公开(公告)号：WO2008140614A3

公开(公告)日：2009-04-23

申请号：PCT/US2007088059

申请日：2007-12-19

Applicant: BOEING CO ,  TOH CHIN H ,  HARMAN EDWARD BRUCE ,  SARH BRANKO

Inventor： TOH CHIN H ,  HARMAN EDWARD BRUCE ,  SARH BRANKO

IPC: B21J15/14

CPC classification number: B23P19/04 ,  B21J15/14 ,  B21J15/142 ,  B23P2700/01 ,  Y10T29/49616 ,  Y10T29/49895 ,  Y10T29/49947 ,  Y10T29/4995 ,  Y10T29/53 ,  Y10T29/53039 ,  Y10T29/53087 ,  Y10T29/5343

Abstract: An assembly system and method for assembling an aircraft wing box (200) or other structure that may define an interior area accessible through at least one access opening are provided. The method includes inserting a robot (250) having an assembly tool (452) mounted thereto into the interior area through the at least one access opening. The assembly tool may be positioned at a fastener location, and may be clamped to the structure. A hole may be made through the structure, and a fastener may be installed in the hole.

Abstract translation: 提供了一种用于组装飞机机翼盒（200）或可以限定通过至少一个进入开口可接近的内部区域的其他结构的组装系统和方法。 该方法包括将具有安装在其上的装配工具（452）的机器人（250）插入到通过至少一个进入开口的内部区域中。 组装工具可以定位在紧固件位置处，并且可以被夹紧到结构上。 可以通过该结构制造孔，并且紧固件可以安装在孔中。

公开(公告)号：WO2006113041A3

公开(公告)日：2007-04-05

申请号：PCT/US2006010705

申请日：2006-03-22

Applicant: BOEING CO ,  SARH BRANKO

Inventor： SARH BRANKO

IPC: B64C1/12 ,  B64C1/00

CPC classification number: B64C1/068 ,  B29C70/32 ,  B64C1/061 ,  B64C1/064 ,  B64C1/12 ,  B64C2001/0072 ,  B64C2211/00 ,  B64F5/10 ,  Y02T50/433

Abstract: An aircraft fuselage barrel (10) includes a skin (12) and a shear tie (18). The shear tie (18) resides within and is integrally formed with the skin (12). The shear tie (18) is separate from and configured for frame attachment thereon. A multi-ring system (79) for fuselage barrel formation includes a mold (68) with a ring (50). The ring (50) has width (W2) approximately equal to a separation distance (D) between two adjacent fuselage frames (22) and includes a module (52) that has a circumferential length (L1) that is greater than a circumferential distance between two fuselage longerons (14). A support structure (80) is coupled to and supports the mold (68). A method of forming the aircraft fuselage barrel (10) includes constructing the support structure (80). Rings (86) of the mold (68) are attached to and over the support structure (80). The mold (68) is constructed. Material is laid-up onto the mold (68) to integrally form the one-piece fuselage barrel (10) including a Hat-configured longeron (14).

Abstract translation: 飞机机身枪管（10）包括皮肤（12）和剪切带（18）。 剪切带（18）位于皮肤（12）内并与皮肤（12）一体形成。 剪切带（18）与其上的框架附接分离并构造成用于框架附接。 用于机身桶形成的多环系统（79）包括具有环（50）的模具（68）。 环（50）具有大致等于两个相邻的机身框架（22）之间的间隔距离（D）的宽度（W2），并且包括具有大于圆周长度（L1）的周向长度（L1）的模块（52） 两个机身长度（14）。 支撑结构（80）联接到并支撑模具（68）。 形成飞行器机身筒（10）的方法包括构造支撑结构（80）。 模具（68）的环（86）附接到支撑结构（80）上和上方。 构造模具（68）。 将材料放置在模具（68）上以整体形成包括帽构造的龙门（14）的单件机身筒体（10）。

公开(公告)号：WO2012012034A3

公开(公告)日：2012-05-24

申请号：PCT/US2011040033

申请日：2011-06-10

Applicant: BOEING CO ,  SARH BRANKO ,  AMIREHTESHAMI DAVID HASSAN

Inventor： SARH BRANKO ,  AMIREHTESHAMI DAVID HASSAN

IPC: B62D57/024 ,  B64F5/00

CPC classification number: B23Q9/02 ,  B23Q9/0007 ,  B23Q9/0042 ,  B62D57/024 ,  B64F5/10 ,  Y10T29/49 ,  Y10T29/49622 ,  Y10T29/49826 ,  Y10T29/49828 ,  Y10T29/5146 ,  Y10T29/5173 ,  Y10T29/53961 ,  Y10T29/53991 ,  Y10T29/54 ,  Y10T408/554

Abstract: A method and apparatus for performing operations on a workpiece. A first frame in a frame system may be held on the workpiece by applying a vacuum to the first frame. A second frame in the frame system may be detached from the workpiece by applying a pressure to the second frame. The second frame may be moved to a location on the workpiece. The second frame may be attached to the workpiece by applying the vacuum to the second frame. An operation may be performed on the workpiece.

Abstract translation: 一种用于对工件进行操作的方法和装置。 框架系统中的第一框架可以通过向第一框架施加真空而保持在工件上。 框架系统中的第二框架可以通过向第二框架施加压力而与工件分离。 第二框架可以移动到工件上的位置。 第二框架可以通过将真空施加到第二框架而附接到工件。 可以对工件进行操作。

公开(公告)号：WO2005110842A3

公开(公告)日：2006-02-16

申请号：PCT/US2005014329

申请日：2005-04-26

Applicant: BOEING CO ,  SARH BRANKO

Inventor： SARH BRANKO

IPC: B64C1/00 ,  B64C3/00 ,  B64F5/00

CPC classification number: B64C3/18 ,  B64C3/00 ,  B64F5/10

Abstract: An airfoil box and associated method are provided. The airfoil box (10) includes two or more half-shell structures (30, 50). Each half-shell structure (30, 50) is an integral or unitary member that includes at least a portion of the outer skin (16) of the airfoil as well as stiffener members (34, 54) and connection members (38, 58). For example, the half-shell structures (30, 50) can be integrally formed of composite materials. The half-shell structures (30, 50) can be assembled by connecting the connection members (38, 58) with fasteners (70) such as rivets to form the airfoil box (10).

Abstract translation: 提供了一种翼型箱和相关方法。 翼型箱（10）包括两个或更多个半壳结构（30,50）。 每个半壳结构（30,50）是包括翼型件的外皮（16）的至少一部分以及加强件（34,54）和连接构件（38,58）的整体或整体构件， 。 例如，半壳结构（30,50）可以由复合材料一体形成。 半壳结构（30,50）可以通过将连接构件（38,58）与诸如铆钉之类的紧固件（70）连接而形成翼型箱（10）来组装。