公开(公告)号：EP2527251A3

公开(公告)日：2018-01-10

申请号：EP12160224.7

申请日：2012-03-19

申请人： The Boeing Company

发明人： Bernhardt, Roger D

IPC分类号： B64D1/08 ,  B64D17/02 ,  G06F1/16 ,  H04W88/00

CPC分类号： B64D1/08 ,  B64D17/025 ,  G01C21/00

摘要： A method and apparatus comprising a housing, a processor unit, a display, a navigation module, and a number of modules. The navigation module is configured to guide an airdrop system to a target location. The number of modules is configured to provide functions for use by a number of operators to perform a mission in addition to an airdrop.

摘要翻译： 一种方法和设备，包括外壳，处理器单元，显示器，导航模块和多个模块。 导航模块被配置为将空投系统引导至目标位置。 模块的数量被配置为提供功能以供多个操作员在空投之外执行任务。

公开(公告)号：EP2475577A2

公开(公告)日：2012-07-18

申请号：EP10751941.5

申请日：2010-09-08

申请人： Porcher Industries

发明人： FAUQUIGNON, Eric

IPC分类号： B64C31/036 ,  B64D17/02 ,  B64D17/10 ,  D03D15/00

CPC分类号： B64C31/036 ,  B64D17/025

摘要： The invention relates to a sail (2) including a fabric made of continuous warp and weft yarns. When the sail is in flight, first yarns, which are either warp yarns or weft yarns, extend in the anteroposterior direction (AP) of the sail, while the second yarns, which are either the weft yarns or the warp yarns, respectively, extend in the lateral direction (L) of the sail. In order to enhance the lightness of the fabric while retaining the mechanical strength performance thereof, the invention proposes that the resistance to deformation of the fabric along the second yarns thereof be higher, in particular by 10 %, than the resistance of the fabric along the first yarns thereof. For this purpose, the size and/or the number of the second yarns is strictly higher than the size and/or the number of the first yarns.

公开(公告)号：EP2429896A1

公开(公告)日：2012-03-21

申请号：EP10721428.0

申请日：2010-05-11

申请人： Geiger, Joachim ,  Eck, Werner

发明人： Geiger, Joachim ,  Eck, Werner

IPC分类号： B64C31/036 ,  B64C17/02

CPC分类号： B64C31/036 ,  B64D17/025

摘要： A drive unit for a paraglider (1) comprises a motor (2), a propeller (3), and a control unit (4) for the motor (2). The motor (2) can be fastened to the back of a paragliding person (7) by way of a fastening unit (6). The control unit (4) controls the motor (2) depending on control commands (SB) received and first/second sensor signals (S1, S2). The first sensor signals (S1) are characteristic of whether or not the paraglider (1) is located in a stable position above the paragliding person (7). The second sensor signals (S2) characterize a position of the paragliding person (7) relative to the propeller volume (V).

公开(公告)号：EP2007624B1

公开(公告)日：2010-11-10

申请号：EP06741675.0

申请日：2006-06-30

申请人： iii-solutions GmbH

发明人： REINHARD, Andreas

IPC分类号： B64C31/036 ,  B64D17/02 ,  B64D17/34

CPC分类号： B64D17/025

摘要： The present invention relates to an autonomous stratosphere platform which is preferably intended to be positioned in the stratosphere, is carried by a carrying shield (1) and is controlled by a control and drive unit (3) which can use control elements (301) to control the carrying shield (1) via lines (302). A cable (5) is used to connect the control and drive unit (3) to a capsule (2) which is intended to hold a payload and the requisite electrical and electronic components for operating the autonomous stratosphere platform. A control element (8) having an anchoring shield (6) is fastened to the capsule (2), again on a cable (5). The stratosphere platform experiences uplift as a result of the wind gradient between the wind layer of the anchoring shield (6) and that of the carrying shield (1). The control element (8) and the control and drive unit (3) contain at least one respective GPS receiver and radio means for transmitting their coordinates to a receiver in the capsule (2), as well as a respective cable pulley for changing the length of the cable (5). The cable (5), the capsule (2), the control and drive unit (3) and the control element (8) have radar transponders (9) or Lüneburg lenses for passive localization.

