| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 301 | Aircraft having buoyant gas balloon | JP13235193 | 1993-05-12 | JPH06135391A | 1994-05-17 | FUREDERITSUKU FUAAGUSON |
| PURPOSE: To improve the lift and drag obtained by a rotating balloon to obtain good flight characteristics by locating a gondola near the balloon surface and making the gondola top surface matched with the balloon surface. CONSTITUTION: An aircraft comprises a balloon, a central gondola 36, an arm 32 extending therefrom, a shaft 30 for rotatably connecting the balloon with the top end of the arm 32, and a gas turbine engine 40. The balloon has cables 12b forming a series of squares on the balloon surface in addition to peripheral cables 12a, the gondola 36 is disposed very close to the balloon and has a recessed part to the rear of the gondola top behind a standard horizontal shaft 16 to thereby improve the blanking effect. Such constitution restricts the air flow between the balloon and the gondola 36, this reduces the drag caused on the balloon surface while the lift increases with an increase in the balloon rotation speed, thus improving the flight characteristics. COPYRIGHT: (C)1994,JPO | ||||||
| 302 | Refuge gondola from ultra-high building | JP23857591 | 1991-06-14 | JPH0679007A | 1994-03-22 | EMANIERU ROORAN; KOYANAGI SHIGETAKA |
| PURPOSE:To enable the soft landing of a refuge gondola falling from a rooftop through the air by utilizing a parachute at the time of the occurence of disasters such as a fire in an ultra-high building. CONSTITUTION:A gondola 1 carrying refugees is formed and a support 13 having seats 7 and grasping members is provided in the gondola 1 and a door 4 is attached to one side surface of the gondola and one ends of support frames 15 supporting capsule A storing a parachute are fixed to a plurality of the side surfaces of the gondola 1 by rivets and the other ends thereof are fixed by rivets through the fixing jigs 17 fixed to the lower part of the capsule and an expandable cushion part 14 is provided to the bottom surface part of the gondola. | ||||||
| 303 | Flying vehicle | JP41856790 | 1990-12-28 | JPH04230493A | 1992-08-19 | SUKAI HARUO |
| PURPOSE: To attain stable flight by preventing an envelope from deformation. CONSTITUTION: A flying vehicle flies floating in the air by filling an envelope 10 with gas. A plurality of reinforcing materials 70 are arranged along a direction as the first direction, for instance, longitudinal direction in the periphery of the envelope 10. A plurality of reinforcing materials 71 are arranged along a direction as the second direction, for instance, longitudinal direction. The reinforcing material is wrapped with a coating protective material 80 as shown in drawings 3, 4 preferably in a tape shape. COPYRIGHT: (C)1992,JPO&Japio | ||||||
| 304 | Flying vehicle | JP41856090 | 1990-12-28 | JPH04230490A | 1992-08-19 | SUKAI HARUO |
| PURPOSE: To ensure stable flight while hanging a gondola. CONSTITUTION: In the case of a flying vehicle which has an envelope 10 and a gondola 13 suspended to this envelope 10 to fly in floatation by filling the envelope 10 with gas, hanging members 300 arranged around the envelope 10 are provided between the gondola 13 and the envelope 10 to suspend the gondola 13 relating to the envelope 10 by using these hanging members 300. COPYRIGHT: (C)1992,JPO&Japio | ||||||
| 305 | JPH0163000U - | JP13183988 | 1988-10-11 | JPH0163000U | 1989-04-21 | |
| 306 | Airship with blade area variable propeller, ship weight thereof is slightly larger than buoyancy by buoyancy body | JP16228880 | 1980-11-17 | JPS5787794A | 1982-06-01 | NIIHARA TOSHIHIRO |
| 307 | Airship with propeller, weight of body thereof is slightly larger than buoyancy of buoyancy body | JP14459680 | 1980-10-14 | JPS5770798A | 1982-05-01 | NIIHARA TOSHIHIRO |
| 308 | Aircraft with floating gas balloon | JP11856480 | 1980-08-29 | JPS5744598A | 1982-03-13 | FUREDERITSUKU FUAAGUSON |
| 309 | JPS5623836B2 - | JP8605471 | 1971-10-28 | JPS5623836B2 | 1981-06-02 | |
| 310 | Compound aircraft | JP6510979 | 1979-05-28 | JPS54157999A | 1979-12-13 | CRIMMINS ARTHUR G JR |
