公开(公告)号：WO2008105850A3

公开(公告)日：2008-12-24

申请号：PCT/US2007021852

申请日：2007-10-12

Applicant: BOEING CO ,  BANKS DAVID P ,  ZENKNER GRANT C ,  MCCOWIN PETER D ,  JONES DARRELL D

Inventor： BANKS DAVID P ,  ZENKNER GRANT C ,  MCCOWIN PETER D ,  JONES DARRELL D

IPC: B29C70/38 ,  B29C70/54

CPC classification number: B29C70/386 ,  B29C70/545 ,  B29L2031/3082 ,  B29L2031/3085 ,  Y10T156/1054 ,  Y10T156/1064 ,  Y10T156/1075 ,  Y10T156/108 ,  Y10T156/1082 ,  Y10T156/1098 ,  Y10T156/12 ,  Y10T156/125 ,  Y10T156/13 ,  Y10T156/1322 ,  Y10T156/1348 ,  Y10T156/17

Abstract: Disclosed is a method and apparatus (10) for manufacturing multiple layer composite structures and structures containing components made of multiple layer composite structures, comprising dispensing (5) layers of composite material, trimming (3) each layer to its final shape as it is being dispensed, and positioning it properly with respect to prior layers in the part lay-up.

Abstract translation: 公开了一种用于制造包含由多层复合结构制成的组分的多层复合结构和结构的方法和装置（10），包括分配（5）复合材料层，将（3）每层修剪成其最终形状，因为它是 分配，并相对于零件叠层中的现有层适当地定位。

公开(公告)号：WO2007053156A2

公开(公告)日：2007-05-10

申请号：PCT/US2005042472

申请日：2005-11-22

Applicant: BOEING CO ,  SPISHAK NOEL A ,  WAGNER DAVID L ,  JONES DARRELL D ,  LUM MATTHEW K ,  OLSON VINCENT T ,  APPLETON JOSEPH A ,  HALL THOMAS D

Inventor： SPISHAK NOEL A ,  WAGNER DAVID L ,  JONES DARRELL D ,  LUM MATTHEW K ,  OLSON VINCENT T ,  APPLETON JOSEPH A ,  HALL THOMAS D

CPC classification number: B25B5/14 ,  B64F5/10 ,  Y10T29/49622 ,  Y10T29/49904 ,  Y10T29/49998 ,  Y10T29/53978

Abstract: A one-piece barrel assembly cart includes a right assembly cart base connected with a left assembly cart base and at least three stabilizer rings that are attached to the assembly cart base. The one-piece barrel assembly cart may be used to stabilize a tapered cured composite barrel, for example the large fuselage barrel of the aft section of a large new generation aircraft, such as a 7E7 Boeing airplane. A modular assembly cart includes at least two identical modules. Each of these modules includes a cart base and a stabilizer ring. The diameter of the inner surface of the stabilizer ring may vary as needed. Other modules including a fuselage support may be added. By providing modular assembly carts any shape and size of a one-piece composite barrel may be stabilized after curing of the composite material.

Abstract translation: 单件式桶组装车包括与左组件车基座连接的右组件车基座和附接到组装车基座的至少三个稳定环。 单件式桶组装车可以用于稳定锥形固化复合材料筒，例如大型新一代飞机（例如7E7波音飞机）后部的大型机身筒。 模块化组装车包括至少两个相同的模块。 这些模块中的每一个包括推车基座和稳定环。 稳定环的内表面的直径可根据需要而变化。 可以添加包括机身支持的其他模块。 通过提供模块化的组装车，在复合材料固化之后，单件复合筒的任何形状和尺寸可以被稳定。

公开(公告)号：WO2006113048A2

公开(公告)日：2006-10-26

申请号：PCT/US2006/010825

申请日：2006-03-24

Applicant: THE BOEING COMPANY ,  WILLDEN, Kurtis S ,  LEE, Michael A ,  EVANS, Richard B ,  JONES, Darrell D.

Inventor： WILLDEN, Kurtis S ,  LEE, Michael A ,  EVANS, Richard B ,  JONES, Darrell D.

IPC: B29C70/46

CPC classification number: B29C33/307 ,  B29C33/308 ,  B29C70/462 ,  B29L2031/003 ,  B29L2031/008

Abstract: A method and associated apparatus for forming a composite structural member from a charge are provided. The charge can be disposed on a first die of the apparatus and formed to a desired configuration defined by a recess of the die by inserting a second die or a tool into the recess. In some cases, the first die can include two portions that are adjustable in a transverse direction so that the recess can be opened by the insertion of the second die or tool. The second die or tool can be a substantially rigid member or an inflatable bladder. In either case, the charge can be disposed on the first die, formed, and then further processed on the first die, thereby facilitating indexing of the charge for each operation.

Abstract translation: 提供了一种用于从电荷形成复合结构构件的方法和相关联的装置。 电荷可以设置在设备的第一裸片上，并且通过将第二模具或工具插入凹槽中而形成为由凹模的凹槽限定的期望构型。 在一些情况下，第一模具可以包括在横向方向上可调节的两个部分，使得可以通过插入第二模具或工具来打开凹部。 第二模具或工具可以是基本上刚性的构件或可充气囊。 在任一种情况下，电荷可以设置在第一裸片上，形成，然后在第一裸片上进一步处理，从而便于每个操作的电荷分度。