| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 141 | VORRICHTUNG UND VERFAHREN ZUR WIEDERGABE VON LICHTSTRAHLUNG AN EINEM LUFTFAHRZEUG | EP03702420.5 | 2003-01-10 | EP1472667A1 | 2004-11-03 | Lick, Jürgen; Schedlbauer, Veronika |
| The invention relates to a device and method for displaying luminous radiation on a shell of an aircraft, comprising at least one light source for producing luminous radiation, and at least one projection device for converting the luminous radiation into projectable luminous radiation. The at least one projection device is mounted inside the shell in order to project the luminous radiation through the interior (15) and onto the shell (60). Said shell is translucent at least in portions thereof whereby making the projected luminous radiation visible from the outside. The invention also relates to a method for displaying luminous radiation on a shell of an aircraft. | ||||||
| 142 | DIRIGIBLE AIRSHIP | EP92918827.4 | 1992-09-09 | EP0603238B1 | 1996-08-14 | FERGUSON, Frederick D., 160 George Street |
| An airship in the form of a self-powered, elongated dirigible which comprises at least three sections connected together by joints. The sections including a front section (10) with propulsion devices (22) and control surfaces (23), at least one intermediate section (12a, 12b, 12c) designed to carry a payload and a rear section (14) with control surfaces. The joints allow limited articulation between sections under gust conditions and tend to return the sections to aligned condition in calm air. A cover may provide a streamline exterior shape for the airship; alternatively the sections may have rims which mate together when there is no articulation to provide a smooth exterior shape. | ||||||
| 143 | Omnidirectional propelling type airship | EP93112188.3 | 1993-07-29 | EP0583666A1 | 1994-02-23 | Bundo, Mutsuro |
An omnidirectional propelling type airship which can be propelled in any desired direction in the three-dimensional space including front-rear, upper-lower and left-right directions, is disclosed. The airship comprises a gas chamber (1, 2) capable of tightly sealing gas, gas having a specific gravity smaller than air and filled in the gas chamber, a section (14) capable of being loaded with men, cargoes and the like, and propelling means (6) supported in a gimbal fashion and capable of propelling in any arbitrary spacial direction. |
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| 144 | DIRIGEABLE HYDRIDE A ENVELOPPE EXTERIEURE SOUPLE ET COMPARTIMENTEE | EP16206518.9 | 2016-12-22 | EP3187410B1 | 2018-09-26 | SIMONIS, Alexandre; GONZE, Yann; BARGETON, Etienne |
| 145 | CONTINUOUS FIBER REINFORCEMENT FOR AIRSHIP CONSTRUCTION | EP17199570.7 | 2017-11-01 | EP3318480A1 | 2018-05-09 | MOREHEAD, John P. |
An airship hull (105) is disclosed. The airship hull (105) comprises a gas-tight shape fabricated from a membrane (110). The airship hull (105) comprises one or more fibers (205) 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 (205) wraps around a circumference of the gas-tight shape multiple times, wherein the applied one or more fibers (205) are affixed to the outer surface of the gas-tight shape.
