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1. 发明授权

EP3966106B1 AIRCRAFT AND SYSTEMS THEREFOR 有权
公开(公告)号：EP3966106B1
公开(公告)日：2024-06-19
申请号：EP20739431.3
申请日：2020-05-07
IPC分类号： B64B1/62 , G01F17/00
CPC分类号： B64B1/62 , G01F17/00

2. 发明公开

EP4105127A1 AUTOMATIC READINESS INDICATION FOR AIRCRAFT EMERGENCY EVACUATION 审中-实审
公开(公告)号：EP4105127A1
公开(公告)日：2022-12-21
申请号：EP22177660.2
申请日：2022-06-07
申请人： Goodrich Corporation
发明人： PALANIAPPAN, Elangovan , JOHN, Poly , SALDANHA, Nikhil Anthony , SUBRAMANIAN, Petchi
IPC分类号： B64D25/14 , B63C9/04 , B64B1/62
摘要： An inflation system for an inflatable includes a readiness indicator module (270); a stretch sensor (220) configured for mounting to the inflatable and to provide a real-time stretch data of an elastic deformation of the inflatable; and a controller (258) configured to receive the real-time stretch data and to transmit a control signal to the readiness indicator module (270) to indicate a deployed status of the inflatable.

3. 发明授权

EP2885204B1 BALLOON POWER SOURCES WITH A BUOYANCY TRADE-OFF 有权转让
公开(公告)号：EP2885204B1
公开(公告)日：2018-07-04
申请号：EP13830352.4
申请日：2013-08-12
申请人： X Development LLC
发明人： DEVAUL, Richard, Wayne , TELLER, Eric , BIFFLE, Clifford, L. , WEAVER, Joshua
IPC分类号： B64B1/44 , H04W16/18 , B64B1/40 , B64B1/62
CPC分类号： G05D1/042 , B64B1/40 , B64B1/62 , C25B1/04 , H02S20/30 , Y02E60/366 , Y02E70/10 , Y02P20/134
摘要： Example embodiments may facilitate altitude control by a balloon in a balloon network. An example method involves: (a) causing a balloon to operate in a first mode, wherein the balloon comprises an envelope, a high-pressure storage chamber, and a solar power system, (b) while the balloon is operating in the first mode: (i) operating the solar power system to generate power for the balloon and (ii) using at least some of the power generated by the solar power system to move gas from the envelope to the high-pressure storage chamber such that the buoyancy of the balloon decreases; (c) causing the balloon to operate in a second mode; and while the balloon is operating in the second mode, moving gas from the high-pressure storage chamber to the envelope such that the buoyancy of the balloon increases.

4. 发明授权

EP2514666B1 Vehicle comprising heavier than air internal ballast 有权
标题翻译：车辆用内部压载，这是比空气重
公开(公告)号：EP2514666B1
公开(公告)日：2016-10-19
申请号：EP12000891.7
申请日：2012-02-10
申请人： Lockheed Martin Corporation
发明人： Piini, Nicholas , Siler, Alex , Kinkopf, Joseph , Fahey, Caitlyn
IPC分类号： B64B1/60 , B64B1/62
CPC分类号： B64B1/60 , B64B1/62

5. 发明公开

EP2872394A1 BALLOON ALTITUDE CONTROL USING DENSITY ADJUSTMENT AND/OR VOLUME ADJUSTMENT 有权转让
标题翻译：其密度和/或体积调整气球高度控制
公开(公告)号：EP2872394A1
公开(公告)日：2015-05-20
申请号：EP13816199.7
申请日：2013-06-24
申请人： Google Inc.
发明人： TELLER, Eric , DEVAUL, Richard, Wayne , WEAVER, Joshua , BIFFLE, Clifford
IPC分类号： B64B1/44 , B64B1/62 , H01L31/042
CPC分类号： B64B1/62 , B64B1/40 , B64B1/56
摘要： A balloon having an envelope and a payload positioned beneath the envelope. The envelope comprises a first portion and a second portion, wherein the first portion allows more solar energy to be transferred to gas within the envelope than the second portion. The balloon may operate in a first mode in which altitudinal movement of the balloon is caused, at least in part, by rotating the envelope to change an amount of the first portion that faces the sun and an amount of the second portion that faces the sun, and wherein the control system is further configured to cause the balloon to operate in a second mode in which altitudinal movement of the balloon is caused, at least in part, by moving a lifting gas or air into or out of the envelope.

