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1. 发明授权

US10538307B2 Hinged raked wing tip 有权
公开(公告)号：US10538307B2
公开(公告)日：2020-01-21
申请号：US13664416
申请日：2012-10-30
申请人： The Boeing Company
发明人： Paul W. Dees , Mark S. Good , Seiya Sakurai , Jan A. Kordel , Stephen J. Fox , Matthew A. Lassen , Bruce Robert Fox , Steven Paul Walker , Gregory M. Santini
IPC分类号： B64C3/56 , B64C3/58
摘要： A wing assembly comprises a raked wing tip having an outboard portion hinged to one of a main wing having at least one moveable control surface and an inboard raked wing tip portion. The outboard portion of the raked wing tip does not carry any moveable flight control surfaces.

2. 发明授权

US09783284B2 Rotary drive assembly for wing tip 有权
公开(公告)号：US09783284B2
公开(公告)日：2017-10-10
申请号：US14282595
申请日：2014-05-20
申请人： THE BOEING COMPANY
发明人： Keith Townsend , Stephen J. Fox
IPC分类号： B64C3/56
CPC分类号： B64C3/56 , Y10T29/49318
摘要： A rotary drive assembly is provided. The assembly includes a tip hinge box, a body hinge box pivotably coupled to the tip hinge box, a rotary actuator positioned within the body hinge box, and a linkage mechanism coupled between the rotary actuator and the tip hinge box, the linkage mechanism including a first linkage fixedly coupled to the rotary actuator, and a second linkage coupled between the first linkage and the tip hinge box, wherein rotation of the rotary actuator causes the tip hinge box to rotate relative to the body hinge box.

3. 发明授权

US09365284B2 High-positioned 2-position variable camber Krueger 有权
标题翻译：高位二位置可变角度Krueger
公开(公告)号：US09365284B2
公开(公告)日：2016-06-14
申请号：US13867562
申请日：2013-04-22
申请人： The Boeing Company
发明人： Seiya Sakurai , Stephen J. Fox , Victor H. Reyes
IPC分类号： B64C3/50 , B64C9/22 , B64C9/02
CPC分类号： B64C9/24 , B64C9/02 , B64C9/22 , B64C9/34
摘要： A variable camber Krueger flap deployment linkage mechanism is presented. A first linkage assembly couples a flap assembly and an airfoil, and comprising a first drive arm, a first drive link, and a support arm. A second linkage assembly couples the flap assembly and the first drive arm, and comprises a drive transfer arm, a middle connection segment, and a bullnose link.
摘要翻译：提出了一种可变的弧度Krueger挡板部署联动机构。第一连杆组件联接翼片组件和翼型件，并且包括第一驱动臂，第一驱动连杆和支撑臂。第二连杆组件联接翼片组件和第一驱动臂，并且包括驱动传递臂，中间连接段和长臂连杆。

4. 发明申请

US20150336657A1 ROTARY DRIVE ASSEMBLY FOR WING TIP 有权
标题翻译：旋转驱动装置
公开(公告)号：US20150336657A1
公开(公告)日：2015-11-26
申请号：US14282595
申请日：2014-05-20
申请人： THE BOEING COMPANY
发明人： Keith Townsend , Stephen J. Fox
IPC分类号： B64C3/56
CPC分类号： B64C3/56 , Y10T29/49318
摘要： A rotary drive assembly is provided. The assembly includes a tip hinge box, a body hinge box pivotably coupled to the tip hinge box, a rotary actuator positioned within the body hinge box, and a linkage mechanism coupled between the rotary actuator and the tip hinge box, the linkage mechanism including a first linkage fixedly coupled to the rotary actuator, and a second linkage coupled between the first linkage and the tip hinge box, wherein rotation of the rotary actuator causes the tip hinge box to rotate relative to the body hinge box.
摘要翻译：提供旋转驱动组件。所述组件包括尖端铰链盒，可枢转地联接到所述尖端铰链盒的主体铰链盒，位于所述主体铰链箱内的旋转致动器，以及联接在所述旋转致动器和所述顶端铰链盒之间的连杆机构，所述连杆机构包括固定地联接到所述旋转致动器的第一连杆以及联接在所述第一连杆机构和所述顶部铰链箱之间的第二连杆，其中所述旋转致动器的旋转使所述顶端铰链箱相对于所述车身铰链箱转动。