| 311 | JPS4862197A - | JP8605471 | 1971-10-28 | JPS4862197A | 1973-08-30 | |
| 312 | 一种快速拆解的飞艇吊舱 | PCT/CN2020/087064 | 2020-04-26 | WO2021169022A1 | 2021-09-02 | 杨思强 |
一种快速拆解的飞艇吊舱，快速拆解的飞艇吊舱包括吊舱本体（1）、气囊（2）和方向舵（3），气囊（2）安装在吊舱本体（1）上方为飞艇提供升力，方向舵（3）安装在吊舱本体（1）两侧为飞艇提供动力和转向力，其中，气囊（2）与吊舱本体（1）之间通过连接组件可拆卸连接，方向舵（3）包括一端与吊舱本体（1）可拆卸连接的连接杆（31），以及与连接杆（31）的另一端可拆卸连接的动力组件（32）。 |
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| 313 | 浮空器 | PCT/CN2015/086764 | 2015-08-12 | WO2016065973A1 | 2016-05-06 | 刘若鹏; 栾琳; 何为 |
一种浮空器（100），包括：多个囊体（10），为母线为弧形的轴对称体，该囊体（10）为浮力囊体；与该多个囊体（10）相对应的多个拉网结构（12），每个拉网结构（12）从对应囊体（10）的顶端向下延伸；及桁架结构（14），连接于该拉网结构（12）的远离该囊体（10）的一端，该桁架结构（14）包括：水平桁架部（140），每个囊体（10）对应的拉网结构（12）均连接于该水平桁架部（140），且该多个囊体（10）对应的拉网结构（12）连接于该水平桁架部（140）的位置以该桁架结构（14）的平行于竖直方向的中心轴等角度分布；及连接于该水平桁架部的下方吊舱固定部（142），该吊舱固定部（142）用于收容或固定吊舱，该吊舱固定部（142）连接于该水平桁架部（140）的中心区域。该浮空器结构简单，制作成本低，整体结构结实稳固。 |
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| 314 | CARGO AIRSHIP | PCT/US2014063675 | 2014-11-03 | WO2015108607A3 | 2015-11-26 | GOELET JOHN; KAPITAN LOGINN; HOCHSTETLER RON |
| A cargo airship (10) is disclosed. The cargo airship may include a hull (12) configured to contain a gas and at least one propulsion assembly (16) coupled to the airship and including a propulsion device. The cargo airship may further include a payload bay (64) comprising an external cargo area (66) located outside of the hull. The cargo airship may also include a cargo handling system including at least one hoisting mechanism (82) configured to lift cargo into the external cargo area while the airship is hovering. | ||||||
| 315 | LUFTFAHRZEUG UMFASSEND EIN AEROSTATENSYSTEM MIT EINER STEUEREINHEIT UND EINER ANTRIEBSEINHEIT SOWIE EINER FUNKTIONSEINHEIT | PCT/EP2014/057866 | 2014-04-17 | WO2014173797A1 | 2014-10-30 | VON GABLENZ, Carl-Heinrich; VON GABLENZ, Alexander; GLASS, Steffen |
Die Erfindung betrifft ein Luftfahrzeug L umfassend ein Aerostatensystem (100), wobei das Aerostatensystem (100) mindestens einen mit einem Traggas befüllbaren Aerostaten (101), insbesondere mindestens einen Ballon aufweist. Das Luftfahrzeug L ist gekennzeichneten durch eine mit dem Aerostaten (101) indirekt in Verbindung stehende Steuereinheit (250) und eine Antriebseinheit (200; 200-1), wobei die Steuereinheit (250) und die Antriebseinheit (200; 200-1) entweder • als eine bifunktionale in einer Kompakteinheit angeordnete Steuer- und Antriebseinheit (200; 250) oder • als monofunktionale in einer Dualeinheit angeordnete Steuer- und Antriebseinheit (200-1, 250) oder • als Kombination aus einer bifunktionalen Kompakteinheit (200; 250) und einer monofunktionalen Dualeinheit (200-1) ausgebildet sind, wobei der Steuereinheit (250) mindestens ein Sitz (200B) für mindestens eine Person (P1) zugeordnet ist, wobei die jeweilige Steuer- und Antriebseinheit (200; 250; 200-1) das Manövrieren des Luftfahrzeuges L zwischen verschiedenen Orten SO, EO, LO ermöglicht. |
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| 316 | NEW KIND OF AIRSHIPS OF THE FUTURE | PCT/AT2012000075 | 2012-03-22 | WO2012135876A3 | 2013-03-28 | KITA FIROOZ |
| An airship with a wide and flat, aircraft-like, not cigar-like, form, comprising a centrally arranged long fuselage and two wings, arranged on both sides of said fuselage, wherein a number of chambers or gas tanks that are delimited or separated from one another are provided, at least one, preferably more than one, in each of the two wings, and at least one means of propulsion, preferably a propeller, is provided in the front region and a means of propulsion is provided in the rear region of the airship, specifically on the upper side of the airship, wherein apertures or clearances, into or through which the means of propulsion can be pivoted or swung are formed in the airship or in the wings of the airship. | ||||||
| 317 | AERIAL TRANSPORTER | PCT/EP2006011702 | 2006-12-06 | WO2007065649A3 | 2007-09-27 | ZULKOWSKI ROLF; HENK JUERGEN; VON GABLENZ CARL; VON KESSEL CHRISTOPH |
