| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 1 | 一种可长期维型的气球结构 | CN202410880367.0 | 2024-07-02 | CN118665700A | 2024-09-20 | 苏浩东; 廖航; 房冠辉; 王智超; 王国庆 |
| 本发明提供了一种可长期维型的气球结构。包括骨架内胆、气球蒙皮和尼龙搭扣；所述气球蒙皮形成气球外形，提供气动阻力且自身具有抗撕裂能力；骨架内胆由充气管组成，起到支撑气球蒙皮的作用，尼龙搭扣用于连接骨架内胆与气球蒙皮；所述的骨架内胆在气球蒙皮破损时保持充气状态，保证结构外形不发生破坏性变化，且能保持87.5％以上的阻力特性。 | ||||||
| 2 | 包括内部隔墙的航空器 | CN201080062447.1 | 2010-11-30 | CN102741118B | 2015-04-08 | F·达泽特 |
| 本发明涉及一种航空器，该航空器包括结构元件，例如机身、机翼或机尾，该结构元件包括：壁，该壁将所述元件的内部与外部分离，并包括共同限定所述元件的内部容积的部分；以及至少一个结构隔墙（20），该结构隔墙将区域彼此分离，例如将前部容积（109）和后部容积（111）彼此分离，该隔墙包括至少一个挠性隔板（60）和不连续地支撑所述隔板的至少两个安装件，该隔板能够变形，该安装件优选地是刚性的。 | ||||||
| 3 | 包括内部隔墙的航空器 | CN201080062447.1 | 2010-11-30 | CN102741118A | 2012-10-17 | F·达泽特 |
| 本发明涉及一种航空器，该航空器包括结构元件，例如机身、机翼或机尾，该结构元件包括：壁，该壁将所述元件的内部与外部分离，并包括共同限定所述元件的内部容积的部分；以及至少一个结构隔墙（20），该结构隔墙将区域彼此分离，例如将前部容积（109）和后部容积（111）彼此分离，该隔墙包括至少一个挠性隔板（60）和不连续地支撑所述隔板的至少两个安装件，该隔板能够变形，该安装件优选地是刚性的。 | ||||||
| 4 | 一种新型平流层飞艇 | CN201610034230.9 | 2016-01-19 | CN105644762B | 2017-11-28 | 邓志诚 |
| 一种新型平流层飞艇，布局如下：一：内部超压单元为多个独立布置的充氦气囊，单元采用多层复合柔性材料拼接而成，单元安装了放气阀门、温度测量传感器、压差测量传感器、浮力测量传感器、安控装置等设备；二：外部整流蒙皮采用轻质材料拼接而成，蒙皮沿内部浮力单元形成流线外形，蒙皮不封闭；三：太阳能电池采用柔性电池直接铺设在外部整流蒙皮上；四：下部刚性结构采用轻质复合材料桁架架构，在结构的前后方安装矢量推进螺旋桨，在结构的左右两侧安装非矢量推进螺旋桨；五：设备吊舱集成在半密封的轻质碳纤维结构桁架上，通过热控系统实现对设备吊舱内部的温度调节；六：在桁架结构的底部安装气囊或蜂窝缓冲系统。 | ||||||
| 5 | 一种新型平流层飞艇 | CN201610034230.9 | 2016-01-19 | CN105644762A | 2016-06-08 | 邓志诚 |
| 一种新型平流层飞艇，布局如下：一：内部超压单元为多个独立布置的充氦气囊，单元采用多层复合柔性材料拼接而成，单元安装了放气阀门、温度测量传感器、压差测量传感器、浮力测量传感器、安控装置等设备；二：外部整流蒙皮采用轻质材料拼接而成，蒙皮沿内部浮力单元形成流线外形，蒙皮不封闭；三：太阳能电池采用柔性电池直接铺设在外部整流蒙皮上；四：下部刚性结构采用轻质复合材料桁架架构，在结构的前后方安装矢量推进螺旋桨，在结构的左右两侧安装非矢量推进螺旋桨；五：设备吊舱集成在半密封的轻质碳纤维结构桁架上，通过热控系统实现对设备吊舱内部的温度调节；六：在桁架结构的底部安装气囊或蜂窝缓冲系统。 | ||||||
| 6 | 激光辐照多功能光伏风电动力飞艇 | CN201920882351.8 | 2019-06-12 | CN210653611U | 2020-06-02 | 张毅; 尤良 |
| 本实用新型公开了一种激光辐照多功能光伏风电动力飞艇。包括艇皮、艇架、后艇囊、后起落架、安定面、后艇架、失量架、电机、蜗扇、舵面、太阳板、控制翼、前气囊、头罩、陀罗仪、射频器、仪器座、仰角仪、起落架、铆钉、航行仪、变速器、推进器、烟火器、航拍器、近激光器、远激光器、地形仪、吊舱、色谱泵、电容矩阵、锂电矩阵、电源、计算机、飞控器、驱动模块、失量控制器、艇翼控制器、无人机受能器、受能器。本实用新型解决了飞艇仅能单一使用发动机、太阳能、燃料电池，滞空时程小、人工影响大、不能同时利用光风能为动力实现长久滞空与多用途巡航、不能为其它飞行器、地面装置提供动力及空空、空地能量无线传输，属于多用途、绿色能源飞行器。 | ||||||
| 7 | Hybrid aircraft | JP51615697 | 1996-10-24 | JPH11513635A | 1999-11-24 | ボセ ハンス−ユーゲン |
| A hybrid aircraft having VTOL R-VTOL and S-STOL capabilities having a lifting body hull (1) and four wing sections (20) arranged in tandem which are pivotally moveable about their neutral axis. Each wing section has mounted thereon a pivotal propeller-rotor (21) assembly for providing thrust substantially in a range between horizontal and vertical. The wings and propellers are integrated to the hull by an outrigger designed to be very stiff and to distribute forces from the wings and propellers from the hull. The hull is shaped to provide aerodynamic lift in an airstream and to facilitate construction by minimizing the number of panels of differing curvature required. The hull is formed of a pressure tensioned frame covered with semi-rigid panels, a lower cladding frame and bow and stem cladding nose cones. The semi-rigid panels covering the frame are formed of gas-tight and abrasion resistant laminate material and are connected to the frame by means of an interface rib and latch system. The frame is formed of a plurality of curved elongate segments arranged in series orthogonal to the long axis of the hull and connected by means of torsion members. A turbo-electric drive system can be used to drive the aircraft. An advanced hybrid aircraft is also described having about 8 to 12 high speed fans in place of the propeller-rotors. <IMAGE> | ||||||
