公开(公告)号：WO2016204180A1

公开(公告)日：2016-12-22

申请号：PCT/JP2016/067809

申请日：2016-06-15

Applicant: 中村 浩平

Inventor： 中村　浩平

IPC: B64B1/30 ,  B64C25/06 ,  B64C27/08 ,  B64C39/02

CPC classification number: B64B1/30 ,  B64B1/58 ,  B64C25/06 ,  B64C27/08 ,  B64C39/02 ,  B64C39/024 ,  B64C2201/022 ,  B64C2201/027 ,  B64C2201/101 ,  B64C2201/108 ,  B64C2201/127

Abstract: 【課題】　墜落リスクを低減して高い安全性を確保し、風の影響を抑制して移動制御を容易にし高い移動能力を発揮できる浮揚型飛行体を提供する。 【解決手段】　内部に空気より小さい比重のガスを密閉してなる浮揚機体と、この浮揚機体に垂直方向の推進力を付与する垂直推進用プロペラと、前記浮揚機体に水平方向の推進力を付与する水平推進用プロペラとを有し、前記浮揚機体は、水平方向の風の通り道が少なくとも２方向に形成されているとともに、その外周縁の角度が側面視で鋭角状に形成されている。

Abstract translation: [问题]提供一种浮力飞行体，以便降低风险，以确保高水平的安全性，并且通过减少风的影响以便发挥高水平的移动性，可以促进运动控制。 [解决方案]具有浮力主体的浮力飞行体，其中具有比空气小的比重的气体被密封，用于向浮力主体提供垂直推进的垂直推进推进器以及用于向浮力提供水平推进的水平推进推进器 主体，其中浮力主体至少在两个方向上形成水平风道，其外围边缘在侧视图中分别形成锐角。

公开(公告)号：WO2015170078A2

公开(公告)日：2015-11-12

申请号：PCT/GB2015051271

申请日：2015-05-01

Applicant: SPILLCONSULT LTD

Inventor： GAIR STUART DAVID

IPC: B64B1/50

CPC classification number: B64B1/50 ,  B64C39/022 ,  B64C39/024 ,  B64C2201/022 ,  B64C2201/027 ,  B64C2201/127 ,  B64C2201/148 ,  G03B15/006 ,  G03B37/04

Abstract: An aerial observation system is described and comprises a tethered aerial platform and a plurality of ground-based monitoring devices. The aerial platform carries a payload comprising a plurality of fixed focal length cameras mounted at selected positions about the aerial platform and communication means connected to the plurality of cameras for transmitting, independently to each of the plurality of ground-based monitoring devices, a data signal comprising image data captured by one or more of the plurality of cameras. Each ground-based monitoring device is independently operable to select and display an image area of interest from the image data contained in the data signal. By utilising fixed focal length cameras instead of the normal (but much heavier, more delicate and more power-hungry) pan, tilt and zoom cameras conventionally used in such application, sensor payload on the balloon can be reduced, robustness can be increased, and battery life improved. Moreover, multiple users are able to independently access different fields of view simply by selecting different image areas out of the image data transmitted (potentially to all base stations) from the aerial platform.

Abstract translation: 描述了一种空中观测系统，并包括一个系留式空中平台和多个基于地面的监视装置。 空中平台携带有效载荷，其包括安装在围绕天线平台的选定位置处的多个固定焦距照相机和连接到多个相机的通信装置，用于独立地向多个地面监视装置中的每一个发送数据信号 包括由所述多个照相机中的一个或多个捕获的图像数据。 每个基于地面的监视设备可独立地操作以从包含在数据信号中的图像数据中选择和显示感兴趣的图像区域。 通过利用固定焦距相机，而不是通常在这种应用中常规使用的正常（但更重，更精细和更耗电）的平底锅，倾斜和变焦相机，可以降低球囊上的传感器有效载荷，提高鲁棒性， 电池寿命提高。 此外，多个用户能够通过从空中平台中选择从所发射的图像数据（潜在地到所有基站）的不同图像区域来独立地访问不同的视场。

公开(公告)号：WO2014000729A2

公开(公告)日：2014-01-03

申请号：PCT/DE2013000352

申请日：2013-06-24

Applicant: EMAMI ARMAN

Inventor： EMAMI ARMAN

IPC: B64B1/44 ,  A63H27/10

CPC classification number: B64C39/024 ,  A63H27/10 ,  A63H2027/1066 ,  B64C2201/022 ,  B64C2201/042 ,  B64C2201/101 ,  B64C2201/162

Abstract: A flying robot (1) which is carried by a gas balloon for use in interior spaces is proposed, wherein the gas balloon (2) can be adjusted in such a way that a horizontal hovering height which is provided or predefined can be adjusted or implemented. Working devices (5) are located in a valve unit (3) and/or a housing which is arranged underneath the gas balloon (2). Together with the valve unit (3) or the housing, a drive unit (4) whose direction can be adjusted is provided with respect to said unit and said housing for moving the flying robot (1). The flying robot can be used both for monitoring tasks and for filming.