| The invention relates to an aerial transporter comprising rigid cell structures which are covered with light materials as a skin, composed of modules. The inventive aerial transporter represents some type of airship without a tail unit as well as an approximate balloon construction encompassing a rigid structure and an independent drive unit. Said aerial transporter can transport loads in the range of about 20 t and more over short to medium distances using lighter-than-air technology while meeting air traffic regulations. Furthermore, the disclosed aerial transporter can be used as an air crane in the tied state. | ||||||
| 318 | LIGHTER-THAN-AIR FLYING CRAFT AND METHOD FOR COUNTERBALANCING THE FLYING CRAFT AND FOR SETTING DOWN A LOAD FASTENED TO THE SAME | PCT/EP2000/004709 | 2000-05-24 | WO00073141A2 | 2000-12-07 | |
| The invention relates to a lighter-than-air flying craft comprising a multitude of ballast tanks (122, 123) and a load hoisting device (125) which can be lowered and which is provided for setting a load (L) fastened in a loading bay (102) on the ground. The inventive craft also comprises a stabilizer (150) and rudder assemblies connected to the craft. A steering system (120) with steering axes (X, Y, Z) is provided for steering the flying craft (100), whereby the flying craft (100) can be positioned in every axis (X, Y, Z) by a rudder deflection ( delta R) of the rudder assembly effected by the steering system (120). Damping elements (10) are also provided in the flying craft (100) in order to reduce arising vibrations to a level that is adequate for conducting a safe flying operation. The flying craft is characterized in that the rudder deflection ( delta R) can be modulated with a control pulse ( DELTA delta R) which comprises an additional rudder deflection with a dampening effect, and in that the load hoisting device (125) is configured such that it can be displaced along a longitudinal direction and/or a transversal direction of the loading bay (102) so that a load (L) can be set down from the air at a precise set-down point. The invention also relates to a method for counterbalancing the position of the lighter-than-air flying craft when setting down a load and additionally relates to a method for setting a load fastened to the lighter-than-air flying craft down on the ground. | ||||||
| 319 | AIRSHIP FOR THE TRANSPORT OF GOODS AND PASSENGERS | PCT/EP9301369 | 1993-06-01 | WO9324364A3 | 1994-02-03 | GELHARD EGON |
| An airship for the transport of goods and passengers has a lattice body made of nodes (12) and circular and longitudinal beams (13, 15) stuck in or on receptions of the nodes, as well as tensioning ropes (14) which brace the circular and longitudinal beams in or on the receptions, are held on the nodes and form with the lattice body a three-dimensional framework. The lattice body consists of circular and longitudinal beams precisely cut to length with small tolerance and the nodes are braced by tensioning ropes provided with hooks (30) and cut with tight tolerance to the length needed to achieve the required pretensioning, so that a structure made of uniform components suitable for lattice bodies of various sizes is obtained. The lattice body can have a cargo bay (7) in its lower area, buoyant gas cells suspended on rings within the lattice body, a rope bracing of the gas cell enveloppe that substantially extends in the radial and axial directions in at least one gas cell and a winch drive that engages the rope bracing in order to adjust the gas cell volume. At least one inherently stiff, movable and lowerable cargo pallet secured to the lattice body which closes the cargo bay and forms its bottom, can be arranged in the lower area of the lattice body and allows the airship to be quickly loaded and unloaded, in particular with containers. | ||||||
| 320 | 一种监测用系留飞艇 | CN202420924127.1 | 2024-04-30 | CN222591781U | 2025-03-11 | 梅方颖 |
| 本实用新型提供一种监测用系留飞艇，包括锚泊车，锚泊车设置在地面上并装载有安装有系留单元的系留结构；飞艇设置在锚泊车的上方，飞艇上还集成安装有设备搭载单元；锚泊车和飞艇之间通过系留缆绳单元连接。本实用新型利用在锚泊车和飞艇之间通过系留缆绳单元连接，达到了稳定飞艇的效果，此外，在飞艇的底部安装有气阀和安全阀，为飞艇提供稳定的浮力，保障安全的同时又能提供稳定的支撑性，为设备搭载单元提供的保障，同时又能提高了系留飞艇对环境的适应力，广泛运用于应急事件中。 | ||||||
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