| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 21 | JPH07500785A - | JP50478493 | 1992-09-09 | JPH07500785A | 1995-01-26 | FERGUSON FREDERICK D |
| 22 | Airship | JP3438692 | 1992-01-24 | JPH05201390A | 1993-08-10 | TAKEUCHI MASAAKI |
| PURPOSE: To provide an airship which improves sharply work efficiency by a method wherein even when an airship is large, it is easily contained in a building and further, when it is anchored at a field, no space is needed, and the influence of wind is minimized. CONSTITUTION: The body of an airship is dividable into compartments of a head part A, an intermediate part B, and a tail part C. The connection part of each compartment is provided with a circular frame F, and a removable flexible joint J is mounted on the opposite surfaces, making a pair, of the circular frames F. The flexible joint J regulates the connection length of a shaft and has adjustability with which the direction of a shaft itself is changed in a 360° arc. COPYRIGHT: (C)1993,JPO&Japio | ||||||
| 23 | JPH05280B2 - | JP22887589 | 1989-09-04 | JPH05280B2 | 1993-01-05 | TAKAHASHI MASAKATSU; TAKAHASHI RYUTARO; TAKAHASHI KENTARO |
| 24 | 成層圏飛行船と反射板を用いた地表面の温度調節方法 | JP2014512776 | 2012-10-22 | JP5792896B2 | 2015-10-14 | チェ、ジュンミン |
| 25 | airship | JP2012533677 | 2010-10-12 | JP2013507293A | 2013-03-04 | レガス，バプティステ; ジョザン，オリビエ |
| 本発明は、剛性の内部構造を有さず、空気よりも軽い気体を格納する外皮（２）と、ゴンドラ（３）と、を備えた飛行船（１）に関するものである。 飛行船は、また、表面に到着できるようにするための３つの足と着陸構造体（５）とを備える。 着陸構造体（５）は、外皮の外側に位置し、足（６ａ，６ｂ，６ｃ）、ゴンドラ（３）、および外皮（２）の間に接続し、外皮（２）を取り囲む。 | ||||||
| 26 | Multipurpose airship | JP2004180560 | 2004-06-18 | JP2006001435A | 2006-01-05 | BUNTO MUTSURO |
| PROBLEM TO BE SOLVED: To provide a multipurpose airship which can be multipurposely used and takes an inexpensive administrative and maintenance expense. SOLUTION: A balloon 5 which is made of either material of soft, semi-soft or hard material, in appropriate shape such as sphere or spindle shape, and generates a levitation force by filling a gas lighter than air is detachably mounted to the top, and is equipped with a two steps variable angle rotor 4 capable of adjusting an angle so as to generate both the levitation force and propulsive force, a stabilizing wing 2 where a propulsion unit 3 composed of a propeller or a jet engine is variable from the horizontal to vertical for the propulsive direction and detachably mounted to the end part, and a cabin 1 for a crew. A working apparatus such as a spraying device 10 of agricultural chemical can be mounted to the cabin 1. COPYRIGHT: (C)2006,JPO&NCIPI | ||||||
| 27 | All directions-propelled airship | JP22144692 | 1992-08-20 | JP3468783B2 | 2003-11-17 | 睦郎 豊東 |
| 28 | Airship | JP2001140860 | 2001-05-11 | JP2002331999A | 2002-11-19 | OGAWA DAIHACHI; OGAKI MASANOBU; SASAKI YOSHITAKA; SUGAWARA MASAHIKO; MAEHATA TAKAYOSHI; FUKUMOTO KATSUHARU |
| PROBLEM TO BE SOLVED: To provide an airship capable of improving responsiveness to attitude control and attitude stability. SOLUTION: A plurality of bulkheads 23a-23d are provided to divided a space S of an airframe 21 into a plurality of space portions ΔS1-ΔS5 along an airframe axis 22. The space portions ΔS1-ΔS5 are partitioned into respective upper floating-gas storage regions 25a-25e for storing floating gas and respective lower air storage regions 26a-26e for storing air by respective flexible barriers 24a-24e which cut off the passage of the floating gas and the air. Respective upper regions A1a-A1d of the bulkheads 23a-23d face to the respective floating- gas storage regions 25a-25e above respective connection points 27a-27d of the barriers 24a-24e and are formed with vent holes for permitting the passage of the floating gas. COPYRIGHT: (C)2003,JPO | ||||||
| 29 | Steerable airship | JP50478493 | 1992-09-09 | JP3270895B2 | 2002-04-02 | ファーガソン，フレデリック・ディ |
| 30 | Omnidirectional propulsion type airship | JP22144692 | 1992-08-20 | JPH0664592A | 1994-03-08 | BUNTOU MUTSUROU |
| PURPOSE:To enable propulsion in the desired direction in three-dimensional space in longitudinal, vertical and lateral directions by providing a propulsion means supported in the gimbal state so as to be propulsive toward an optional direction in space. CONSTITUTION:In a propulsion device 6, a propeller 7 and its engine 8 are supported by a gimbal 9 so that the propulsion device 6 can face all directions in space. The propeller 7, the engine 8 for rotatory-driving the propeller 7, and the gimbal 9 are supported in the alternately rotatable state by orthogonal shafts the center of which an inner frame 10 and an outer frame 11 pass. Upon rising to the required altitude, the propellers 7 are turned forward to shift into an ahead flight. In the case of turning to the right, the propeller 7 on the starboard side is set to pitch 0(zero) to eliminate thrust, and the propeller 7 on the port side can be turned to face forward, but turning can be performed further rapidly by turning the starboard propeller 7 to face backward and the port propeller 7 to face forward. In the case of turning to the left, reverse operation is performed. | ||||||
