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1. 发明授权

US09868517B2 Rotatable wing tip joint and method of making same 有权
公开(公告)号：US09868517B2
公开(公告)日：2018-01-16
申请号：US14458337
申请日：2014-08-13
申请人： The Boeing Company
发明人： Timothy James McMahon , John Scott Kruse , Adam L. Kehrer
IPC分类号： B64C23/06 , B64C5/08 , B64C3/38
CPC分类号： B64C23/065 , B64C3/38 , B64C5/08 , B64C23/072 , Y02T50/162 , Y02T50/164
摘要： A joint for coupling a wing tip to a wing base includes a linking member that extends from a first end to a second end. The linking member first end is coupleable to the wing base, and the linking member second end is coupleable to the wing tip. The linking member may be curved and may extend for a fixed distance between the wing tip and the wing base. The linking member defines first second hinge lines that are substantially parallel. The joint also includes at least two actuators. A first end of each actuator is coupled to the linking member, and a second end of each actuator is coupleable to one of the wing base and the wing tip. The actuators are operable to rotate the wing tip about the first and second hinge lines between a first orientation and a second orientation relative to the wing base.

2. 发明授权

US10759521B2 Rotatable wing tip joint and method of making same 有权
公开(公告)号：US10759521B2
公开(公告)日：2020-09-01
申请号：US15675954
申请日：2017-08-14
申请人： The Boeing Company
发明人： Timothy James McMahon , John Scott Kruse , Adam L. Kehrer
IPC分类号： B64C23/06 , B64C5/08 , B64C3/38
摘要： A joint for coupling a wing tip to a wing base includes a linking member that extends from a first end to a second end. The linking member first end is coupleable to the wing base, and the linking member second end is coupleable to the wing tip. The linking member defines first second hinge lines that are substantially parallel. The joint also includes at least one actuator. A first end of each at least one actuator is coupled to the linking member, and a second end of each at least one actuator is coupleable to one of the wing base and the wing tip. The at least one actuator is operable to rotate the wing tip about the first and second hinge lines between a first orientation and a second orientation relative to the wing base.

3. 发明申请

US20160020512A1 AERIAL VEHICLE RADOME ASSEMBLY AND METHODS FOR ASSEMBLING THE SAME 有权
标题翻译：空中车载雷达组件及其组装方法
公开(公告)号：US20160020512A1
公开(公告)日：2016-01-21
申请号：US14336866
申请日：2014-07-21
申请人： The Boeing Company
发明人： Thomas Richardson Pinney , John C. Waldrop, III , John Scott Kruse
IPC分类号： H01Q1/42 , H01Q1/28
CPC分类号： H01Q1/42 , H01Q1/281
摘要： An aerial vehicle includes at least one antenna configured to at least one of transmit and receive a signal and a radome assembly at least partially covering the antenna. The radome assembly includes a shell having an inner surface that defines an opening therein and a tip comprising an extension portion coupled to the shell. The radome assembly also includes a component that engages a portion of the extension portion such that the extension portion is impeded from exiting the opening.
摘要翻译：航空器包括至少一个天线，其被配置为至少部分地覆盖天线的发射和接收信号中的至少一个以及天线罩组件。天线罩组件包括壳体，壳体具有在其中限定开口的内表面，并且尖端包括连接到壳体的延伸部分。天线罩组件还包括与延伸部分的一部分接合的部件，使得延伸部分阻止离开开口。

4. 发明申请

US20170361922A1 ROTATABLE WING TIP JOINT AND METHOD OF MAKING SAME 审中-公开
公开(公告)号：US20170361922A1
公开(公告)日：2017-12-21
申请号：US15675954
申请日：2017-08-14
申请人： The Boeing Company
发明人： Timothy James McMahon , John Scott Kruse , Adam L. Kehrer
IPC分类号： B64C23/06 , B64C3/38 , B64C5/08
CPC分类号： B64C23/065 , B64C3/38 , B64C5/08 , B64C23/072 , Y02T50/162 , Y02T50/164
摘要： A joint for coupling a wing tip to a wing base includes a linking member that extends from a first end to a second end. The linking member first end is coupleable to the wing base, and the linking member second end is coupleable to the wing tip. The linking member defines first second hinge lines that are substantially parallel. The joint also includes at least one actuator. A first end of each at least one actuator is coupled to the linking member, and a second end of each at least one actuator is coupleable to one of the wing base and the wing tip. The at least one actuator is operable to rotate the wing tip about the first and second hinge lines between a first orientation and a second orientation relative to the wing base.

5. 发明授权

US09711845B2 Aerial vehicle radome assembly and methods for assembling the same 有权
公开(公告)号：US09711845B2
公开(公告)日：2017-07-18
申请号：US14336866
申请日：2014-07-21
申请人： The Boeing Company
发明人： Thomas Richardson Pinney , John C. Waldrop, III , John Scott Kruse
IPC分类号： H01Q1/42 , H01Q1/28
CPC分类号： H01Q1/42 , H01Q1/281
摘要： An aerial vehicle includes at least one antenna configured to at least one of transmit and receive a signal and a radome assembly at least partially covering the antenna. The radome assembly includes a shell having an inner surface that defines an opening therein and a tip comprising an extension portion coupled to the shell. The radome assembly also includes a component that engages a portion of the extension portion such that the extension portion is impeded from exiting the opening.

6. 发明申请

US20160244153A1 ROTATABLE WING TIP JOINT AND METHOD OF MAKING SAME 有权
标题翻译： ROTATABLE WING TIP JOINT及其制作方法
公开(公告)号：US20160244153A1
公开(公告)日：2016-08-25
申请号：US14458337
申请日：2014-08-13
申请人： The Boeing Company
发明人： Timothy James McMahon , John Scott Kruse , Adam L. Kehrer
IPC分类号： B64C23/06 , B64C3/38 , B64C5/08
CPC分类号： B64C23/065 , B64C3/38 , B64C5/08 , B64C23/072 , Y02T50/162 , Y02T50/164
摘要： A joint for coupling a wing tip to a wing base includes a linking member that extends from a first end to a second end. The linking member first end is coupleable to the wing base, and the linking member second end is coupleable to the wing tip. The linking member defines first second hinge lines that are substantially parallel. The joint also includes at least one actuator. A first end of each at least one actuator is coupled to the linking member, and a second end of each at least one actuator is coupleable to one of the wing base and the wing tip. The at least one actuator is operable to rotate the wing tip about the first and second hinge lines between a first orientation and a second orientation relative to the wing base.
摘要翻译：用于将翼尖连接到翼基部的接头包括从第一端延伸到第二端的连接构件。连接构件第一端部可与翼基座连接，并且连接构件第二端部可与翼尖连接。连接构件限定基本上平行的第一第二铰链线。接头还包括至少一个致动器。每个至少一个致动器的第一端联接到连接构件，并且每个至少一个致动器的第二端可连接到翼基座和翼尖之一。所述至少一个致动器可操作以相对于所述机翼基座在第一方向和第二方向之间围绕所述第一和第二铰链线旋转所述翼尖。

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