公开(公告)号：WO2007053156A3

公开(公告)日：2007-05-10

申请号：PCT/US2005/042472

申请日：2005-11-22

Applicant: THE BOEING COMPANY ,  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.

IPC: B64F5/00

Abstract: A one-piece barrel assembly cart (10) includes a right assembly cart base (210) connected with a left assembly cart base (220) and at least three stabilizer rings (17, 18, 19) that are attached to the assembly cart base. The one-piece barrel assembly cart may be used to stabilize a tapered cured composite barrel (31), 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 (40) includes at least two identical modules (41). Each of these modules includes a cart base (42) and a stabilizer ring (43). 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.

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：WO2006137994A1

公开(公告)日：2006-12-28

申请号：PCT/US2006/017573

申请日：2006-05-05

Applicant: THE BOEING COMPANY ,  SPISHAK, Noel, A. ,  NELSON, Paul, E. ,  HAGMAN, Thomas, J. ,  SCHWINDT, Jeffrey, D. ,  MASTERS, Matthew, J. ,  SANDERS, Michael, G. ,  MERKLEY, Alan, R. ,  REID, Eric, M. ,  MURPHY, James, C.

Inventor： SPISHAK, Noel, A. ,  NELSON, Paul, E. ,  HAGMAN, Thomas, J. ,  SCHWINDT, Jeffrey, D. ,  MASTERS, Matthew, J. ,  SANDERS, Michael, G. ,  MERKLEY, Alan, R. ,  REID, Eric, M. ,  MURPHY, James, C.

IPC: B64F5/00

CPC classification number: B64F5/10 ,  Y10S269/909 ,  Y10T29/49622 ,  Y10T29/49826 ,  Y10T29/49899 ,  Y10T29/49998 ,  Y10T29/53974

Abstract: A rotating internal support (10) for a large hollow structure (18) can include a rigid central truss (12) and two or more annular disks (14) coupled to the truss by support arms (16). The annular disks (14) can be axially spaced along the longitudinal centerlme of the truss (12), and can be coupled to the support arms (16) by guide rollers (20) that allow the annular disks (14) to rotate about a central axis. The internal support (10) can also include support rods (80) with contact pads (82) that extend axially around the annular disks (14) to contact and support the inner surface of the large hollow structure (18) .

Abstract translation: 用于大型中空结构（18）的旋转内部支撑件（10）可以包括刚性中心桁架（12）和通过支撑臂（16）联接到桁架的两个或更多个环形盘（14）。 环形盘（14）可以沿着桁架（12）的纵向中心轴向间隔开，并且可以通过导辊（20）联接到支撑臂（16），引导辊（20）允许环形盘（14）围绕 中心轴。 内部支撑件（10）还可以包括具有接触垫（82）的支撑杆（80），其具有围绕环形盘（14）轴向延伸以接触和支撑大型中空结构（18）的内表面。