公开(公告)号：US09714092B2

公开(公告)日：2017-07-25

申请号：US15117211

申请日：2015-01-24

申请人： ALFRED-WEGENER-INSTITUT HELMHOLTZ-ZENTRUM FUER POLAR- UND MEERESFORSCHUNG

发明人： Andreas Herber ,  Dirk Kalmbach ,  Ruediger Gerdes ,  James Bradley Watson

IPC分类号： B64D3/00 ,  B64C13/16 ,  B64C9/32 ,  B64D27/24 ,  B64D45/00 ,  B64D47/08 ,  B64C9/00

CPC分类号： B64D3/00 ,  B64C9/326 ,  B64C13/16 ,  B64C2009/005 ,  B64D27/24 ,  B64D45/00 ,  B64D47/08

摘要： A cylindrical active airborne platform for determining measurement data is latchable to a carrying cable such that the airborne platform is towable through the air. Sensors are configured to determine the measurement data and a flight position of the airborne platform. Two aerofoils arranged in the middle region of the airborne platform are adjustable and are connected to electrical adjusting devices configured as ailerons so as to vary a vertical flight position. Opposing two first air guide surfaces and two second air guide surfaces have further electrical adjusting devices configured respectively as elevators and as rudders. A computer-supported control device comprises an automatic flight management system that is configured to provide self-acting control of the vertical flight position of the airborne platform, and that is configured to control the further electrical adjusting devices.

公开(公告)号：US20160355260A1

公开(公告)日：2016-12-08

申请号：US15117211

申请日：2015-01-24

申请人： ALFRED-WEGENER-INSTITUT HELMHOLTZ-ZENTRUM FUER POLAR- UND MEERESFORSCHUNG

发明人： Andreas Herber ,  Dirk Kalmbach ,  Ruediger Gerdes ,  James Bradley Watson

IPC分类号： B64D3/00 ,  B64D45/00 ,  B64C13/16 ,  B64D47/08 ,  B64D27/24 ,  B64C9/32

CPC分类号： B64D3/00 ,  B64C9/326 ,  B64C13/16 ,  B64C2009/005 ,  B64D27/24 ,  B64D45/00 ,  B64D47/08

摘要： A cylindrical active airborne platform for determining measurement data is latchable to a carrying cable such that the airborne platform is towable through the air. Sensors are configured to determine the measurement data and a flight position of the airborne platform. Two aerofoils arranged in the middle region of the airborne platform are adjustable and are connected to electrical adjusting devices configured as ailerons so as to vary a vertical flight position. Opposing two first air guide surfaces and two second air guide surfaces have further electrical adjusting devices configured respectively as elevators and as rudders. A computer supported control device comprises an automatic flight management system that is configured to provide self-acting control of the vertical flight position of the airborne platform, and that is configured to control the further electrical adjusting devices.

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，使得机载平台可通过空气拖动。 传感器被配置为确定测量数据和机载平台的飞行位置。 布置在机载平台中部区域的两个翼型可调，并连接到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气调节装置。 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。