专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

1. 发明授权

EP3102488B1 GESCHLEPPTER AKTIVER FLUGKÖRPER ZUR ERMITTLUNG VON MESSDATEN 有权
标题翻译： GESCHLEPPTER AKTIVERFLUGKÖRPERZUR ERMITTLUNG VON MESSDATEN
公开(公告)号：EP3102488B1
公开(公告)日：2017-04-26
申请号：EP15708707.3
申请日：2015-01-24
申请人： Alfred-Wegener-Institut Helmholtz-Zentrum für Polar- und Meeresforschung
发明人： HERBER, Andreas , KALMBACH, Dirk , GERDES, Rüdiger , WATSON, James Bradley
IPC分类号： B64C13/06 , B64D3/00
CPC分类号： B64D3/00 , B64C9/326 , B64C13/16 , B64C2009/005 , B64D27/24 , B64D45/00 , B64D47/08

2. 发明公开

EP3102488A1 GESCHLEPPTER AKTIVER FLUGKÖRPER ZUR ERMITTLUNG VON MESSDATEN 有权
标题翻译： GESCHLEPPTER AKTIVERFLUGKÖRPERZUR ERMITTLUNG VON MESSDATEN
公开(公告)号：EP3102488A1
公开(公告)日：2016-12-14
申请号：EP15708707.3
申请日：2015-01-24
申请人： Alfred-Wegener-Institut Helmholtz-Zentrum für Polar- und Meeresforschung
发明人： HERBER, Andreas , KALMBACH, Dirk , GERDES, Rüdiger , WATSON, James Bradley
IPC分类号： B64D3/00
CPC分类号： B64D3/00 , B64C9/326 , B64C13/16 , B64C2009/005 , B64D27/24 , B64D45/00 , B64D47/08
摘要： Towed flying objects (01) are towed through the air on a cable by an aircraft and in the process carry out measurements for, for example, environmental observation and monitoring processes in inaccessible areas, for example in the polar regions. The passive navigation by means of the aircraft is hazardous here, in particular at very low heights and when obstacles arise. Known flying objects (01) are controlled independently at the flying height by means of an automatic flight control system and have an adjustment device of the aerofoils which is retracted into the non-deflected home position in the event of malfunctions occurring. The flying object (01) according to the invention is, in contrast, independently fully manoeuvrable in all three spatial directions and has an aileron (21), a pitch elevator (27) and a stabilizer (28). An automatic flight control system (32) has, in addition to a stabilization module (33) which also serves specifically for avoiding dangerous oscillating motions of the flying object (01) when bringing it in, an avoidance module (34) which operates in the three-dimensional space, and a malfunction system (36) which, in the event of a failure of its power supply owing to a malfunction, moves the aileron, pitch elevator and stabilizer (21, 27, 28) into the non-deflected home position in a purely mechanical fashion and securely locks them there, with the result that the flying object (01) can be brought in without manoeuvring operations.
摘要翻译：用于确定测量数据的圆柱形主动式空中平台可锁定到承载电缆，使得机载平台能够通过空气拖动。传感器被配置为确定测量数据和机载平台的飞行位置。布置在机载平台的中部区域的两个翼型件是可调节的，并且连接到被配置为副翼的电气调节装置，以便改变垂直飞行位置。相反的两个第一空气引导表面和两个第二空气引导表面具有分别配置为电梯和方向舵的电调节装置。计算机支持的控制装置包括自动飞行管理系统，其被配置为提供对空中平台的垂直飞行位置的自动控制，并且被配置为控制另外的电气调节装置。

