公开(公告)号：US06808143B2

公开(公告)日：2004-10-26

申请号：US10001536

申请日：2001-11-13

申请人： Clayton L. Munk ,  Paul E. Nelson ,  David E. Strand

发明人： Clayton L. Munk ,  Paul E. Nelson ,  David E. Strand

IPC分类号： B64C326

CPC分类号： G05B19/44 ,  B23P21/00 ,  B23P2700/01 ,  B25B5/122 ,  B25B5/163 ,  B25B11/005 ,  B25B11/007 ,  B64C3/18 ,  B64C3/26 ,  B64F5/10 ,  G05B19/401 ,  G05B19/4083 ,  G05B2219/36503 ,  G05B2219/49136 ,  Y02P90/265 ,  Y10T29/49764 ,  Y10T29/49885 ,  Y10T29/49895 ,  Y10T29/49904

摘要： A method and apparatus for manufacturing wings includes a fixture that holds wing panels for drilling and edge trimming by accurate numerically controlled machine tools using original numerical part definition records, utilizing spatial relationships between key features of detail parts or subassemblies as represented by coordination features machined into the parts and subassemblies, thereby making the parts and subassemblies intrinsically determinant of the dimensions and contour of the wing. Spars are attached to the wing panel using the coordination holes to locate the spars accurately on the panel in accordance with the original engineering design, and in-spar ribs are attached to rib posts on the spar using accurately drilled coordination holes in the ends of the rib and in the rib post. The wing contour is determined by the configuration of the spars and ribs rather than by any conventional hard tooling which determines the wing contour in conventional processes.

摘要翻译： 用于制造机翼的方法和装置包括一个固定装置，其通过使用原始数字部分定义记录的精确的数控机床来保持用于钻孔和边缘修剪的翼板，利用细节部件或子组件的关键特征之间的空间关系，由协调特征加工成 部件和组件，从而使部件和组件固有地决定了机翼的尺寸和轮廓。 翼片使用协调孔连接到翼板上，以根据原始工程设计将翼梁准确地定位在面板上，并且翼梁用肋板上的肋柱连接，使用准确钻孔的协调孔 肋骨和肋骨柱。 机翼轮廓由翼梁和肋骨的结构决定，而不是通过任何常规的硬工具来确定传统工艺中的机翼轮廓。

公开(公告)号：US06830218B2

公开(公告)日：2004-12-14

申请号：US10334452

申请日：2002-12-31

申请人： Jan A. Kordel ,  Richard B. Tanner

发明人： Jan A. Kordel ,  Richard B. Tanner

IPC分类号： B64C326

CPC分类号： B64C3/26 ,  B64F5/10 ,  F16B2200/30

摘要： A method, system, and apparatus for attaching a fairing to a body or aircraft wing are disclosed. A plurality of attach anchors is disposed on the body or aircraft wing to which the fairing is to be attached. Disposed in the fairing is a plurality of core pockets that are alignable with the plurality of attach anchors, and each of the core pockets defines a channel. The fairing is placed over the body or the aircraft wing such that the heads of the attach anchors are received in the core pockets. The fairing is then slid across the body or the aircraft wing with the channels sliding along the heads of the attach anchors such that the fairing is prevented from being lifted away from the body or aircraft wing.

摘要翻译： 公开了一种用于将整流罩附接到身体或飞机机翼上的方法，系统和装置。 多个附接锚固件设置在整流罩将要连接到的主体或飞机机翼上。 布置在整流罩中的是多个可与多个连接锚固件对准的芯袋，并且每个芯袋限定通道。 整流罩放置在身体或飞机机翼上，使得附接锚的头部被容纳在芯袋中。 然后，整流罩滑过身体或飞机机翼，通道沿连接锚的头部滑动，从而防止整流罩从身体或飞机机翼上抬起。

公开(公告)号：US06328261B1

公开(公告)日：2001-12-11

申请号：US09212569

申请日：1998-12-16

申请人： Tim Wollaston ,  Richard Pedwell ,  Paul Bush

发明人： Tim Wollaston ,  Richard Pedwell ,  Paul Bush

IPC分类号： B64C326

CPC分类号： B23K20/122 ,  B23K20/123 ,  B23K20/129

摘要： A method of forming a structural airframe component for an aircraft and an airframe structural component The method includes placing at least two components (1,2) in abutting relationship with each other and joining them together by friction stir butt welding (3), and the structural airframe component comprises a component manufactured according to the method of the invention.

摘要翻译： 一种形成用于飞行器和机身结构部件的结构性机身部件的方法该方法包括将至少两个彼此邻接的部件（1,2）彼此放置并通过摩擦搅拌对接焊接（3）将它们连接在一起，并且 结构机身部件包括根据本发明的方法制造的部件。