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公开(公告)号：US09714092B2
公开(公告)日：2017-07-25
申请号：US15117211
申请日：2015-01-24
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.
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公开(公告)号：US20170341749A1
公开(公告)日：2017-11-30
申请号：US15535431
申请日：2015-12-04
CPC分类号： B64D3/02 , B64C3/16 , B64C39/022 , B64C2001/0045 , B64C2201/104 , B64C2201/12 , B64C2201/141 , B64C2201/206 , F41J9/10
摘要： An aerodynamically shaped, active towed body includes a fuselage curved along its vertical and horizontal longitudinal plane. The fuselage has a unit chamber and a load chamber. A transverse plane of the fuselage is triangular, two upper corners being located on an upper face of the fuselage and a lower corner being located on a lower face of the fuselage. Each of two wings is subdivided into a small and a large segment. The small segment points downwards and is attached to the fuselage in a region of the lower corner and the large segment points upwards and is attached to the small segment. Each of the small segments comprise an additional load chamber. The towed body further includes a tail fin, rudders that are each adjustable by the control device and a coupling for the towing cable.
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公开(公告)号：US09849983B2
公开(公告)日：2017-12-26
申请号：US15535431
申请日：2015-12-04
CPC分类号： B64D3/02 , B64C3/16 , B64C39/022 , B64C2001/0045 , B64C2201/104 , B64C2201/12 , B64C2201/141 , B64C2201/206 , F41J9/10
摘要： An aerodynamically shaped, active towed body includes a fuselage curved along its vertical and horizontal longitudinal plane. The fuselage has a unit chamber and a load chamber. A transverse plane of the fuselage is triangular, two upper corners being located on an upper face of the fuselage and a lower corner being located on a lower face of the fuselage. Each of two wings is subdivided into a small and a large segment. The small segment points downwards and is attached to the fuselage in a region of the lower corner and the large segment points upwards and is attached to the small segment. Each of the small segments comprise an additional load chamber. The towed body further includes a tail fin, rudders that are each adjustable by the control device and a coupling for the towing cable.
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公开(公告)号：US20160355260A1
公开(公告)日：2016-12-08
申请号：US15117211
申请日：2015-01-24
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。
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