5. 发明授权

US09688386B2 High-positioned 2-position variable camber Krueger 有权
公开(公告)号：US09688386B2
公开(公告)日：2017-06-27
申请号：US15180707
申请日：2016-06-13
申请人： The Boeing Company
发明人： Seiya Sakurai , Stephen J. Fox , Victor H. Reyes
IPC分类号： B64C9/24 , B64C9/02 , B64C9/34
CPC分类号： B64C9/24 , B64C9/02 , B64C9/22 , B64C9/34
摘要： A variable camber Krueger flap deployment linkage mechanism is presented. A first linkage assembly couples a flap assembly and an airfoil, and comprising a first drive arm, a first drive link, and a support arm. A second linkage assembly couples the flap assembly and the first drive arm, and comprises a drive transfer arm, a middle connection segment, and a bullnose link.

6. 发明申请

US20160297513A1 High-Positioned 2-Postion Variable Camber Krueger 有权
标题翻译：高位2位可变弧度Krueger
公开(公告)号：US20160297513A1
公开(公告)日：2016-10-13
申请号：US15180707
申请日：2016-06-13
申请人： The Boeing Company
发明人： Seiya Sakurai , Stephen J. Fox , Victor H. Reyes
IPC分类号： B64C9/24 , B64C9/34 , B64C9/02
CPC分类号： B64C9/24 , B64C9/02 , B64C9/22 , B64C9/34
摘要： A variable camber Krueger flap deployment linkage mechanism is presented. A first linkage assembly couples a flap assembly and an airfoil, and comprising a first drive arm, a first drive link, and a support arm. A second linkage assembly couples the flap assembly and the first drive arm, and comprises a drive transfer arm, a middle connection segment, and a bullnose link.
摘要翻译：提出了一种可变的弧度Krueger挡板部署联动机构。第一连杆组件联接翼片组件和翼型件，并且包括第一驱动臂，第一驱动连杆和支撑臂。第二连杆组件联接翼片组件和第一驱动臂，并且包括驱动传递臂，中间连接段和长臂连杆。

7. 发明申请

US20140312175A1 HIGH-POSITIONED 2-POSITION VARIABLE CAMBER KRUEGER 有权
标题翻译：高位两位可变摄像机KRUEGER
公开(公告)号：US20140312175A1
公开(公告)日：2014-10-23
申请号：US13867562
申请日：2013-04-22
申请人： The Boeing Company
发明人： Seiya Sakurai , Stephen J. Fox , Victor H. Reyes
IPC分类号： B64C13/28 , B64C9/24
CPC分类号： B64C9/24 , B64C9/02 , B64C9/22 , B64C9/34
摘要： A variable camber Krueger flap deployment linkage mechanism is presented. A first linkage assembly couples a flap assembly and an airfoil, and comprising a first drive arm, a first drive link, and a support arm. A second linkage assembly couples the flap assembly and the first drive arm, and comprises a drive transfer arm, a middle connection segment, and a bullnose link.
摘要翻译：提出了一种可变的弧度Krueger挡板部署联动机构。第一连杆组件联接翼片组件和翼型件，并且包括第一驱动臂，第一驱动连杆和支撑臂。第二连杆组件联接翼片组件和第一驱动臂，并且包括驱动传递臂，中间连接段和长臂连杆。

8. 发明申请

US20130099060A1 Hinged Raked Wing Tip 审中-公开
标题翻译：铰链耙翼提示
公开(公告)号：US20130099060A1
公开(公告)日：2013-04-25
申请号：US13664416
申请日：2012-10-30
申请人： THE BOEING COMPANY
发明人： Paul W. Dees , Mark S. Good , Seiya Sakurai, , Jan A. Kordel , Stephen J. Fox , Matthew A. Lassen , Bruce Robert Fox , Steven Paul Walker , Gregory M. Santini
IPC分类号： B64C3/56 , B64C3/58
摘要： A wing assembly comprises a raked wing tip having an outboard portion hinged to one of a main wing having at least one moveable control surface and an inboard raked wing tip portion. The outboard portion of the raked wing tip does not carry any moveable flight control surfaces.
摘要翻译：翼组件包括具有外侧部分的外侧翼部，所述外侧部分铰接到具有至少一个可移动控制表面和内侧倾斜翼尖部分的主翼中的一个。倾斜翼尖的外侧部分不携带任何可移动的飞行控制表面。

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