公开(公告)号：EP2236420A2

公开(公告)日：2010-10-06

申请号：EP10158091.8

申请日：2010-03-28

申请人： Köflinger, Christian

发明人： Köflinger, Christian

IPC分类号： B64D17/02 ,  B64D17/10

CPC分类号： B64D17/025 ,  B64D17/10

摘要： Ein Flugschirm mit wenigstens einem Flächengebilde (11), das mindestens einlagig ausgebildet ist und das aus einer Mehrzahl von miteinander verbundenen Stoffbahnen (12a,12b,12c) oder Stoffstücken besteht, die in Randbereichen dauerhaft miteinander verbunden sind, zeichnet sich dadurch aus, dass die Stoffbahnen (12a,12b,12c) oder Stoffstücke stoffschlüssig miteinander verbunden sind durch Verschweißen.

摘要翻译： 用于滑翔伞，滑行滑行，救援等的降落伞生产过程涉及通过将条带的材料在其边缘处焊接在一起的区段布置（11）中彼此连接的条（12a，12b，12c）或多个材料片 区域。 可以将三层或更多层材料焊接在一起，其中至少一层具有位于焊接外侧的表面的一部分与其它层的表面分开的层。

公开(公告)号：EP1463663A4

公开(公告)日：2009-08-05

申请号：EP02797214

申请日：2002-12-09

申请人： ATAIR AEROSPACE INC

发明人： PRESTON DANIEL

IPC分类号： B64D17/34 ,  B64C31/036 ,  B64D1/14 ,  B64D17/02 ,  B64D17/04 ,  B64D17/08 ,  B64D17/38 ,  B64D17/54

CPC分类号： F42B10/56 ,  B64D1/08 ,  B64D1/14 ,  B64D17/025 ,  B64D17/04 ,  B64D17/08 ,  B64D17/34 ,  B64D17/38 ,  B64D17/54 ,  B64D17/74 ,  F42B4/28 ,  F42B10/58 ,  G05D1/105

摘要： An autonomous guided parachute system for cargo drops that divides the requirements of guidance and soft landing into separate parachutes. Said invention includes a high wing-loaded ram air parachute for guidance, a larger round parachute for soft landing, a harness/container system, flight computer, position sensors and actuation system. The system is dropped from an airplane, a predetermined period of drogue fall ensures a stable position prior to deploying the guidance parachute. The flight controller determines a heading to intersect with an area substantially above the desired target and controls the guidance parachute via pneumatic actuators connected to the parachutes steering lines to fly on that heading. At a minimum altitude prior to the systems impact with the ground the flight computer transitions the system from the fast high performance guidance parachute to a larger landing parachute by releasing the guidance parachute to static line extract and deploy the landing parachute. If the system reaches a position substantially above target area prior to the parachute transition altitude flight computer controls the system into a spiral dive or other rapid altitude dropping maneuver until the transition altitude is reached. Once transitioned to the landing parachute the system descends for a brief period unguided under the landing parachute until touchdown.

公开(公告)号：EP2007624A1

公开(公告)日：2008-12-31

申请号：EP06741675.0

申请日：2006-06-30

申请人： III-Solutions GmbH

发明人： REINHARD, Andreas

IPC分类号： B64C31/036 ,  B64D17/02 ,  B64D17/34

CPC分类号： B64D17/025

摘要： The present invention relates to an autonomous stratosphere platform which is preferably intended to be positioned in the stratosphere, is carried by a carrying shield (1) and is controlled by a control and drive unit (3) which can use control elements (301) to control the carrying shield (1) via lines (302). A cable (5) is used to connect the control and drive unit (3) to a capsule (2) which is intended to hold a payload and the requisite electrical and electronic components for operating the autonomous stratosphere platform. A control element (8) having an anchoring shield (6) is fastened to the capsule (2), again on a cable (5). The stratosphere platform experiences uplift as a result of the wind gradient between the wind layer of the anchoring shield (6) and that of the carrying shield (1). The control element (8) and the control and drive unit (3) contain at least one respective GPS receiver and radio means for transmitting their coordinates to a receiver in the capsule (2), as well as a respective cable pulley for changing the length of the cable (5). The cable (5), the capsule (2), the control and drive unit (3) and the control element (8) have radar transponders (9) or Lüneburg lenses for passive localization.

