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11. 发明授权

US09725160B2 Flow body and method for taking in and/or blowing out fluid through a plurality of openings in a flow surface section of a flow body 有权
公开(公告)号：US09725160B2
公开(公告)日：2017-08-08
申请号：US13606835
申请日：2012-09-07
申请人： Burkhard Gölling , Erik Wassen , Tobias Hoell , Frank Thiel
发明人： Burkhard Gölling , Erik Wassen , Tobias Hoell , Frank Thiel
IPC分类号： B64C21/02
CPC分类号： B64C21/025 , B64C2230/06 , Y02T50/166
摘要： A flow body and method for taking in and/or blowing out fluid through a plurality of openings in a flow surface section of a flow body is disclosed. In some aspects, the flow body includes a flow surface section that extends in a flow body wingspan direction and a flow body chord direction and with a plurality of fluid lines that lead into the flow surface section and respectively form an opening therein. In some aspects, the method includes taking in and/or blowing out fluid through at least one fluid line that leads into a flow surface section of a flow body and respectively forms an opening therein.

12. 发明授权

US09090340B2 High lift system for an aircraft 有权
标题翻译：飞机高升程系统
公开(公告)号：US09090340B2
公开(公告)日：2015-07-28
申请号：US13608035
申请日：2012-09-10
申请人： Burkhard Gölling
发明人： Burkhard Gölling
IPC分类号： B64C21/04 , B64C9/18 , B64C21/08 , B64C21/06
CPC分类号： B64C21/04 , B64C9/18 , B64C21/06 , B64C21/08 , B64C2230/04 , B64C2230/06 , Y02T50/166 , Y02T50/44
摘要： A high lift system with a main wing and control flaps, wherein the respective guiding device are at least partially provided with a fairing, having a flow control device for purposes of controlling the flow around the high lift system with at least two inlet ducts running along the main wing chordwise direction with in each case at least one inlet, which device is located on or underneath the lower surface of the high lift system, wherein at least one outlet duct for air is furthermore provided, which is connected with the inlet ducts in a fluid-communicating manner, and has at least one outlet, which is located on the upper surface of at least one regulating flap and/or with respect to the main wing chordwise direction in the rear third of the main wing of the high lift system.
摘要翻译：具有主翼和控制翼片的高升程系统，其中相应的引导装置至少部分地设置有整流罩，具有流量控制装置，用于控制围绕高升程系统的流动，其中至少两个入口管道沿着主翼弦方向，在每种情况下至少有一个入口，该装置位于高升力系统的下表面上或下方，其中还提供至少一个用于空气的出口管道，其与入口管道连接流体连通方式，并且具有至少一个出口，其位于至少一个调节翼片的上表面上和/或相对于主升力方向的主翼弦方向位于高升力系统的主翼的后三分之一。

13. 发明授权

US08690107B2 High-lift system for an aircraft 有权
标题翻译：一架飞机高架系统
公开(公告)号：US08690107B2
公开(公告)日：2014-04-08
申请号：US13530156
申请日：2012-06-22
申请人： Burkhard Gölling
发明人： Burkhard Gölling
IPC分类号： B64C21/08
CPC分类号： B64C9/18 , B64C9/16 , B64C9/38 , B64C21/04 , Y02T50/166 , Y02T50/32 , Y02T50/44
摘要： A high-lift system with a main wing and adjustable flaps as well as guiding devices for holding the adjustable flaps and adjustment devices for adjusting the adjustable flaps, wherein the respective guiding device and/or adjustment device at least in part include/includes a fairing, including a flow influencing device for influencing the flow around the high-lift system, with at least one inlet line with at least one inlet that is situated on or below the bottom of the high-lift system, wherein, furthermore, at least one outlet line for air is provided that includes a fluid-communicating connection to the inlet line and includes at least one outlet situated at the top in the region of at least one adjustable flap of the high-lift system.
摘要翻译：具有主翼和可调节翼片的高升力系统以及用于保持可调节翼片的引导装置和用于调节可调节翼片的调节装置，其中相应的引导装置和/或调节装置至少部分地包括/包括整流罩，包括用于影响高升力系统周围的流动的流动影响装置，其中至少一个入口管线具有位于高升程系统底部或底部的至少一个入口，此外，至少一个提供用于空气的出口管线，其包括与入口管线的流体连通连接，并且包括位于高升程系统的至少一个可调节的挡板的区域中的顶部的至少一个出口。