| 31 | Airship | JP29212890 | 1990-10-31 | JPH04169397A | 1992-06-17 | OMIYA SOSUKE |
| PURPOSE: To perform acrobatic flights such as a complete roll and a loop by providing a propelling/attitude control means for propelling and yaw/pitch/roll angle controlling each on both side sections of an airframe with a specific shape, and providing external tails with a specific area. CONSTITUTION: The airframe 1 of a soft airship has a rotary elliptical outer shape, it is nearly symmetrically formed statically and dynamically on the horizontal and vertical planes containing the airframe axis X, and the center of gravity position is preferably set up to 20% of the maximum radius of the airframe downward from the center of buoyancy. The ratio between the whole length and the maximum diameter of the airframe 1 is set to 0.75-3.5 to improve controllability. Reversible propellers 6, 7 are provided via tilt systems 4, 5 respectively at positions within the front 20% of the airframe 1 on the right and left side sections for the propulsion and attitude control of the airframe 1. Horizontal and vertical external tails 10, 11 are provided on the periphery of the rear section of the airframe 1, and the total area A is set to 0.1×Q 2/ 3≤A≤0.5×Q 2/ 3, where Q is the volume of the airframe 1. COPYRIGHT: (C)1992,JPO&Japio | ||||||
| 32 | 비행선을 이용한 풍력발전시스템 | KR1020160056602 | 2016-05-09 | KR1020170126326A | 2017-11-17 | 안광우 |
| 비행선을이용하여제트스트림(jet stream)의강한바람을이용하여풍력발전을하고, 이를레이져로변환하여지상으로송신한후 지상에서이를전기로변환하여전력을생산할수 있도록한 비행선을이용한풍력발전시스템에관한것으로서, 공중부양되어풍력발전을통해전력을생산하고, 생산전력을레이져로송신하는비행선; 및상기비행선로부터송신된레이져를수신하여전기로변환하는지상수신부를포함하여비행선을이용한풍력발전시스템을구현함으로써, 지상에서비행선의전력을회수하는데 효율성과편리함을제공한다. | ||||||
| 33 | 풍선형 공중 로봇 키트 | KR1020120052858 | 2012-05-18 | KR1020130128818A | 2013-11-27 | 김현식 |
| Disclosed is a balloon-type airborne robot kit which can be horizontally and vertically moved by a programmed control board in a state of being airborne using a balloon. The balloon-type airborne kit according to the present invention comprises: the balloon; a main rack coupled to the balloon; a first motor; a mass attaching plate on which the control board and a battery are mounted; a pinion which is driven by the first motor, which is coupled to the main rack, and which moves the mass attaching plate along the main rack; a first control plate which has one end fixed on the main rack, and which is vertically mounted along the longitudinal direction of the main rack; a second control plate which is vertically mounted along the longitudinal direction of the main rack in the opposite side of the first control plate, and which has one end fixed on the main rack; a first frame which is coupled to the first control plate, and on which a second motor is mounted; a second frame which is coupled to the second control plate, and on which a third motor is mounted a first propeller coupled to a rotary shaft of the second motor; and a second propeller coupled to a rotary shaft of the third motor. | ||||||
| 34 | 여객용 비행선 | KR1020110022596 | 2011-03-14 | KR1020110033911A | 2011-04-01 | 김대원 |
| PURPOSE: A passenger airship is provided to achieve high efficiency, profitability, and environmentally-friendly property by employing solar power generation or nano technology as well as a levitation force. CONSTITUTION: A passenger airship, which transports a plurality of people or cargo using a levitation force and an engine, is equipped with a search light to search for objects in the air or on the ground in the night time. A solar panel is attached to the outer shell of the airship to supply electric power to the internal components of the airship. | ||||||
| 35 | Hydrogen ballooning car rope | KR20070081038 | 2007-08-13 | KR20070089666A | 2007-08-31 | KIM GYOUNG GON |
