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1.发明公开AUTOMATED BALLOON LAUNCHING SYSTEM AND METHOD FOR LAUNCHING 审中-公开AUTOMATISIERSES BALLONSTARTSYSTEM UND VERFAHREN ZUM STARTEN
公开(公告)号：EP3102969A4
公开(公告)日：2017-09-06
申请号：EP15746021
申请日：2015-02-06
申请人： VAISALA OYJ
发明人： LEINONEN ISMO , SAARI TUOMO
摘要： According to an example aspect of the present invention, there is provided an automated balloon launching system for launching at least one balloon such as a meteorological balloon or a radiosonde. The system comprises a container and a storage arranged in the container for storing at least one box at a defined storage position p=1, 2, . . . , n. The at least one box includes a balloon and a sonde. A release silo is arranged at least partially on top of or above and adjacent to the container for sheltering the balloon during inflation. A x-, y- and z-manipulator is arranged in the container for removing a specific box from one of the defined storage positions p=1, 2, . . . , n, and for subsequent feeding the release silo with the specific box. The present invention also concerns a method for launching at least one balloon such as a meteorological balloon or a radiosonde.
摘要翻译： 根据本发明的示例性方面，提供了一种用于发射至少一个气球的气球发射系统，例如气象气球或无线电探空仪。 该系统包括容器和布置在容器中的存储器，用于在限定的存储位置p = 1,2，...处存储至少一个盒子。 。 。 ，n。 至少一个盒子包括气球和探测器。 释放筒仓至少部分地布置在容器的顶部上方或上方并且与容器相邻，用于在充气期间遮蔽球囊。 在容器中布置一个x，y和z操纵器，用于从定义的存储位置p = 1,2，...中的一个移除特定的盒子。 。 。 ，n，并随后将该释放筒仓送入特定的箱子。 本发明还涉及用于发射至少一个气球的方法，例如气象气球或无线电探空仪。
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公开(公告)号：EP2734440B1
公开(公告)日：2015-06-10
申请号：EP12750421.5
申请日：2012-07-19
申请人： Dirisolar
发明人： TIXIER, Philippe
CPC分类号： B64B1/005 , B64B1/00 , B64B1/20 , B64B1/66 , B64B2201/00
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公开(公告)号：EP2488409A1
公开(公告)日：2012-08-22
申请号：EP10785104.0
申请日：2010-10-12
发明人： REGAS, Baptiste , JOZAN, Olivier
IPC分类号： B64B1/00
摘要： The invention relates to an airship (1) including a flexible envelope (2) having no rigid inner structure containing a gas that is lighter than air, and a gondola (3). The balloon also includes three legs for setting the balloon on the surface and a landing structure (5). Said landing structure (5) is located on the outside of the envelope, and provides a connection between the legs (6a, 6b, 6c), the gondola (3) and the envelope (2) while surrounding the envelope (2).
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4.发明公开AUTONOMOUS INTELLIGENCE SURVEILLANCE RECONNAISSANCE AND PAYLOAD DELIVERY SYSTEM WITH SAFE RETURN 审中-公开具有安全返回的自主智能监视侦察和有效载荷传送系统
公开(公告)号：EP3309055A1
公开(公告)日：2018-04-18
申请号：EP17198066.7
申请日：2012-08-06
发明人： STIGLER, Michael , SETAR, Nicholas
IPC分类号： B64B1/00
CPC分类号： B64B1/12 , B64B1/005 , B64B1/10 , B64B1/14 , B64B1/18 , B64B1/22 , B64B1/24 , B64B1/36 , B64B1/60 , B64B1/62 , B64B1/64 , B64B1/66 , B64C39/024 , B64C2201/022 , B64C2201/126 , B64C2201/127 , B64C2201/141 , G05D1/0027 , G05D1/101 , G08G5/0069 , G09F21/04 , G09F21/06
摘要： An intelligence, surveillance, and reconnaissance system and associated operating method is disclosed including a ground station and one or more autonomous aerial vehicles. Each automomous vehicle is adapted to
a) self-monitor a plurality of environment data;
b) calculate, based at least in part upon the environment data, a soft wall radius from which it can return to the command and control interface station;
c) receive a destination position to which it is commanded to fly;
d) determine if the destination position is beyond the soft wall radius; and
e) communicate an alert to the command and control interface station if the destination position is beyond the soft wall radius.摘要翻译： 公开了包括地面站和一个或多个自主飞行器的情报，监视和侦察系统以及相关的操作方法。 每辆自动驾驶车辆适用于：a）自我监视多个环境数据; b）至少部分地基于环境数据计算软墙半径，其可以返回到命令和控制接口站; c）接收命令飞往的目的地位置; d）确定目标位置是否超出软壁半径; 和e）如果目的地位置超出软墙半径，则向指挥和控制接口站传送警报。
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公开(公告)号：EP2763901A1
公开(公告)日：2014-08-13
申请号：EP12778786.9
申请日：2012-10-01
申请人： Voliris
发明人： BERNARD, Alain
CPC分类号： B65G63/004 , B64B1/005 , B64B1/02 , B64B1/04 , B64B2201/00 , B64F1/32
摘要： The invention relates to a method for transporting containers (30), in which a group of containers comprises a sub-group M assigned to the transportation of goods and a sub-group V assigned to the transportation of a vehicle (10) that can be dismantled, and in which: prior to transportation, the dismantled vehicle (10) is loaded into the containers (30) of sub-group V; between the initial handling centre (1) and an intermediate handling centre (2), the group of containers including sub-groups M and V is transported by a first transport means; between the intermediate handling centre (2) and the final handling centre (3), sub-group M of containers (30) is transported by the vehicle (10) that can be dismantled; and the dismantlable vehicle (10) is a modular multi-lift aircraft formed by modules that can be housed in the containers (30) of group V.