14. 发明申请

US20130240676A1 HIGH LIFT SYSTEM FOR AN AIRCRAFT 有权
标题翻译：用于飞机的高起升系统
公开(公告)号：US20130240676A1
公开(公告)日：2013-09-19
申请号：US13608035
申请日：2012-09-10
申请人： Burkhard Gölling
发明人： Burkhard Gölling
IPC分类号： B64C21/04 , B64C21/06
CPC分类号： B64C21/04 , B64C9/18 , B64C21/06 , B64C21/08 , B64C2230/04 , B64C2230/06 , Y02T50/166 , Y02T50/44
摘要： A high lift system with a main wing and control flaps, wherein the respective guiding device are at least partially provided with a fairing, having a flow control device for purposes of controlling the flow around the high lift system with at least two inlet ducts running along the main wing chordwise direction with in each case at least one inlet, which device is located on or underneath the lower surface of the high lift system, wherein at least one outlet duct for air is furthermore provided, which is connected with the inlet ducts in a fluid-communicating manner, and has at least one outlet, which is located on the upper surface of at least one regulating flap and/or with respect to the main wing chordwise direction in the rear third of the main wing of the high lift system.
摘要翻译：具有主翼和控制翼片的高升程系统，其中相应的引导装置至少部分地设置有整流罩，具有流量控制装置，用于控制围绕高升程系统的流动，其中至少两个入口管道沿着主翼弦方向，在每种情况下至少有一个入口，该装置位于高升力系统的下表面上或下方，其中还提供至少一个用于空气的出口管道，其与入口管道连接流体连通方式，并且具有至少一个出口，其位于至少一个调节翼片的上表面上和/或相对于主升力方向的主翼弦方向位于高升力系统的主翼的后三分之一。

15. 发明申请

US20120318929A1 AIRCRAFT WITH A REFUELING DEVICE AND METHOD FOR CONTROLLING THE FLIGHT PATH OF AN AIRCRAFT DURING ITS REFUELING 审中-公开
标题翻译：具有补救装置的飞机和在其补救期间控制飞机的飞行路径的方法
公开(公告)号：US20120318929A1
公开(公告)日：2012-12-20
申请号：US13478433
申请日：2012-05-23
申请人： Burkhard Gölling
发明人： Burkhard Gölling
IPC分类号： B64D39/00 , B64C13/16
CPC分类号： B64C13/18 , B64C13/16 , B64C17/10 , B64D39/00
摘要： An aircraft with a refueling device for receiving fuel from a tanker aircraft in-flight is described, including an arrangement of flow influencing devices, an arrangement of flow condition sensor devices measuring flow conditions on respective surface segments, a flight data transmission device receiving flight data of a tanker aircraft, a flight path specification module that determines a nominal flight path or a nominal flight path corridor from the flight data of the flight data transmission device, and a flight control device configured to generate nominal commands for the flow influencing devices based on the measured flow condition and the nominal flight path or the nominal flight path corridor. These nominal commands control or maintain the movement of the aircraft along the nominal flight path or in the nominal flight path corridor. A method for controlling the flight path of an aircraft during the refueling thereof is also provided.
摘要翻译：描述了一种具有用于从飞机上的油罐飞机接收燃料的加油装置的飞机，包括流动影响装置的布置，测量各个表面段上的流动状况的流动状况传感器装置的布置，接收飞行数据的飞行数据传输装置飞行路径规范模块，其根据飞行数据传输装置的飞行数据确定标称飞行路径或标称飞行路径走廊;以及飞行控制装置，其被配置为基于以下方式为流量影响装置生成标称命令：测量的流量条件和标称飞行路径或名义飞行路径走廊。这些名义命令控制或保持飞机沿标称飞行路径或标称飞行路径走廊的运动。还提供了一种用于在加油期间控制飞机的飞行路径的方法。

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