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1. 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。

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。

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