| A cable car with a hydrogen balloon is provided to be installed on a road or on a sea with an unlimited length of a rope to expect an advantage of a light aircraft. A cable car with a hydrogen balloon includes an upper main rope(1), an upper sub rope(2), a lower main rope(3), a lower sub rope(4), a gas balloon, a transporting room, and a propeller. The upper main rope and the upper sub rope are connected to the gas balloon for guiding the cable car. The lower main rope and the lower sub rope are connected to the transporting room to guide the cable car on an intended course. The gas balloon contains hydrogen to lift up the cable car helping the cable car move forward more easily. The transporting room is a space for passengers. The propeller is installed in a rear part of the transporting room to obtain the propulsion for the cable car. | ||||||
| 36 | Continuous Fiber Reinforcement For Airship Construction | US15342821 | 2016-11-03 | US20180118320A1 | 2018-05-03 | John P. Morehead |
| An airship hull is disclosed. The airship hull comprises a gas-tight shape fabricated from a membrane. The airship hull comprises one or more fibers applied to an outer surface of the gas-tight shape in a continuous manner such that a particular one of the one or more fibers wraps around a circumference of the gas-tight shape multiple times, wherein the applied one or more fibers are affixed to the outer surface of the gas-tight shape. | ||||||
| 37 | Near-space operation systems | US14188581 | 2014-02-24 | US09694910B2 | 2017-07-04 | Taber K. MacCallum; Jacob H. Dang; Robert Alan Eustace; John Zaniel Maccagnano; Julian R. Nott; Sebastian A. Padilla; Sreenivasan Shankarnarayan; John Straus; Jared Leidich; Daniel Pieter Jacobus Blignaut |
| A system enabling safe manned and unmanned operations at extremely high altitudes (above 70,000 feet). The system utilizes a balloon launch system and parachute and/or parafoil recovery. | ||||||
| 38 | Aerial vehicle and method of flight | US14324306 | 2014-07-07 | US09694894B2 | 2017-07-04 | Nicholas James Deakin |
| An aerial vehicle comprises an elongate envelope within which are at least one first compartment for holding a lighter than air gas and at least one second compartment for holding atmospheric air and said at least one second compartment having an inlet and an outlet and at least one pair of wings extending laterally from the envelope; said wings being planar units with a leading and trailing edge, the width of the wings from their leading edges to their trailing edges being substantially less than the length of the envelope with airfoil portions fitted between the leading and trailing edges of the wing: the top and bottom of the wings are mirror images of one another; in which forward motion of the vehicle is obtainable without trust through alternate diving and climbing motion. | ||||||
| 39 | HYBRID AIRSHIP WITH A FLEXIBLE COMPARTMENTED EXTERIOR ENVELOPE | US15391126 | 2016-12-27 | US20170183073A1 | 2017-06-29 | Alexandre Simonis; Yann Gonze; Etienne Bargeton |
| A hybrid airship has both aerostatic and aerodynamic lift comprising: an engine, a flexible external envelope (2) and at least one primary enclosure Ep filled with lifting gas (G). The primary enclosure Ep having an elastic wall P1 separating this enclosure from compartment C1, the latter having an elastic wall P1 separating compartment C1 from compartment Ci, the latter having an elastic wall Pi+1 separating the compartment Ci from compartment Ci+1, and so on up until elastic wall PJ+1 separating compartment CJ from compartment CJ+1 where J corresponds to a whole number greater than or equal to 1, each compartment Ci being equally delimited by the flexible exterior envelope. The hybrid airship includes a) a valve Vi between each compartment Ci and its adjacent compartment Ci+1, and b) a controller (22) for the valve Vi. | ||||||
| 40 | Gas barrier material with atomic sheet | US14045368 | 2013-10-03 | US09598165B2 | 2017-03-21 | Steven Edward Bullock; Jaime Ballester |
| A gas barrier material includes an atomic sheet, such as graphene and/or an analog of graphene. The gas barrier material can be arranged as part of a component, such as a container or other vessel, to limit the flow or permeation of gas through the component. Where the component is a container or part of a container, the gas barrier material may be formulated and arranged to limit or prevent gas ingress or egress with respect to the internal volume of the container. The atomic sheet offers improved gas barrier properties compared to traditional polymeric barrier materials and is particularly useful in applications where it is desired to limit permeation of small gas molecules such as helium, such as airships or other lighter than air vehicles. | ||||||
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