首页> 外国专利> METHOD OF SHIFTING AVIATION VEHICLE BETWEEN CROSS-WIND FLIGHT AND HOVER FLIGHT AND SYSTEM

METHOD OF SHIFTING AVIATION VEHICLE BETWEEN CROSS-WIND FLIGHT AND HOVER FLIGHT AND SYSTEM

机译:横风飞行与悬停飞行之间的飞行飞行方法及系统

摘要

PROBLEM TO BE SOLVED: To optimize an aviation vehicle for power generation flight.SOLUTION: A method can include a step for making an aviation vehicle operate in hover flight orientation. The aviation vehicle can connect to a tether which defines a tether ball having a radius based on length of the tether, and the tether can connect to a ground station. The method can include a step for positioning the aviation vehicle at a first position which is substantially on the tether ball. The method can include a step in which by shifting the aviation vehicle from a hover flight orientation to an advancing flight orientation, the aviation vehicle shifts from the tether ball. The method can include a step in which the aviation vehicle is operated to rise, at a certain rising angle, to a second position which is substantially on the tether ball, in the advancing flight orientation. The first and second positions may be substantially on a lee side of the ground station.SELECTED DRAWING: Figure 3b
机译:要解决的问题:优化用于发电飞行的航空器。解决方案:一种方法可以包括使航空器以悬停飞行方向运行的步骤。航空器可以连接至系绳,该系绳限定具有基于系绳的长度的半径的系绳球,并且该系绳可以连接至地面站。该方法可以包括用于将飞行器定位在基本上在系链球上的第一位置的步骤。该方法可以包括以下步骤:其中,通过将飞行器从悬停飞行方向转换为前进飞行方向,该飞行器从系绳球转换。该方法可以包括以下步骤:在该步骤中,操作飞行器以一定的上升角上升到在前进的飞行方向上基本上在系绳球上的第二位置。第一和第二位置可能基本上在地面站的背风侧。选定的图:图3b

著录项

  • 公开/公告号JP2017124824A

    专利类型

  • 公开/公告日2017-07-20

    原文格式PDF

  • 申请/专利权人 X DEVELOPMENT LLC;

    申请/专利号JP20170022562

  • 发明设计人 ERIK CHRISTOPHER CHUBB;DAMON VANDER LIND;

    申请日2017-02-09

  • 分类号B64C31/06;B64F3;

  • 国家 JP

  • 入库时间 2022-08-21 14:01:24

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