Abstract translation: 本发明公开了一个气体球载飞行机器人（1），用于内部空间的使用，其中所述气体球囊（2）是可调节的，使得预期的或预定的水平的浮动高度是可调节的或可行的。 在阀单元（3）和/或在气体球囊（2）布置在所述壳体如下工作装置（5）。 与阀单元（3）或所述壳体的飞行机器人（1）的移动相对地设置该一个方向上调节驱动单元（4）。 随着飞行机器人两种监测任务以及电影镜头可以实现的。

公开(公告)号：WO2012094716A1

公开(公告)日：2012-07-19

申请号：PCT/BR2012/000005

申请日：2012-01-16

Applicant: AVENA DE AZEVEDO, Bruno ,  MENDES NOGUEIRA, Leonardo

Inventor： AVENA DE AZEVEDO, Bruno ,  MENDES NOGUEIRA, Leonardo

IPC: H04W88/08 ,  B64B1/42 ,  H04B7/185

CPC classification number: B64B1/50 ,  B64C2201/022 ,  B64C2201/101 ,  B64C2201/122 ,  H04B7/18504 ,  H04W88/085

Abstract: Patente de Privilégio de Invenção para um sistema de células de radiocomunicação portáteis, leves e flexíveis para offload de tráfego de voz ou dados em eventos ou aglomeração de pessoas e ampliação rápida de área de cobertura compreendendo uma plataforma aeronáutica flutuante, denominada "CÉLULA FLUTUANTE" (20), que se comunica com estações móveis (21) através de uma ou mais modulações diferentes (25), incluindo tecnologias Wi-Fi, 2G, 3G e 4G, mas não limitadas a estas, e opcionalmente com estações de transmissão de solo (22) através de protocolo sem fio (24), que transportam a comunicação para a rede (23). A "CÉLULA FLUTUANTE" é compreendida por um invólucro (12) e seus acessórios, responsáveis pela sustentação da carga útil (19) e por um sistema de ancoragem portátil. A parte flutuante e a parte de solo se conectam através de um cabo de amarração (15). Na primeira vertente a "CÉLULA FLUTUANTE" funciona como um elemento de antena distribuída, transportando sinal RF sobre fibra óptica (radio over fiber), através do cabo de amarração (15). Na segunda vertente a "CÉLULA FLUTUANTE" embarca o sistema irradiante completo, com processamento e cabeça de RF, podendo ser uma combinação de Wi-Fi Access Points (AP) ou células miniaturizadas.

Abstract translation: 一种用于在事件或公众集会处卸载语音或数据业务并且快速增加覆盖区域的便携式，轻便和灵活的无线电通信小区系统的专利，包括被称为“浮动小区”（20）的浮动航空平台，其中 使用一个或多个不同的调制（25）与移动站（21）进行通信，包括但不限于Wi-Fi，2G，3G和4G技术，以及可选地使用无线协议（24）的地面传输站（22） 将通信传送到网络（23）。 “浮动细胞”包括用于支持有效载荷（19）的壳体（12）和相关附件以及便携式锚固系统。 浮动部分和接地部分通过系泊电缆（15）连接。 在第一方面，“浮动单元”用作分布式天线元件，其使用系泊电缆（15）承载无线电信号。 在第二方面，“浮动细胞”包含整个辐射系统，具有处理和RF头，其可以是Wi-Fi接入点（AP）或小型化小区的组合。

公开(公告)号：WO2012025769A1

公开(公告)日：2012-03-01

申请号：PCT/HR2011/000032

申请日：2011-08-19

Applicant: HIPERSFERA D.O.O. ,  PECNIK, Bojan

Inventor： PECNIK, Bojan

IPC: B64B1/06 ,  B64B1/08 ,  B64B1/30 ,  B64B1/58

CPC classification number: B64B1/08 ,  B64B1/06 ,  B64B1/30 ,  B64B1/58 ,  B64C2201/022 ,  B64C2201/122 ,  B64C2201/127