6. 发明授权

EP1394038B1 AIRSHIP 有权
标题翻译：飞艇
公开(公告)号：EP1394038B1
公开(公告)日：2010-08-04
申请号：EP02705145.7
申请日：2002-03-13
申请人： KAWASAKI JUKOGYO KABUSHIKI KAISHA
发明人： OGAWA, Daihachi , OGAKI, Masanobu , SASAKI, Yoshitaka , SUGAWARA, Masahiko , MAEHATA, Takayoshi , FUKUMOTO, Katsuji
IPC分类号： B64B1/02 , B64B1/60 , B64B1/62
CPC分类号： B64B1/62 , B64B1/02 , B64B1/60

7. 发明公开

EP2132087A1 AIRCRAFT CONFIGURED FOR VERTICALLY ASCENDING AND LANDING 有权
标题翻译： FOR垂直上升和-LANDUNG配置飞机
公开(公告)号：EP2132087A1
公开(公告)日：2009-12-16
申请号：EP08723889.5
申请日：2008-03-10
申请人： Sst Condor Holding B.v. I.o.
发明人： VAN HELDEN, Aalbert Adrianus
IPC分类号： B64B1/60 , B64B1/62
CPC分类号： B64B1/60 , B64B1/62 , B64B2201/00
摘要： An aircraft which is configured for vertically ascending and landing, comprises at least two wings (2a, 2b, 4a, 51, 4b, 52), a space (2c, 4c) for the generating during operation of climbing power, and an intermediate portion (3), the intermediate portion (3) being provided with thrust motors (6), and the space (2c, 4c) for the generating during operation of climbing power being provided with a quantity of lifting power units (HV). Each lifting power unit comprises a first variable volume (Vl) for the storage of an amount of relatively light gas which is lighter than atmospheric air, and is configured for the controllable adjustment of an upward force or lifting power by means of the variable volume taken up by the amount of relatively light gas.

8. 发明授权

EP1280698B1 BALLON DIRIGEABLE RIGIDIFIE PAR LES RESERVOIRS D'HELIUM 有权
标题翻译： BY氦气罐僵硬飞艇
公开(公告)号：EP1280698B1
公开(公告)日：2005-03-30
申请号：EP01934085.0
申请日：2001-05-11
申请人： Aerospace Adour Technology , Senepart, Marc
发明人： SENEPART, Marc
IPC分类号： B64B1/08 , B64B1/62
CPC分类号： B64B1/08 , B64B1/62
摘要： The invention concerns a variable portability flying device powered by helium. Said device comprises a balloon (1) consisting of an outer flexible shroud (3) supported by a rigid structure. The rigid structure comprises several hollow toroids (4) having an internal volume serving as tank for storing pressurised helium.

9. 发明授权

EP0729423B1 A BALLONET SYSTEM FOR A LIGHTER-THAN-AIR VEHICLE 失效
标题翻译： Ballonett SYSTEM FOR比空气轻的车辆
公开(公告)号：EP0729423B1
公开(公告)日：2000-03-29
申请号：EP94927391.6
申请日：1994-09-12
申请人： Lockheed Martin Corporation
发明人： KALISZ, John, B. , WEXLER, Mark, H.
IPC分类号： B64B1/62
CPC分类号： B64B1/60
摘要： The invention is a ballonet system for a lighter-than-air-vehicle, the vehicle having a lift producing gasbag and a longitudinal, vertical and lateral axis. In detail, the ballonet system includes a plurality of ballonets (34A) located within the gasbag (12) positioned along the longitudinal axis (18) and on each side of the vertical axis (19) of the vehicle (10). Each of the ballonets (34A) include a flexible sheet (40) joined at its periphery (43) thereof to a portion of the wall (44) of the gasbag. A ballonet pressurization system (45) is coupled ot each ballonet (34A) for pressurizing them with air that includes the portion of the wall (44) of the gasbag (12) forming the ballonet having a plurality of holes (54) therethrough. A manifold (60) having an inlet port (64) is joined to the wall covering the holes (54) therein and is adapted to diffuse the pressurized air entering therein. Also included is at least one fan (46) having an inlet port (50) coupled to ambient atmosphere and an outlet port (51) coupled to the inlet port (64) of the manifold (60) for providing pressurized air to the interior thereof. A check valve (52) located in the outlet port (51) of the fan (46) is provided for preventing air from flowing from the interior of the manifold out the inlet port of the fan. A ballonet venting system (70) is included for venting the interior of the ballonet to ambient atmosphere.

10. 发明授权

EP3696080B1 TETHERED HELIUM KITE GAS REPLENISHMENT DEVICE AND GAS REPLENISHMENT METHOD 有权转让
公开(公告)号：EP3696080B1
公开(公告)日：2022-02-23
申请号：EP20156826.8
申请日：2020-02-12
发明人： Knap, Lech , Wolejsza, Zbigniew , Graczykowski, Cezary , Faraj, Rami , Holnicki-Szulc, Jan
IPC分类号： B64B1/64 , F16L37/32 , B64B1/52 , B64B1/62 , F16L37/096 , F16L37/62

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