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2. 发明授权

EP0917920B2 Lap splice mini-riveter system and method for using the system 有权
标题翻译：系统和方法铆接
公开(公告)号：EP0917920B2
公开(公告)日：2008-10-22
申请号：EP98203998.4
申请日：1998-11-26
申请人： The Boeing Company
发明人： Banks, David Paul , Buttrick, James N., Jr. , Glaisyer, Charles H. , Jones, Darrell D. , McCrum, Russell C. , Wright, Philip M.
IPC分类号： B21J15/10 , B23Q9/00
CPC分类号： B23Q9/0007 , B21J15/10 , B21J15/142 , B21J15/28 , B23Q9/0042 , B64F5/10 , Y02P70/585

3. 发明公开

EP1671745A1 Manufacturing system for aircraft structures and other large structures 有权
标题翻译：对飞机部件和其他大型结构的生产体系
公开(公告)号：EP1671745A1
公开(公告)日：2006-06-21
申请号：EP06075472.8
申请日：2002-10-28
申请人： The Boeing Company
发明人： Hazelhurst, Laurence N. , Philpott, Bobby C. Jr. , Buttrick, James N. , Jones, Darrel D. , Papanikolaou, Kostandinos D. , Banks, David P. , Rowe, Terrence J. , Outous, Ronald W. , Glaisyer, Charles H. , Townsend, Harry E. , Boberg, Mark C. , Nelson, Paul E. , Porter, John R.
IPC分类号： B23Q9/00 , B23Q16/00 , B64F5/00
CPC分类号： B23Q17/2233 , B21C51/005 , B21J15/14 , B21J15/142 , B21J15/28 , B23Q9/0042 , B23Q16/00 , B23Q16/001 , B64F5/10 , B64F5/50 , Y10T29/49778 , Y10T29/4978 , Y10T29/49829 , Y10T29/49895 , Y10T29/49943 , Y10T29/49948 , Y10T29/49956 , Y10T29/5118 , Y10T29/5191 , Y10T29/53052 , Y10T29/53061 , Y10T29/53087 , Y10T29/534 , Y10T29/53961 , Y10T29/53978 , Y10T408/03 , Y10T408/173 , Y10T408/175 , Y10T408/21 , Y10T408/5612 , Y10T408/56245 , Y10T408/567 , Y10T408/57 , Y10T408/93 , Y10T409/306384 , Y10T409/307672 , Y10T409/308176 , Y10T483/10 , Y10T483/1729 , Y10T483/1736 , Y10T483/1748 , Y10T483/1752
摘要： A production system for manufacturing a workpiece comprises an index system including a plurality of index devices removably mounted on the workpiece at known longitudinally spaced locations therealong, and a longitudinally extending index member releasably engaged with at least two of the index devices such that a position and orientation of the index are fixed relative to the workpiece by the index devices, the index member having position-indicating features distributed therealong. The production system further comprises a machine module mounted for longitudinal movement along the index member and operable to perform an operation, the machine module being operable to detect the position-indicating features on the index member and thereby determine a position of the machine module relative to the workpiece.

5. 发明授权

EP0917920B1 Lap splice mini-riveter system and method for using the system 有权
标题翻译：系统和方法铆接
公开(公告)号：EP0917920B1
公开(公告)日：2005-03-09
申请号：EP98203998.4
申请日：1998-11-26
申请人： THE BOEING COMPANY
发明人： Banks, David Paul , Buttrick, James N., Jr. , Glaisyer, Charles H. , Jones, Darrell D. , McCrum, Russell C. , Wright, Philip M.
IPC分类号： B21J15/10 , B23Q9/00
CPC分类号： B23Q9/0007 , B21J15/10 , B21J15/142 , B21J15/28 , B23Q9/0042 , B64F5/10 , Y02P70/585

6. 发明公开

EP0917920A3 Lap splice mini-riveter system and method for using the system 有权
标题翻译：系统和Verfahren zum Nieten
公开(公告)号：EP0917920A3
公开(公告)日：2000-04-26
申请号：EP98203998.4
申请日：1998-11-26
申请人： THE BOEING COMPANY
发明人： Banks, David Paul , Buttrick, James N., Jr. , Glaisyer, Charles H. , Jones, Darell D. , McCrum, Russell C. , Wright, Philip M.
IPC分类号： B21J15/10 , B23Q9/00
CPC分类号： B23Q9/0007 , B21J15/10 , B21J15/142 , B21J15/28 , B23Q9/0042 , B64F5/10 , Y02P70/585
摘要： The present invention relates to a portable process for automated fastening of aircraft structures. The invention will employ two primary elements for locating and installing through-the-skin fasteners. Inside and outside units are attached onto an airframe and indexed to each other through coordination holes that have been pre-drilled through the structure. The aircraft structure is assembled with the pre-drilled coordination holes by aligning adjacent airframe parts and inserting alignment pins. The alignment pins will provide a degree of clamping to pull the parts together and provide indexing for inside and outside vacuum attachment track systems. The invention is equipped to traverse along the track system, accurately position itself, and drill only or countersink a hole, insert a fastener, and fasten, i.e., upset a rivet, or run down a threaded nut, then reposition itself to the next fastener location and repeat the process.
摘要翻译：本发明涉及用于飞机结构的自动紧固的便携式方法。本发明将采用两个主要元件来定位和安装通过皮肤的紧固件。内部和外部单元通过已经通过结构预钻孔的协调孔而附接到机身上并彼此分离。飞机结构通过对准相邻的机身部件并插入对准销，与预钻孔的协调孔组装。定位销将提供一定程度的夹紧力，将零件拉到一起，并为内部和外部真空附件履带系统提供分度。本发明被设置为沿轨道系统横向移动，精确地定位自身，仅钻孔或锪孔，插入紧固件，并固定，即压住铆钉，或者沿着螺纹螺母倒下，然后将其自身重新定位到下一个紧固件位置并重复该过程。

7. 发明公开

EP0917920A2 Lap splice mini-riveter system and method for using the system 有权
标题翻译：系统和方法铆接
公开(公告)号：EP0917920A2
公开(公告)日：1999-05-26
申请号：EP98203998.4
申请日：1998-11-26
申请人： THE BOEING COMPANY
发明人： Banks, David Paul , Buttrick, James N., Jr. , Glaisyer, Charles H. , Jones, Darell D. , McCrum, Russell C. , Wright, Philip M.
IPC分类号： B21J15/10
CPC分类号： B23Q9/0007 , B21J15/10 , B21J15/142 , B21J15/28 , B23Q9/0042 , B64F5/10 , Y02P70/585
摘要： The present invention relates to a portable process for automated fastening of aircraft structures. The invention will employ two primary elements for locating and installing through-the-skin fasteners. Inside and outside units are attached onto an airframe and indexed to each other through coordination holes that have been pre-drilled through the structure. The aircraft structure is assembled with the pre-drilled coordination holes by aligning adjacent airframe parts and inserting alignment pins. The alignment pins will provide a degree of clamping to pull the parts together and provide indexing for inside and outside vacuum attachment track systems. The invention is equipped to traverse along the track system, accurately position itself, and drill only or countersink a hole, insert a fastener, and fasten, i.e., upset a rivet, or run down a threaded nut, then reposition itself to the next fastener location and repeat the process.

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