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| 146 | AIRSHIP LAUNCH FROM A CARGO AIRSHIP | EP13745206.6 | 2013-01-10 | EP2802511B1 | 2018-05-02 | HEPPE, Stephen |
| A method for launch of an airship includes connecting a cargo airship to a deflated second airship, launching the cargo airship, inflating the second airship with lifting gas carried by the cargo airship while aloft; and releasing the second airship from the cargo airship. A high-altitude airship launch system is also provided. | ||||||
| 147 | METHOD FOR CONTROLLING LAND SURFACE TEMPERATURE USING STRATOSPHERIC AIRSHIPS AND REFLECTOR | EP12851053.4 | 2012-10-22 | EP2784560B1 | 2017-04-05 | CHOI, Joon-Min |
| The present invention relates to a method for controlling land surface temperature using stratospheric airships and a reflector. In the method for controlling land surface temperature using stratospheric airships and a reflector, four corners are connected to a lower end of support lines coupled to be disposed vertically downward from a plurality of airships, and sunlight is reflected by a reflector unfolded into a tetragonal shape in the air, wherein the reflecting surface of the reflector plate is maintained at an angle to remain perpendicular to an incident angle of sunlight to shield the land surface from incident sunlight. | ||||||
| 148 | "MOMOHELI II" LIFTING MODULE AND VEHICLES | EP10765983.1 | 2010-09-23 | EP2619083B1 | 2016-04-27 | Monsch, Daniel; Monsch, Hans |
| 149 | BALLON DIRIGEABLE | EP13727276.1 | 2013-05-13 | EP2855260A1 | 2015-04-08 | REGAS, Baptiste; REGAS, Adrien; JOZAN, Olivier |
| An airship (1) comprising a flexible envelope (2), a wall (3) located inside the envelope, and a pumping means. The wall (3) extends longitudinally between the nose and the tail, separating the space inside the envelope into a first space (E1) and a second space (E2), said second space being located at the periphery of the envelope between a first point (P1) and a second point (P2). The pumping means is capable of inflating the second space in order for the envelope to assume a second shape, and of deflating the second space in order for the envelope to assume a first shape different from the second shape. | ||||||
| 150 | AIRSHIP LAUNCH FROM A CARGO AIRSHIP | EP13745206.6 | 2013-01-10 | EP2802511A2 | 2014-11-19 | HEPPE, Stephen |
| A method for launch of an airship includes connecting a cargo airship to a deflated second airship, launching the cargo airship, inflating the second airship with lifting gas carried by the cargo airship while aloft; and releasing the second airship from the cargo airship. A high-altitude airship launch system is also provided. | ||||||
| 151 | METHOD FOR CONTROLLING LAND SURFACE TEMPERATURE USING STRATOSPHERIC AIRSHIPS AND REFLECTOR | EP12851053.4 | 2012-10-22 | EP2784560A1 | 2014-10-01 | CHOI, Joon-Min |
The present invention relates to a method for controlling land surface temperature using stratospheric airships and a reflector. In the method for controlling land surface temperature using stratospheric airships and a reflector, four corners are connected to a lower end of support lines coupled to be disposed vertically downward from a plurality of airships, and sunlight is reflected by a reflector unfolded into a tetragonal shape in the air, wherein the reflecting surface of the reflector plate is maintained at an angle to remain perpendicular to an incident angle of sunlight to shield the land surface from incident sunlight. |
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| 152 | AIRSHIP | EP02705145.7 | 2002-03-13 | EP1394038B1 | 2010-08-04 | OGAWA, Daihachi; OGAKI, Masanobu; SASAKI, Yoshitaka; SUGAWARA, Masahiko; MAEHATA, Takayoshi; FUKUMOTO, Katsuji |
| 153 | SYSTEM AND APPARATUS FOR PROPELING AND CARRYING A USER WITHIN A CONFINED INTERIOR | EP06800345 | 2006-07-26 | EP1919587A4 | 2010-01-20 | MEADOWS J STEPHEN |
| 154 | HIGH-SECURITY AIRCRAFT | EP05769453.1 | 2005-07-07 | EP1899220A1 | 2008-03-19 | CAPUANI, Alfredo |
| The aircraft (10) comprises an elongated framework (26) provided with propelling means and direction-control planes. The framework is coupled to a pneumatic chamber (16) suited to be filled with lighter-than-air gas and comprising two tubular branches (12, 14) joined to form a V-shaped profile, with an aerodinamic-lift surface (22, 24) extending therebetween. | ||||||
| 155 | Direct mounted propulsion for non-rigid airship | EP06255086.8 | 2006-09-30 | EP1772374A3 | 2008-02-20 | Marimon, Thomas L.; Peritt, Jonathan; Houmard, James E. |
A propulsion assembly (20) for attachment to the enclosing material (14) of an airship (10) includes a base (21) which is positioned proximate to the enclosing material. An extension member (40) having opposed ends projects away from the base (21) and includes opposed ends. A motor assembly (50) is attached to the end of the extension member (40) opposed to the base (21). A mounting assembly (70) is attached to the enclosing material and a plurality of pre-tensioned guy cables (60) connect the mounting assembly (70) to the extension member (40).
