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1. 发明授权

US09014877B2 Aircraft with a control device 有权
标题翻译：具有控制装置的飞机
公开(公告)号：US09014877B2
公开(公告)日：2015-04-21
申请号：US13525282
申请日：2012-06-16
申请人： Burkhard Gölling , Frank Haucke , Matthias Bauer , Wolfgang Nitsche , Inken Peltzer
发明人： Burkhard Gölling , Frank Haucke , Matthias Bauer , Wolfgang Nitsche , Inken Peltzer
IPC分类号： B64C15/00 , B64C29/00 , B64C23/00
CPC分类号： B64C23/005 , B64C9/16 , B64C9/38 , B64C13/18 , B64C21/04 , B64C29/0025 , Y02T50/166
摘要： An aircraft with aerofoils including a main wing and a control flap that includes an adjustment flap. The aircraft includes an actuator for the control flap, as well as a sensor device for acquiring the position of the control flap, an arrangement of flow-influencing devices for influencing the fluid that flows over a segment of the main wing, and flow-state sensor devices for measuring the flow state. The aircraft includes a flight control device connected to the sensor device for acquiring the position of the control flap and to the flow-state sensor devices, and connected to the actuator and flow-influencing devices for transmitting actuating commands, and a flight-state sensor device connected to the flight control device for transmitting flight states. The flight control device includes a function that selects the flow-influencing devices that are operated for optimizing local lift coefficients on the aerofoil, depending on the flight state.
摘要翻译：具有机翼的飞机包括主翼和包括调节翼片的控制翼片。飞机包括用于控制翼片的致动器，以及用于获取控制翼片的位置的传感器装置，用于影响流过主翼片段的流体的流动影响装置的布置，以及流动状态用于测量流动状态的传感器装置。飞机包括连接到传感器装置的飞行控制装置，用于获取控制翼片和流动状态传感器装置的位置，并连接到用于传送致动指令的致动器和流量影响装置，以及飞行状态传感器连接到飞行控制装置的装置用于传送飞行状态。飞行控制装置包括根据飞行状态选择用于优化机翼上的局部升力系数的流量影响装置的功能。

2. 发明授权

US08645007B2 Aircraft with an arrangement of flow-influencing devices 有权
标题翻译：具有流量影响装置布置的飞机
公开(公告)号：US08645007B2
公开(公告)日：2014-02-04
申请号：US13491629
申请日：2012-06-08
申请人： Burkhard Gölling , Rudibert King , Ulrich Notger Heinz , Wolfgang Nitsche
发明人： Burkhard Gölling , Rudibert King , Ulrich Notger Heinz , Wolfgang Nitsche
IPC分类号： B64C19/00
CPC分类号： B64C21/025 , B64C21/08 , B64C2230/02 , Y02T50/166
摘要： An aircraft, which has a respective arrangement of flow-influencing devices in at least one surface segment of each wing extending in the wingspan direction in order to influence the fluid flow over the surface segment, and of flow condition sensor devices for measuring the flow condition on the respective segment, and a flight control device, wherein the flight control device has a flow-influencing target parameter setting device connected with the arrangement of flow-influencing devices for generating target parameters for the flow-influencing devices of the at least one surface segment, wherein the flow-influencing devices are designed in such a way as to use the target parameters to change the local lift coefficients or correlations between the drag and lift coefficients in the segment where respectively located.
摘要翻译：一种飞机，其在每个机翼的至少一个表面段中具有相应的流量影响装置的布置，其在翼展方向上延伸以便影响表面段上的流体流动，以及用于测量流动状态的流动状态传感器装置在飞行控制装置上，其中所述飞行控制装置具有流量影响目标参数设定装置，该流量影响目标参数设定装置与所述流量影响装置的装置连接，用于产生所述至少一个表面的流量影响装置的目标参数其中所述流量影响装置被设计成使用所述目标参数来改变所述局部升力系数或在分别位于所述段的所述牵引系数和升力系数之间的相关性。

3. 发明申请

US20130166110A1 AIRCRAFT WITH AN ARRANGEMENT OF FLOW-INFLUENCING DEVICES 有权
标题翻译：具有流量流动装置安排的飞机
公开(公告)号：US20130166110A1
公开(公告)日：2013-06-27
申请号：US13491629
申请日：2012-06-08
申请人： Burkhard Gölling , Rudibert KING , Ulrich Notger HEINZ , Wolfgang NITSCHE
发明人： Burkhard Gölling , Rudibert KING , Ulrich Notger HEINZ , Wolfgang NITSCHE
IPC分类号： B64C19/00
CPC分类号： B64C21/025 , B64C21/08 , B64C2230/02 , Y02T50/166
摘要： An aircraft, which has a respective arrangement of flow-influencing devices in at least one surface segment of each wing extending in the wingspan direction in order to influence the fluid flow over the surface segment, and of flow condition sensor devices for measuring the flow condition on the respective segment, and a flight control device, wherein the flight control device has a flow-influencing target parameter setting device connected with the arrangement of flow-influencing devices for generating target parameters for the flow-influencing devices of the at least one surface segment, wherein the flow-influencing devices are designed in such a way as to use the target parameters to change the local lift coefficients or correlations between the drag and lift coefficients in the segment where respectively located.
摘要翻译：一种飞机，其在每个机翼的至少一个表面段中具有相应的流量影响装置的布置，其在翼展方向上延伸以便影响表面段上的流体流动，以及用于测量流动状态的流动状态传感器装置在飞行控制装置上，其中所述飞行控制装置具有流量影响目标参数设定装置，该流量影响目标参数设定装置与所述流量影响装置的装置连接，用于产生所述至少一个表面的流量影响装置的目标参数其中所述流量影响装置被设计成使用所述目标参数来改变所述局部升力系数或在分别位于所述段的所述牵引系数和升力系数之间的相关性。