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6.发明公开
公开(公告)号：EP2595874A2
公开(公告)日：2013-05-29
申请号：EP11738354.7
申请日：2011-07-15
申请人： LTA Corporation
发明人： GOELET, John
IPC分类号： B64B1/00 , B64B1/08 , B64B1/10 , B64B1/14 , B64B1/20 , B64B1/22 , B64B1/28 , B64B1/34 , B64B1/58
CPC分类号： B64B1/06 , B64B1/005 , B64B1/08 , B64B1/10 , B64B1/16 , B64B1/20 , B64B1/22 , B64B1/28 , B64B1/30 , B64B1/58 , B64D9/00
摘要： A solar-powered airship with a hull configured to contain a gas and at least one propulsion assembly with a propulsion device and electric motors configured to drive the propulsion device. The airship may also include a power supply system including solar panels operatively coupled to the electric motors and configured to supply power to the electric motors. The power supply system may also include batteries operatively coupled to the solar panels and configured to receive and store electrical energy supplied by the solar panels, the batteries being further operatively coupled to the electric motors and configured to supply power to the electric motors. The batteries may each be located within an outer envelope of the airship defined by the hull of the airship in a position selected to provide ballast. The solar-powered airship may also include a cargo system configured to contain passengers or freight.
摘要翻译： 具有船体的太阳能飞艇，其构造成容纳气体，并且至少一个具有推进装置的推进组件和构造成驱动推进装置的电动马达。 飞艇还可以包括电源系统，其包括可操作地耦合到电动机并被配置为向电动机供电的太阳能电池板。 电源系统还可以包括可操作地耦合到太阳能电池板并被配置为接收和存储由太阳能电池板供应的电能的电池，电池进一步可操作地耦合到电动机并且被配置为向电动机供电。 电池可以各自位于由飞艇的船体在选定为提供镇流器的位置中限定的飞艇的外部封套内。 太阳能飞艇还可以包括被配置为容纳乘客或货物的货物系统。
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7.发明公开AUTONOMOUS INTELLIGENCE SURVEILLANCE RECONNAISSANCE AND PAYLOAD DELIVERY SYSTEM AND METHOD OF USING SAME 有权自动化ÜBERWACHUNGS-UND ERKENNUNGS- SOWIE NUTZLASTABGABESYSTEM MITFLUIDBEFÜLLUNGSSYSTEM
公开(公告)号：EP2739527A2
公开(公告)日：2014-06-11
申请号：EP12866919.9
申请日：2012-08-06
IPC分类号： B64B1/00
CPC分类号： B64B1/12 , B64B1/005 , B64B1/10 , B64B1/14 , B64B1/18 , B64B1/22 , B64B1/24 , B64B1/36 , B64B1/60 , B64B1/62 , B64B1/64 , B64B1/66 , B64C39/024 , B64C2201/022 , B64C2201/126 , B64C2201/127 , B64C2201/141 , G05D1/0027 , G05D1/101 , G08G5/0069 , G09F21/04 , G09F21/06
摘要： An intelligence, surveillance, and reconnaissance system and associated operating method is disclosed including a ground station and one or more autonomous aerial vehicles. Each automomous vehicle is adapted to a) self-monitor a plurality of environment data; b) calculate, based at least in part upon the environment data, a soft wall radius from which it can return to the command and control interface station; c) receive a destination position to which it is commanded to fly; d) determine if the destination position is beyond the soft wall radius; and e) communicate an alert to the command and control interface station if the destination position is beyond the soft wall radius.