| 8 | AUTONOMOUS INTELLIGENCE SURVEILLANCE RECONNAISSANCE AND PAYLOAD DELIVERY SYSTEM AND METHOD OF USING SAME | US17725454 | 2022-04-20 | US20220242545A1 | 2022-08-04 | Michael J. STIGLER; Nicholas James SETAR |
| 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. | ||||||
| 9 | Airborne power station | US12128561 | 2008-05-28 | US07997532B2 | 2011-08-16 | Brian J. Tillotson |
| A system for generating power from sunlight collected substantially above the earth's surface comprises an airborne platform which supports an apparatus to collect sunlight, an apparatus to convert sunlight to electricity, and an apparatus to transmit the electricity to a selected location on the earth's surface. The airborne platform collects solar energy above the clouds and transmits the energy to a receiving station on the ground via a microwave transmission system, avoiding possible attenuating effects of clouds and pollution. | ||||||
| 10 | FLUGGERÄT | EP17732760.8 | 2017-05-31 | EP3464059A2 | 2019-04-10 | SINGER, Csaba |
| 11 | METHOD AND APPARATUS FOR LIGHTER-THAN-AIR AIRSHIP WITH IMPROVED STRUCTURE AND DELIVERY SYSTEM | EP20951786.1 | 2020-08-28 | EP4204300A4 | 2024-05-22 | BRUTOCO, Rinaldo S.; SHELTON, Robert H.; MERRITT, Shawn |
| A lighter-than-air airship has an exoskeleton constructed of spokes and hubs to create a set of connected hexagrams comprised of isosceles triangles wherein the spokes flex and vary in length to produce the slope of said airship's surface. In one embodiment, the exoskeleton connects to a nose cone that includes a cockpit cabin for controlling the airship's operation from a single location that can be physically separated from the exoskeleton in response to catastrophic events and for autonomous and/or remotely piloted operation. An improved means is also provided for landing and unloading cargo, and through use of unmanned aerial vehicles in another embodiment, the airship is configured for remote pickup, transport, delivery and return of payloads such as packages. In yet another embodiment, the airship provides a communications platform for beam form transmission and satellite signal relay, including in combination with the foregoing disclosed attributes. | ||||||
| 12 | SISTEMA, METODO Y APARATO MEJORADOS PARA FABRICACION DE AEROSTATOS USANDO ROBOTICA. | MX2024005984 | 2022-11-17 | MX2024005984A | 2024-08-27 | SHELTON ROBERT H; BRUTOCO RINALDO S; EVERMAN MICHAEL R |
| La invención propone un sistema, método y aparato para ayudar a ensamblar el marco, unir la piel, y realizar otras tareas en la fabricación de un aerostato y la construcción de otras estructuras que de otro modo serían desafiantes, ineficientes, o inadecuados para que los realicen los humanos, y/o que tradicionalmente requieren inversiones significativas en instalaciones de fabricación intensivas en capital. Se proponen varias modalidades en las que estas y otras tareas de fabricación recurrentes se pueden realizar de forma segura y eficiente con la ayuda de robots autónomos, semiautónomos y/o dirigidos por humanos, que actúan de forma independiente y en enjambres de robots. | ||||||