3. 发明公开

EP3233634A1 AERODYNAMISCH GEFORMTER, AKTIVER SCHLEPPKÖRPER 有权
标题翻译： AERODYNAMISCH GEFORMTER，AKTIVERSCHLEPPKÖRPER
公开(公告)号：EP3233634A1
公开(公告)日：2017-10-25
申请号：EP15831127.4
申请日：2015-12-04
申请人： Alfred-Wegener-Institut Helmholtz-Zentrum für Polar- und Meeresforschung
发明人： HERBER, Andreas , KALMBACH, Dirk , GERDES, Rüdiger , BAYER, Hans-Jörg
IPC分类号： B64D3/02 , B64C3/16 , F41J9/10 , B64C1/00
CPC分类号： B64D3/02 , B64C3/16 , B64C39/022 , B64C2001/0045 , B64C2201/104 , B64C2201/12 , B64C2201/141 , B64C2201/206 , F41J9/10
摘要： Known towed bodies can be maneuvered in all three dimensions but, as pure airborne targets, do not have a large load capacity. The towed body (01) according to the invention is designed for bearing large loads and serves exclusively scientific and commercial measurement purposes. To achieve very good aerodynamic properties, the towed body has a fuselage (02) comprising a triangular transverse plane (15), wherein the upper face (18) is designed to be wide and the lower face (19) is designed to be narrow, and comprising a curvature (23) only on the upper face (18), whereas the lower face (19) runs straight. The wings (03) are bent and consist of two segments (07, 08). Small segments (07) are arranged at the bottom of the fuselage (02), which small segments point downwards and stabilise the towed body (01), large segments (08) are connected to the small segments (07), which large segments point upwards and generate lift. In the front and middle region of the fuselage (02) and in the small segments (07) there are load chambers (10, 11) which can have user-friendly segment chambers (22). The unit chamber (09) comprising various units (27), such as a position-stabilising gyroscope system, an anti collision module, accumulators, a generator and an emergency parachute system (25), is located in the rear region of the towed body (01).
摘要翻译：已知的拖曳机构可以在所有三维空间中进行操纵，但是由于纯粹的空中目标，其载荷能力并不大。根据本发明的拖曳主体（01）被设计用于承受大负载并且专门用于科学和商业测量目的。为了实现非常好的空气动力学特性，被拖曳体具有包括三角形横向平面（15）的机身（02），其中上表面（18）被设计成宽的并且下表面（19）被设计成窄的，并且仅在上表面（18）上包括曲率（23），而下表面（19）直线延伸。翼（03）弯曲并由两个部分（07,08）组成。在机身（02）的底部设置小段（07），小段向下指向并稳定拖曳主体（01），大段（08）连接到小段（07），大段向上并产生升力。在机身（02）的前部和中部区域以及小部分（07）中，存在可具有用户友好的分段腔室（22）的装载腔室（10,11）。包括诸如位置稳定陀螺仪系统，防撞模块，蓄电池，发电机和应急降落伞系统（25）的各种单元（27）的单元室（09）位于拖曳主体（01）。

4. 发明公开

EP3947140A1 MANÖVRIERFÄHIGER MESSKÖRPER ZUR ERMITTLUNG VON MESSDATEN MIT FEHLFUNKTIONSMODUL 有权
公开(公告)号：EP3947140A1
公开(公告)日：2022-02-09
申请号：EP20714470.0
申请日：2020-03-06
申请人： Alfred-Wegener-Institut Helmholtz-Zentrum für Polar- und Meeresforschung
发明人： HERBER, Andreas , KALMBACH, Dirk , BAYER, Hans-Jörg
IPC分类号： B63G8/14 , B63G8/42 , B64C13/16 , F41J9/10

5. 发明授权

EP3233634B1 AERODYNAMISCH GEFORMTER, AKTIVER SCHLEPPKÖRPER 有权
公开(公告)号：EP3233634B1
公开(公告)日：2018-06-13
申请号：EP15831127.4
申请日：2015-12-04
申请人： Alfred-Wegener-Institut Helmholtz-Zentrum für Polar- und Meeresforschung
发明人： HERBER, Andreas , KALMBACH, Dirk , GERDES, Rüdiger , BAYER, Hans-Jörg
IPC分类号： B64D3/02 , B64C3/16 , F41J9/10 , B64C1/00
CPC分类号： B64D3/02 , B64C3/16 , B64C39/022 , B64C39/024 , B64C2001/0045 , B64C2201/104 , B64C2201/12 , B64C2201/126 , B64C2201/141 , B64C2201/206 , F41J9/10

你已经成功收藏专利！

检索式保存成功!

IPRDB

热门服务

关于我们

友情链接

联系方式