4. 发明授权

US08844571B2 Fluid actuator for producing a pulsed outlet flow in the flow around an aerodynamic body, and discharge device and aerodynamic body equipped therewith 有权
标题翻译：用于在空气动力体周围的流中产生脉冲出口流的流体致动器，以及装备有排气装置和空气动力体的流体致动器
公开(公告)号：US08844571B2
公开(公告)日：2014-09-30
申请号：US13355544
申请日：2012-01-22
申请人： Burkhard Gölling , Matthias Bauer
发明人： Burkhard Gölling , Matthias Bauer
IPC分类号： F15C1/22 , B64C21/02 , F15D1/12
CPC分类号： F15C1/22 , B64C21/025 , B64C2230/18 , F15D1/12 , Y02T50/166 , Y10T137/206 , Y10T137/218 , Y10T137/2229 , Y10T137/2245 , Y10T137/7761
摘要： A fluid actuator for influencing the flow along a flow surface by ejecting a fluid flowing through the fluid actuator is described. The fluid actuator has at least two outlet lines with outlet openings at the respective ends thereof, and a feed line connected to the outlet lines for feeding fluid at a supply pressure, a flow direction diverting device into which the feed line opens and out of which the outlet lines open, and an adjusting device coupled to the flow direction diverting device to control the latter. The adjusting device is configured so the fluid is conducted successively in a cyclic sequence into each of the outlet lines. A discharge device for discharging a fluid out of a flow body, and a flow body having a multiplicity of discharge openings and a discharge device of said type are also described.
摘要翻译：描述了通过喷射流过流体致动器的流体来影响沿着流动表面的流动的流体致动器。流体致动器具有至少两个在其相应端部处具有出口开口的出口管线，以及连接到出口管线的供给管线，用于在供给压力下供给流体，流动方向转向装置，供给管路打开并流入其中出口管线打开，以及联接到流动方向转向装置以控制后者的调节装置。调整装置被配置为使得流体以循环的顺序连续进入每个出口管线。还描述了用于将流体从流体排出的排出装置和具有多个排放口的流动体和所述类型的排出装置。

5. 发明授权

US09045224B2 High lift system for an aircraft 有权
标题翻译：飞机高升程系统
公开(公告)号：US09045224B2
公开(公告)日：2015-06-02
申请号：US13530151
申请日：2012-06-22
申请人： Burkhard Gölling , Thomas Lorkowski
发明人： Burkhard Gölling , Thomas Lorkowski
IPC分类号： B64C3/00 , B64C21/04 , B64C9/16 , B64C9/38
CPC分类号： B64C21/04 , B64C9/16 , B64C9/38 , Y02T50/166 , Y02T50/44
摘要： A high lift system with a main wing and regulating flaps, also bearing devices for the mounting of the regulating flaps, and positioning devices for the positioning of the regulating flaps, wherein the respective bearing device and/or positioning device is 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 one inlet duct with at least one inlet, which device is located on or underneath the lower face of the high lift system, wherein at least one outlet duct for air is furthermore provided, which is connected with the inlet duct in a fluid-communicating manner, and has at least one outlet, which is located on the upper face in the region of at least one regulating flap of the high lift system.
摘要翻译：具有主翼和调节翼片的高升力系统，用于安装调节翼片的轴承装置和用于定位调节翼片的定位装置，其中相应的轴承装置和/或定位装置至少部分地设置有整流罩，具有流量控制装置，用于通过具有至少一个入口的至少一个入口管道控制高升程系统周围的流动，该装置位于高升力系统的下表面上或下方，其中至少还提供了一个用于空气的出口管道，其以流体连通的方式与入口管道连接，并且具有至少一个出口，其位于高升力的至少一个调节翼片的区域中的上表面上系统。