| 13 | METODO Y APARATO PARA AEROSTATO CON ESTRUCTURA Y SISTEMA DE ENTREGA MEJORADOS. | MX2023002440 | 2020-08-28 | MX2023002440A | 2023-05-19 | BRUTCOCO RINALDO S; SHELTON ROBERT H; MERRIT SHAWN |
| La invención se refiere a un aerostato tiene un exoesqueleto construido con radios y cubos para crear un conjunto de hexagramas conectados compuestos por triángulos isósceles en los que los radios se flexionan y varían en longitud para producir la pendiente de la superficie de tal aeronave. En una modalidad, el exoesqueleto se conecta a un morro de fuselaje que incluye una cabina de cabina para controlar la operación del dirigible desde una única ubicación que puede separarse físicamente del exoesqueleto en respuesta a eventos catastróficos y para operación autónoma y/o pilotada remotamente. También se proporciona un medio mejorado para aterrizar y descargar carga, y mediante el uso de vehículos aéreos no tripulados en otra modalidad, el dirigible está configurado para recogida, transporte, entrega y devolución remotos de cargas útiles tales como paquetes. En otra modalidad más, el dirigible proporciona una plataforma de comunicaciones para la transmisión en forma de haz y la retransmisión de señales de satélite, incluso en combinación con los atributos descritos anteriormente. | ||||||
| 14 | ITUB20154251 | 2015-10-09 | ITUB20154251A1 | 2017-04-09 | PETRUZZINO CHRISTIAN | |
| 15 | Castle in the air | AU2341995 | 1995-05-05 | AU2341995A | 1995-11-29 | LU GAO |
| 16 | Double skin airship construction - has skeletal support frame within gasbag to hold engine pods and cabins | FR7603086 | 1976-02-04 | FR2340243A1 | 1977-09-02 | |
| The hull of the airship is formed by a skeletal frame to control the shape and a double skinned airbag which is fastened to the frame, with one wall on the inside and one on the outside. The two skins are joined over the frame at set points to totally enclose the frame. This ensures that the shape of the hull is always retained no matter what the internal pressure. The skeletal frame also enables the enfine pods, cabins, etc, to be securely fastened to the hull in any desired position, for improved control. The rigid shape enables it to be steered in high winds etc. The frame can be in prefabricated sections so that any length of hull can be assembled. | ||||||
| 17 | Double skin airship construction - has skeletal support frame within gasbag to hold engine pods and cabins | DE2659401 | 1976-12-29 | DE2659401A1 | 1977-08-04 | LISOWSKI ADAM ING; BOTHE JURGEN ING; FECHNER JOSEPH; WITHEROW ROBERT G; AMOOS SERGE; RUETER LOREN L |
| The hull of the airship is formed by a skeletal frame to control the shape and a double skinned airbag which is fastened to the frame, with one wall on the inside and one on the outside. The two skins are joined over the frame at set points to totally enclose the frame. This ensures that the shape of the hull is always retained no matter what the internal pressure. The skeletal frame also enables the enfine pods, cabins, etc, to be securely fastened to the hull in any desired position, for improved control. The rigid shape enables it to be steered in high winds etc. The frame can be in prefabricated sections so that any length of hull can be assembled. | ||||||