Abstract: Task of the invention is an autonomous stratospheric unmanned airship (10) with the operating altitude from 5 to 22 km and with the operational cycle measured in months. Spheroid rigid frame of constant volume is done as a geodesic frame (11) formed by a multitude of struts (28), with an outer envelope (12) enclosing the frame (11) defining the eigenfrequency spectrum of the airship (10) in the frequency range above 20 Hz, with the vibrational amplitudes between 0,1 and 1 cm. Independently controllable electrical propulsion units (14) are attached to the frame (11) in the horizontal plane passing through the center of mass, and can change the direction and the value of the thrust vector. Buoyancy is controlled with a system integrated inside the geodesic frame (11) consisting of pressurized tanks (23) containing buoyant fluid, valves (24) for the release of the buoyant fluid through the buoyant fluid conduit (26) into the buoyant gas cell (38) which by expansion fills the geodesic frame (11); and valves (18) placed at the subsystem support platform (17) enabling ambient atmosphere to fill the internal volume of the frame (11) not occupied by the buoyant gas cell (38). Additionally, inside the frame (11) is a power system comprised of batteries (32) and photovoltaic cells (13) placed at the upper part of the envelope (12). Besides the communication system (36, 37) and antennas (19, 20) airship has a control unit (32) and a specialized scientific equipment for various purposes placed at the platform (17) in a form of payload (34).

Abstract translation: 本发明任务是自主平流层无人飞艇（10），运行高度为5〜22公里，运行周期为月。 恒定体积的球体刚架作为由多个支柱（28）形成的测地线框架（11），封闭框架（11）的外壳（12）限定飞艇（10）的本征频谱 频率范围在20Hz以上，震动振幅在0.1和1cm之间。 独立可控的电动推进装置（14）在通过质心的水平面附接到框架（11），并可改变推力矢量的方向和值。 浮力由集成在测地框架（11）内的系统控制，该测地框架（11）由包含浮力流体的加压罐（23）组成，阀（24）用于通过浮力流体导管（26）将浮力流体释放到浮力气体池 38），其通过膨胀填充测地框架（11）; 以及放置在子系统支撑平台（17）处的阀（18），使得环境气氛能够填充未被浮力气室（38）占据的框架（11）的内部容积。 另外，在框架（11）的内部是由置于信封（12）的上部的电池（32）和光伏电池（13）组成的电力系统。 除了通信系统（36,37）和天线（19,20）之外，飞艇还具有控制单元（32）和用于各种目的的专用科学设备，以有效载荷（34）的形式放置在平台（17）。

公开(公告)号：WO2010027801A3

公开(公告)日：2010-05-27

申请号：PCT/US2009054917

申请日：2009-08-25

Applicant: UNIV FLORIDA ,  LIND CHARLES RICHARD JR ,  GRANT DANIEL THURMOND ,  EATON DAVID

Inventor： LIND CHARLES RICHARD JR ,  GRANT DANIEL THURMOND ,  EATON DAVID

IPC: B64C39/02 ,  B25J5/00 ,  B64C3/56 ,  B64C13/20 ,  B64C27/22

CPC classification number: B64C39/024 ,  B60F3/00 ,  B64C37/00 ,  B64C2001/0045 ,  B64C2201/022 ,  B64C2201/027 ,  B64C2201/102 ,  B64C2201/108 ,  B64C2201/203

Abstract: A morphing aircraft that is achieves multi- modality location and camouflage for payload emplacement The morphing aircraft includes a substantially cylindrical fuselage including a shape configured as a packaging container with a first end and a second end A set of wings is coupled to the fuselage The set of wings includes a first position where the set of wings is extended outwards from the fuselage and a second position where the set of wings is retracted inwards towards the fuselage A tail is coupled to the second end of the cylindrical fuselage The tail includes a first position where the tail is extended outward from the fuselage and a second position where the tail is retracted inward towards the fuselage A propeller is mounted to the first end of the fuselage An engine is mechanically coupled to the propeller The engine is enclosed within the fuselage and powers the propeller.

Abstract translation: 实现多模式位置和伪装用于有效载荷的变形飞机变形飞机包括基本上圆柱形的机身，其包括被配置为具有第一端和第二端的包装容器的形状。一组翼结合到机身。该组 的翼部包括第一位置，其中所述一组翼从机身向外延伸，并且第二位置，其中该组翼向内朝向机身A缩回。尾部联接到圆柱形机身的第二端。尾部包括第一位置 其中尾部从机身向外延伸，而第二位置则尾部朝向机身向内缩进。螺旋桨安装在机身的第一端。发动机机械地联接到螺旋桨发动机被封闭在机身内并且动力 螺旋桨

公开(公告)号：WO2010027801A2

公开(公告)日：2010-03-11

申请号：PCT/US2009/054917

申请日：2009-08-25

Applicant: UNIVERSITY OF FLORIDA RESEARCH FOUNDATION, INC. ,  LIND, Charles, Richard, Jr. ,  GRANT, Daniel, Thurmond ,  EATON, David

Inventor： LIND, Charles, Richard, Jr. ,  GRANT, Daniel, Thurmond ,  EATON, David

IPC: B64C39/02 ,  B64C13/20 ,  B64C27/22 ,  B64C3/56 ,  B25J5/00

CPC classification number: B64C39/024 ,  B60F3/00 ,  B64C37/00 ,  B64C2001/0045 ,  B64C2201/022 ,  B64C2201/027 ,  B64C2201/102 ,  B64C2201/108 ,  B64C2201/203

