦的垂直通道和用于降低和提升人员和货物的装置。 身体的下部和空心翼充满泡沫塑料，用于为飞行器提供浮动性和强度。 本发明的目的是扩展技术手段的清单。
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Patent Agency Ranking
公开(公告)号：WO2004087499A2
公开(公告)日：2004-10-14
申请号：PCT/GB2004/001488
申请日：2004-04-05
Applicant: LUFFMAN, Charles, Raymond
Inventor： LUFFMAN, Charles, Raymond
IPC: B64B
Abstract: An airship comprising an envelope and a ballonet positioned within the envelope. Drive means is provided for supplying lateral thrust for the airship, to improve lateral control of the airship. The drive means has a dual function as it has an air supply system with an air inlet provided at the bow of the envelope of the airship for supplying air to the balonet to aid pressurisation. A mooring system and detachable gondola is also disclosed.
Abstract translation: 飞艇包括一个位于信封内的信封和一个气球。 提供用于为飞艇提供侧向推力的驱动装置，以改善飞艇的横向控制。 驱动装置具有双重功能，因为其具有空气供应系统，空气入口设置在飞艇的信封的弓部处，用于将空气供应到支架以辅助加压。 还公开了一种系泊系统和可拆卸的缆车。
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7.发明申请AUTONOMOUS INTELLIGENCE SURVEILLANCE RECONNAISSANCE AND PAYLOAD DELIVERY SYSTEM AND METHOD OF USING SAME 审中-公开自动智能监控和付费交付系统及其使用方法
公开(公告)号：WO2013112198A2
公开(公告)日：2013-08-01
申请号：PCT/US2012/049790
申请日：2012-08-06
Applicant: SILICIS TECHNOLOGIES, INC. , STIGLER, Michael, J. , SETAR, Nicholas, James
Inventor： STIGLER, Michael, J. , SETAR, Nicholas, James
IPC: B26D1/00
CPC classification number: B64B1/12 , B64B1/005 , B64B1/10 , B64B1/14 , B64B1/18 , B64B1/22 , B64B1/24 , B64B1/36 , B64B1/60 , B64B1/62 , B64B1/64 , B64B1/66 , B64C39/024 , B64C2201/022 , B64C2201/126 , B64C2201/127 , B64C2201/141 , G05D1/0027 , G05D1/101 , G08G5/0069 , G09F21/04 , G09F21/06
Abstract: An intelligence, surveillance, and reconnaissance system is disclosed including a ground station and one or more aerial vehicles. The aerial vehicles are autonomous systems capable of communicating intelligence data to the ground station and be used as part of a missile delivery package. A plurality of aerial vehicles can be configured to cast a wide net of reconnaissance over a large area on the ground including smaller overlapping reconnaissance areas provided by each of the plurality of the aerial vehicles.
Abstract translation: 披露了一个智能，监视和侦察系统，包括地面站和一个或多个空中飞行器。 飞行器是能够将情报数据传送到地面站的自主系统，并用作导弹发射包的一部分。 多个飞行器可以被配置为在地面上的大面积上施放广泛的侦察网，包括由多个飞行器中的每一个提供的较小的重叠侦察区域。
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公开(公告)号：WO2009023114A8
公开(公告)日：2009-05-22
申请号：PCT/US2008009453
申请日：2008-08-07
Applicant: LTA CORP , BALASKOVIC PIERRE
Inventor： BALASKOVIC PIERRE
Abstract: A system for controlling yaw associated with an airship may include one or more vertical control surfaces associated with the airship, a first power source and a second power source, each configured to provide a thrust associated with the airship, and a yaw control configured to receive an input indicative of a desired yaw angle. The system may further include a controller communicatively connected to the yaw control, the one or more vertical control surfaces, and the first and second power sources. The controller may be configured to receive an output signal from the yaw control corresponding to the desired yaw angle and to generate a control signal configured to modify a state associated with at least one of the one or more vertical control surfaces, the first power source, and the second power source, such that the airship substantially attains the desired yaw angle.
Abstract translation: 用于控制与飞艇相关的偏航的系统可以包括与飞艇相关联的一个或多个垂直控制表面，第一动力源和第二动力源，每个构造成提供与飞艇相关联的推力，以及偏航控制器，配置为接收 指示期望的偏航角的输入。 该系统可以进一步包括通信地连接到偏航控制器，一个或多个竖直控制表面，以及第一和第二动力源的控制器。 控制器可以被配置为从对应于期望偏航角的偏航控制接收输出信号并且生成控制信号，该控制信号被配置为修改与一个或多个垂直控制表面，第一动力源， 和第二动力源，使得飞艇基本上达到期望的偏航角。
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9.发明申请AERONEF PLUS LEGER QUE L'AIR COMPRENANT PLUSIEURS BALLONS RELIES PAR UN CHASSIS, 审中-公开包含几个连接在一起的几个气球的非空中飞机
公开(公告)号：WO2004002819A1
公开(公告)日：2004-01-08
申请号：PCT/FR2003/001983
申请日：2003-06-26
Applicant: BERTHOLET, Christophe , MARCHEGAY, Anne , LOUSTAUDAUDINE, Christophe , LE ROUX, Pascal
Inventor： LOUSTAUDAUDINE, Christophe , LE ROUX, Pascal
IPC: B64B1/06
Abstract: L'invention concerne le domaine de l'aéronautique. Plus précisément, l'invention concerne un aéronef plus léger que l'air. Selon l'invention l'aéronef comprend au moins deux ballons 1 reliés entre eux par des moyens de liaison formant châssis 2.
Abstract translation: 本发明涉及航空领域。 更准确地说，本发明涉及一种比空中飞行的飞机。 本发明的特征在于，飞行器包括通过形成底盘（2）的连接装置相互连接的两个气球（1）。
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公开(公告)号：WO2018138112A1
公开(公告)日：2018-08-02
申请号：PCT/EP2018/051651
申请日：2018-01-24
Applicant: CARPE ASTRA LIMITED
Inventor： CARLTON, Alex , BINCE, Richard
Abstract: The invention relates to a flying craft (8, 98, 298, 308, 318) comprising lighter than air gas in a receptacle for creating a lifting force by means of buoyancy and a thrust force by combustion in combustion engine as a fuel together with oxygen from an ambient air collector. The invention also relates to a method of operating such a flying craft (8, 98, 298, 308, 318).
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