公开(公告)号：EP1706317A1

公开(公告)日：2006-10-04

申请号：EP04803021.7

申请日：2004-12-16

申请人： Paraparts Holding ApS

发明人： TVINGSHOLM, John

IPC分类号： B64F1/08 ,  B64C31/036 ,  B64C31/032

CPC分类号： B64C31/032 ,  B64C31/036 ,  B64D17/025 ,  B64F1/08

摘要： A towing winch apparatus for paragliders and hang-gliders (4,6) is provided which comprises a line (3) and a towing winch mechanism (5) adapted to apply tension to said line (3) during towing, where one end (15) of the line (3) is releaseably attached to the ground (16) during towing and the towing winch mechanism (5) is attached to the paraglider or hang-glider (4,6). In this way a towing winch apparatus is provided which is useable by a pilot (1) of a paraglider or hang-glider (4,6) without needing a helper on the ground (16). In addition, after the tow process, the pilot (1) of a paraglider or hang-glider (4,6) doesn't need to go back to the ground (16) in order to collect the towing winch mechanism (5).

公开(公告)号：EP1207102A3

公开(公告)日：2002-06-12

申请号：EP01402927.6

申请日：2001-11-14

申请人： Féjan, René

发明人： Féjan, René

IPC分类号： B64D17/02 ,  B64C3/16 ,  B64C33/00

CPC分类号： B64D17/025 ,  B64C3/16 ,  Y02T50/12

摘要： L'invention concerne une série de dispositifs pour une aile de parapente, destinés à l'amélioration des qualités de vol, de pilotage et de sécurité du pilote, qui confèrent à la voilure du parapente les fonctionnalités similaires à celles des oiseaux planeurs. Le parapente selon l'invention comporte une aile (1) dont la voûte est munie d'extrémités de voilure (2) à concavité inversée, et d'une partie centrale (3) invaginée en forme de V. L'aile (1) comporte au bord de fuite une fente entre les tissus extrados (5) et intrados (6). Une commande (11) permet de réduire l'envergure par invagination de la partie centrale. Une commande (20) permet d'augmenter la flèche par plissement du bord de fuite. Deux commandes (34) permettent de moduler la voûte par modification de la longueur du suspentage. Les ouvertures de bord d'attaque sont munies de clapets (39) pour prévenir le dégonflage du parapente.

公开(公告)号：EP1094000A3

公开(公告)日：2002-05-08

申请号：EP00122063.1

申请日：2000-10-11

申请人： Diehl Munitionssysteme GmbH & Co. KG

发明人： Schleicher, Ulrich, Dr.

IPC分类号： B64C31/028 ,  F42B10/56 ,  B64D17/02

CPC分类号： F42B10/56 ,  B64C31/036 ,  B64D17/025

摘要： Ein Gleitschirm als universeller Lastenträger weist in einem Behälter eine Steuereinrichtung auf, die über Steuerleinen die Konfiguration des Gleitschirms beeinflußt. Der Behälter (2) ist wenigstens zweigeteilt. Im oberen Teil (13) sind gleitschirmseitige Komponenten angeordnet, wie Energieversorgung, Antriebsaggregat, Autopilot, Aktuatoren für Steuerleinen, Navigationsmittel, Sender und Empfänger. In einem unteren Teil (23) ist eine Nutzlast bzw. eine absetzbare Nutzlast angeordnet.