Abstract: A morphing aircraft that is achieves multi- modality location and camouflage for payload emplacement The morphing aircraft includes a substantially cylindrical fuselage including a shape configured as a packaging container with a first end and a second end A set of wings is coupled to the fuselage The set of wings includes a first position where the set of wings is extended outwards from the fuselage and a second position where the set of wings is retracted inwards towards the fuselage A tail is coupled to the second end of the cylindrical fuselage The tail includes a first position where the tail is extended outward from the fuselage and a second position where the tail is retracted inward towards the fuselage A propeller is mounted to the first end of the fuselage An engine is mechanically coupled to the propeller The engine is enclosed within the fuselage and powers the propeller.

Abstract translation: 实现用于有效载荷安置的多模式位置和伪装的变形飞行器变体飞机包括基本上圆柱形的机身，该机身包括被配置为包装容器的形状，该包装容器具有第一端和第二端， 机翼被耦合到机身。该组机翼包括第一位置和第二位置，其中该组机翼从机身向外延伸，在第二位置该组机翼朝向机身A向内缩回。尾部耦合到机身的第二端 圆柱形机身尾部包括尾部从机身向外延伸的第一位置和尾部朝着机身向内缩回的第二位置。螺旋桨安装到机身的第一端。发动机机械地耦合到螺旋桨上。 发动机封闭在机身内并为螺旋桨提供动力。

公开(公告)号：WO2009070402A1

公开(公告)日：2009-06-04

申请号：PCT/US2008/081217

申请日：2008-10-24

Applicant: THE BOEING COMPANY ,  KULESHA, Richard, L.

Inventor： KULESHA, Richard, L.

IPC: B64B1/08

CPC classification number: B64B1/06 ,  B64B1/08 ,  B64C2201/022

Abstract: An aerial load lifting system features a non-rigid or blimp-type dirigible providing a lighter-than-air envelope (10) that is placed within a structural shell (50). The system is designed so that the envelope provides essentially neutral buoyancy for the structure, leaving only the cargo weight (20) to be lifted by the rotors (200). The structural shell supports the engine (100), fuel tank (42), rotors, and transmission system (120) that power the lift and vectoring of the aircraft, in addition to supporting the cargo load. The structural shell transfers the weight of the load directly to the location of the rotors, thus avoiding stress on the envelope.

Abstract translation: 一种空中负载提升系统具有非刚性或微型飞行器，提供放置在结构壳体（50）内的轻于空气的空气封套（10）。 该系统被设计成使得外壳为结构提供基本上中性的浮力，仅留下货物重物（20）由转子（200）提升。 结构壳体除了支撑货物载荷之外还支撑为飞行器的提升和矢量化提供动力的发动机（100），燃料箱（42），转子和传动系统（120）。 结构外壳将负载的重量直接转移到转子的位置，从而避免了信封上的压力。

公开(公告)号：WO2009055109A1

公开(公告)日：2009-04-30

申请号：PCT/US2008/071230

申请日：2008-07-25

Applicant: NEAR SPACE SYSTEMS, INC. ,  CHU, Adam N.

Inventor： CHU, Adam N.

IPC: B64C13/30

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。

公开(公告)号：WO2004100289A3

公开(公告)日：2005-11-10

申请号：PCT/US2004013895

申请日：2004-05-05

Applicant: ION AMERICA CORP ,  MCELROY JAMES FREDERICK ,  SRIDHAR K R

Inventor： MCELROY JAMES FREDERICK ,  SRIDHAR K R

IPC: B64B1/62 ,  B64C39/02 ,  B64D27/24 ,  H01M20060101 ,  H01M8/04 ,  H01M8/12 ,  H01M8/18

CPC classification number: H01M8/186 ,  B64C39/024 ,  B64C2201/022 ,  B64C2201/042 ,  B64C2201/101 ,  B64C2201/127 ,  B64C2201/148 ,  B64C2201/165 ,  B64D27/24 ,  B64D2041/005 ,  B64D2211/00 ,  H01M8/04007 ,  H01M8/2475 ,  H01M2250/20 ,  Y02E60/528 ,  Y02T50/44 ,  Y02T50/62 ,  Y02T50/69 ,  Y02T90/32 ,  Y02T90/36 ,  Y10S429/901

Abstract: A neutrally buoyant airship, such as a blimp, contains a lifting body which allows the airship to remain neutrally buoyant in air and a fuel cell located in the airship. A method of generating power in the neutrally buoyant airship, comprising providing a fuel and a oxidizer to a solid oxide fuel cell to generate power, and providing heat from the fuel cell to a remotely located lifting body, wherein the lifting body allows the airship to remain neutrally buoyant in air.