公开(公告)号：US11866201B2

公开(公告)日：2024-01-09

申请号：US17735426

申请日：2022-05-03

申请人： The Boeing Company

发明人： Santiago Mejia ,  Patrick James Macko ,  Byron James Autry ,  Paul Gabriel Werntges ,  Larry Scott Smotherman ,  David Raines ,  Sara Murphy

IPC分类号： B64F5/10 ,  B64C1/12 ,  B64C1/06

CPC分类号： B64F5/10 ,  B23P2700/01 ,  B64C1/061 ,  B64C1/068 ,  B64C1/12

摘要： A device to assemble a skin and a frame of an aircraft fuselage. The device includes first and second brace members that extend along opposing sides of a gap. Arches are spaced apart and fixedly connected to the first and second brace members and that extend across the gap. A strongback is attached to and movable along the first and second brace members with the strongback having a curved shape that matches the plurality of arches. The strongback includes clamps configured to engage with the frame. First and second tension devices apply tension to the skin at the strongback.

公开(公告)号：US20230356857A1

公开(公告)日：2023-11-09

申请号：US17735426

申请日：2022-05-03

申请人： The Boeing Company

发明人： Santiago Mejia ,  Patrick James Macko ,  Byron James Autry ,  Paul Gabriel Werntges ,  Larry Scott Smotherman ,  David Raines ,  Sara Murphy

IPC分类号： B64F5/10

CPC分类号： B64F5/10

摘要： A device to assemble a skin and a frame of an aircraft fuselage. The device includes first and second brace members that extend along opposing sides of a gap. Arches are spaced apart and fixedly connected to the first and second brace members and that extend across the gap. A strongback is attached to and movable along the first and second brace members with the strongback having a curved shape that matches the plurality of arches. The strongback includes clamps configured to engage with the frame. First and second tension devices apply tension to the skin at the strongback.

公开(公告)号：US20240101277A1

公开(公告)日：2024-03-28

申请号：US18526548

申请日：2023-12-01

申请人： The Boeing Company

发明人： Santiago Mejia ,  Patrick James Macko ,  Byron James Autry ,  Paul Gabriel Werntges ,  Larry Scott Smotherman ,  David Raines ,  Sara Murphy

IPC分类号： B64F5/10

CPC分类号： B64F5/10 ,  B23P2700/01 ,  B64C1/061

摘要： A device to assemble a skin and a frame of an aircraft fuselage. The device includes first and second brace members that extend along opposing sides of a gap. Arches are spaced apart and fixedly connected to the first and second brace members and that extend across the gap. A strongback is attached to and movable along the first and second brace members with the strongback having a curved shape that matches the plurality of arches. The strongback includes clamps configured to engage with the frame. First and second tension devices apply tension to the skin at the strongback.