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1. 发明申请

US20130035808A1 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：US20130035808A1
公开(公告)日：2013-02-07
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： B64C13/16 , B64C9/00 , B64C21/00 , B64C13/24
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 optimising 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。

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