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| 156 | LIGHTER-THAN-AIR AIRCRAFT WITH AIR CUSHION LANDING GEAR MEANS | EP02781437.5 | 2002-12-05 | EP1451063B1 | 2005-11-09 | MUNK, Jeffrey Roger |
| A lighter-than-air aircraft (1) having a gas-filled hull (2) and a pair of spaced apart landing gear units (11, 12) on the underside of the hull arranged on opposite sides of a longitudinally extending central vertical plane of the hull. Each landing gear unit (11, 12) comprises bag skirt means (5-7, 5'-7'), means for supplying air to and removing air from the bag skirt means and actuating means operable to move the bag skirt means between an operative configuration for containing one or more air cushions and an inoperative configuration. | ||||||
| 157 | Vorrichtung und Verfahren zur Wiedergabe von Lichtstrahlung an einem Luftfahrzeug | EP05102804.1 | 2003-01-10 | EP1569192A1 | 2005-08-31 | Lick, Jürgen; Schedlbauer, Veronika |
Erfindungsgemäß vorgeschlagen wird eine Vorrichtung zur Wiedergabe von Lichtstrahlung an einer Hülle eines Luftfahrzeuges, mit mindestens einer Lichtquelle zur Erzeugung von Lichtstrahlung; mindestens einer Projektionseinrichtung zur Wandlung der Lichtstrahlung in projektionsfähige Lichtstrahlung; wobei die mindestens eine Projektionseinrichtung im Innenraum der Hülle zur Projektion der Lichtstrahlung durch den Innenraum (15) an die Hülle (60) angeordnet ist; und die Hülle zumindest in Teilen lichtdurchlässig ausgestaltet ist zum Sichtbarmachen der projizierten Lichtstrahlung nach außen. Die Erfindung betrifft ebenfalls ein Verfahren zur Wiedergabe von Lichtstrahlung an einer Hülle eines Luftfahrzeugs. |
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| 158 | LIGHTER-THAN-AIR AIRCRAFT WITH AIR CUSHION LANDING GEAR MEANS | EP02781437.5 | 2002-12-05 | EP1451063A1 | 2004-09-01 | MUNK, Jeffrey Roger |
| A lighter-than-air aircraft (1) having a gas-filled hull (2) and a pair of spaced apart landing gear units (11, 12) on the underside of the hull arranged on opposite sides of a longitudinally extending central vertical plane of the hull. Each landing gear unit (11, 12) comprises bag skirt means (5-7, 5'-7'), means for supplying air to and removing air from the bag skirt means and actuating means operable to move the bag skirt means between an operative configuration for containing one or more air cushions and an inoperative configuration. | ||||||
| 159 | DIRIGIBLE AIRSHIP | EP92918827.0 | 1992-09-09 | EP0603238A1 | 1994-06-29 | FERGUSON, Frederick D., 160 George Street |
| Un ballon prend la forme d'un dirigeable allongé auto-propulsé, doté d'au moins trois sections reliées par des articulations. On trouve une section frontale (10) dotée de dispositifs propulseurs (22) et d'empennages (27), au moins une section intermédiaire (12a, 12b, 12c) conçue pour transporter une charge utile et une section arrière (14) dotée d'empennages. Les articulations confèrent aux sections un jeu limité, quand sévissent des tempêtes, et tendent à les réaligner par situation calme. Un cache peut donner au dirigeable une forme aérodynamique; en l'absence d'articulation, les sections peuvent aussi comporter des rebords à encastrement et présenter ainsi une surface externe lisse. | ||||||
| 160 | 비행체를 위한 부양 구조 | KR1020160102662 | 2016-08-12 | KR1020180017964A | 2018-02-21 | 이상근; 이채은; 이지아 |
| 본발명에따른부양구조체는, 플렉서블한가스주머니(10); 상기가스주머니(10) 감싸는형태로권취되는스트링(20); 상기결속된가스주머니(10)와스트링(20) 상에분사방식으로공급되는약제(30); 및상기스트링(20)이감겨진가스주머니(10)를전체적으로감싸는구조의외부케이스(40);를포함한다. | ||||||