| 18 | Double skin airship construction - has skeletal support frame within gasbag to hold engine pods and cabins | FR7540237 | 1975-12-31 | FR2337080A1 | 1977-07-29 | |
| The hull of the airship is formed by a skeletal frame to control the shape and a double skinned airbag which is fastened to the frame, with one wall on the inside and one on the outside. The two skins are joined over the frame at set points to totally enclose the frame. This ensures that the shape of the hull is always retained no matter what the internal pressure. The skeletal frame also enables the enfine pods, cabins, etc, to be securely fastened to the hull in any desired position, for improved control. The rigid shape enables it to be steered in high winds etc. The frame can be in prefabricated sections so that any length of hull can be assembled. | ||||||
| 19 | Aeronave | ES17732760 | 2017-05-31 | ES2881902T3 | 2021-11-30 | SINGER CSABA |
| Aeronave con una estructura de soporte (12) y una cubierta (10) que se extiende por la estructura de soporte (12) y se puede llenar con un gas, en donde las partes de la cubierta se pueden conectar entre sí a través de al menos un cierre de cremallera y la estructura de soporte (12) tiene una pluralidad de secciones de varilla o tubo (24 - 30) que definen un plano del tramo principal circular, elíptico o poligonal para la cubierta (10), caracterizada porque la concha (10) comprende dos mitades de concha que están conectadas fijamente entre sí en una región de conexión corta y se pueden desplegar en forma de concha cuando la al menos una cremallera está abierta. | ||||||
| 20 | СОЕДИНЕНИЕ ЭЛАСТИЧНЫХ ОБОЛОЧЕК С ЖЕСТКИМИ КОНСТРУКЦИЯМИ | RU2011135342 | 2011-08-25 | RU2011135342A | 2013-02-27 | |
| 1. Соединениеэластичныхоболочекс жесткимиконструкциями, включающеежесткуюконструкциюв видеполосыкромкижесткогоконструктивногоэлементакорпусасуднанавоздушнойподушкеи прикрепленнуюк нейс помощьюсоединительныхэлементовэластичнуюоболочкув видегибкогоограждениясуднанавоздушнойподушке, отличающеесятем, чтов качествесоединительныхэлементовиспользованыП-образныескобыизпрочногоупругогоматериала, концыножеккоторыхзагнутывнутрьскобыв видеупругихподпружиненныхзацеповдляфиксациискобы, приэтомполосакромкижесткогоконструктивногоэлементакорпусасуднаустановленав положении, близкомк нормалипоотношениюк краюоболочкив натянутомсостоянии, иимеетпарныеотверстияподножкискобс зацепами, расположенныевдольподлинесоединения, причемкромкаполотнищаэластичнойоболочкиподогнутаи закреплена, образуякарман, повнешнемукраюкотороговыполненыотверстия, совпадающиес отверстиямив полосекромкижесткойконструкции, черезкоторыев карманпродетыП-образныескобы, иихконцывставленыв соответствующиеответныеотверстияполосыкромкижесткогоконструктивногоэлементакорпусасуднаи вдвинутыв неговплотьдофиксациисоединениязащелкиваниемконцовупругихподпружиненныхзацепов.2. Соединениеэластичныхоболочекс жесткимиконструкциямипоп.1, отличающеесятем, чтокромкаполотнищаэластичнойоболочкиподогнутаи закрепленаклеевымлибосварнымшвом, либопрошитанитью, проволокойилитросиком. | ||||||
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