6. 发明申请

US20130062473A1 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
标题翻译：在流动体的流动表面部分中通过多个开口进入和/或吹扫流体的流动体和方法
公开(公告)号：US20130062473A1
公开(公告)日：2013-03-14
申请号：US13606835
申请日：2012-09-07
申请人： Burkhard Gölling , Erik Wassen , Tobias Hoell , Frank Thiele
发明人： Burkhard Gölling , Erik Wassen , Tobias Hoell , Frank Thiele
IPC分类号： B64C21/04 , B64C21/00 , B64C21/06
CPC分类号： B64C21/025 , B64C2230/06 , Y02T50/166
摘要： The invention pertains to a flow body with 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, as well as to a method for 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.
摘要翻译：本发明涉及一种具有流动面部分的流动体，该流体表面部分沿着流动体翼展方向和流动体弦方向延伸，并且具有引导到流动表面部分并在其中分别形成开口的多条流体管线，以及涉及一种通过至少一条通向流体的流动表面部分并分别在其中形成开口的流体管线吸入和/或吹出流体的方法。

7. 发明申请

US20130037658A1 AIRCRAFT WITH A CONTROL DEVICE 有权
标题翻译：具有控制装置的飞机
公开(公告)号：US20130037658A1
公开(公告)日：2013-02-14
申请号：US13566721
申请日：2012-08-03
申请人： Burkhard Gölling
发明人： Burkhard Gölling
IPC分类号： B64C3/50 , B64C13/04 , B64C13/38 , B64C9/00 , B64C13/26
CPC分类号： B64C13/50 , B64C21/04 , B64C21/08 , Y02T50/166
摘要： An aircraft with airfoils having a main wing and at least one control flap arranged such to be adjusted relative to the main wing, as well as a high-lift system with at least one regulating flap for adjusting the lift of the airfoils to adjust the state of lift of the aircraft, featuring flow control devices for influencing the fluid flowing over the surface segment; an activating unit; and a lift state specification device connected to the activating unit for adjusting the state of lift of the aircraft.
摘要翻译：具有翼型件的飞机具有主翼和至少一个控制翼片，其布置成相对于主翼片调节，以及具有至少一个调节翼片的高升力系统，用于调节翼型件的升力以调节状态具有用于影响流过表面段的流体的流量控制装置; 激活单元; 以及升降器状态指定装置，其连接到所述启动单元，用于调节所述飞行器的升力状态。

8. 发明申请

US20130009015A1 HIGH-LIFT SYSTEM FOR AN AIRCRAFT 有权
标题翻译：飞机高架系统
公开(公告)号：US20130009015A1
公开(公告)日：2013-01-10
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。

9. 发明授权

US09573678B2 Aircraft with a control device 有权
标题翻译：具有控制装置的飞机
公开(公告)号：US09573678B2
公开(公告)日：2017-02-21
申请号：US13566721
申请日：2012-08-03
申请人： Burkhard Gölling
发明人： Burkhard Gölling
IPC分类号： B64C21/08 , B64C13/50 , B64C21/04
CPC分类号： B64C13/50 , B64C21/04 , B64C21/08 , Y02T50/166
摘要： An aircraft with airfoils having a main wing and at least one control flap arranged such to be adjusted relative to the main wing, as well as a high-lift system with at least one regulating flap for adjusting the lift of the airfoils to adjust the state of lift of the aircraft, featuring flow control devices for influencing the fluid flowing over the surface segment; an activating unit; and a lift state specification device connected to the activating unit for adjusting the state of lift of the aircraft.
摘要翻译：具有翼型件的飞机具有主翼和至少一个控制翼片，其布置成相对于主翼片调节，以及具有至少一个调节翼片的高升力系统，用于调节翼型件的升力以调节状态具有用于影响流过表面段的流体的流量控制装置; 激活单元; 以及升降器状态指定装置，其连接到所述启动单元，用于调节所述飞行器的升力状态。

10. 发明申请

US20130026300A1 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：US20130026300A1
公开(公告)日：2013-01-31
申请号：US13530151
申请日：2012-06-22
申请人： Burkhard Gölling , Thomas LORKOWSKI
发明人： Burkhard Gölling , Thomas LORKOWSKI
IPC分类号： B64C21/08 , B64C9/18
CPC分类号： B64C21/04 , B64C9/16 , B64C9/38 , Y02T50/166 , Y02T50/44
摘要： A high lift system with a main wing and regulating flaps, also bearing devices for the mounting of the regulating flaps, and positioning devices for the positioning of the regulating flaps, wherein the respective bearing device and/or positioning device is 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 one inlet duct with at least one inlet, which device is located on or underneath the lower face of the high lift system, wherein at least one outlet duct for air is furthermore provided, which is connected with the inlet duct in a fluid-communicating manner, and has at least one outlet, which is located on the upper face in the region of at least one regulating flap of the high lift system.
摘要翻译：具有主翼和调节翼片的高升力系统，用于安装调节翼片的轴承装置和用于定位调节翼片的定位装置，其中相应的轴承装置和/或定位装置至少部分地设置有整流罩，具有流量控制装置，用于通过具有至少一个入口的至少一个入口管道控制高升程系统周围的流动，该装置位于高升力系统的下表面上或下方，其中至少还提供了一个用于空气的出口管道，其以流体连通的方式与入口管道连接，并且具有至少一个出口，其位于高升力的至少一个调节翼片的区域中的上表面上系统。

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