摘要翻译： 披露了一个智能，监视和侦察系统，包括地面站和一个或多个空中飞行器。 飞行器是能够将情报数据传送到地面站的自主系统，并用作导弹发射包的一部分。 多个飞行器可以被配置为在地面上的大面积上施放广泛的侦察网，包括由多个飞行器中的每一个提供的较小的重叠侦察区域。
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公开(公告)号：EP2734440A1
公开(公告)日：2014-05-28
申请号：EP12750421.5
申请日：2012-07-19
申请人： Dirisolar
发明人： TIXIER, Philippe
CPC分类号： B64B1/005 , B64B1/00 , B64B1/20 , B64B1/66 , B64B2201/00
摘要： The present invention relates to an air vehicle such as an airship, which has a rounded top portion, and the bottom portion of which has a substantially planar shape (711), specifically consisting of a region which has a smaller inclination, which is referred to as a bottom surface (S2), and the surface area of which is larger or even much larger than that of the intermediate region having a greater inclination, referred to as an intermediate surface (S1). Said general shape produces, due to relative wind (69), a resulting overall downward force (67) near the ground. According to the invention, said vehicle also includes a device for anchoring same to the ground (722), said anchoring device being stationary or controllable from said vehicle, located at the front portion of said vehicle, and projecting downward, in particular a ram (722, 9) including a portion (921, 922) which can be expanded by applying a bar (924) against a translatably movable shoulder (923). The invention also relates to a landing method implementing such a vehicle. Said method involves, as a result of the downward force (67) with compensation (65) by maintaining a nose-up attitude (T711), downward flight until a rear portion (730) of the vehicle makes contact with the ground, followed by reducing the nose-up angle until the anchoring device makes contact with the ground, in particular with a ram (722, 9) sinking into the ground. Preferably, the method also includes docking, in particular by means of an expandable ram (9), while the vehicle is applied against the ground due to the downward force.
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公开(公告)号：EP0861773B1
公开(公告)日：2000-03-22
申请号：EP96935628.6
申请日：1996-10-07
摘要： The hybrid dirigible craft belongs to the category of flying vehicles which use an air cushion and take off and land at any type of airfield. The aim of the invention is to design an improved dirigible craft capable of taking off from and landing on water and low-load bearing surfaces. To that end the hybrid dirigible craft comprises the following elements: a discoid body (1) with a central passage (2) in which is mounted a flow-permitting body (5) with a rotor (6) on its upper part and secured to the walls by radial partitions (7) which have an aerodynamic profile; the pilot-passenger and cargo compartments (9 and 10 respectively); a propulsion unit with propellers (8), units for landing on an air cushion in the form of an inflatable toroidal bag (11) and wheel-skid supports (12, 13) mounted on the lower surfaces; rotating flaps (3) mounted at the inlet into the central passage (2); control and stabilising elements (4) mounted at the outlet of the central passage (2); outer wing units (14) and a tail assembly with stabiliser (19) and two or more fins (17) mounted on the rear part of the hull; airflow flaps (21) on the rear flaps of the outer wing elements and hull (22); and airflow control surfaces (20) on the stabiliser and outer wing elements. The dirigible craft also has elevons (22) on the stabiliser and a flexible guard element (23) mounted on and underneath the forward part of the toroidal bag (11). It also has gear for taking off from water in the form of gliding surfaces (28) underneath the compartment (9).
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公开(公告)号：EP0735969A1
公开(公告)日：1996-10-09
申请号：EP95904567.0
申请日：1994-12-19
申请人： Gobbi, Matthieu , Giacomoni, Jérôme
发明人： Gobbi, Matthieu , Giacomoni, Jérôme
摘要： An apparatus for landing a tethered balloon, comprising a balloon which is drawn down to the ground (9) by means of a pulling cable (2) and has a gondola (6) hollow central portion for the cable (2) to pass therethrough, and a cable take-up and pay-out assembly (11) arranged in a hole (10) in the ground. A landing platform (3) covering the hole (10) comprises an opening (12) through which the cable (2) passes and which is centred on the vertical pay-out axis (12a) of the pulling cable (2). The landing platform (3) consists of a curved surface (3a, 3b) of at least one upright cone frustum (13, 14) with a substantially horizontal ring-shaped landing pad (15, 15') extending from the lower end thereof, said frustum being centred on the vertical pay-out axis (12a) of the pulling cable (2). The gondola (6) of the balloon (1) has at least three swivelling wheels attached to the underside of the gondola (6) in a ring-shaped portion having the same size as the landing pad (15, 15').
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