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公开(公告)号:US20130212883A1
公开(公告)日:2013-08-22
申请号:US13771379
申请日:2013-02-20
Applicant: Airbus Operations S.L.
Inventor: Jorge Juan Soto Martinez , Juan Francisco Garcia Amado , Marta Gimenez Olazabal , Jose Gorrotxategi Txurruka , Jokin Lekunberri Urkidi , Jon Ander Altamira Ugarte
CPC classification number: B23P19/06 , B21J15/022 , B21J15/142 , B21J15/32 , B23P19/001 , B23P19/005 , B23P19/006 , B23P19/04 , B23P19/10 , B23P2700/01 , B23Q16/00 , B25B1/04 , B25B21/002 , B25B23/1415 , B25J9/1697 , B25J11/005 , B25J11/007 , B25J15/0019 , B25J19/0058 , B64F5/10 , F16B31/021 , G05B2219/45088 , G05B2219/45126 , Y10T29/49622 , Y10T29/49908 , Y10T29/49948 , Y10T29/49956 , Y10T29/53078 , Y10T29/53091 , Y10T29/53096 , Y10T29/53774 , Y10T29/53991
Abstract: A head of a riveting device—for Hi-Lite type rivets—of at least two components of a structure for installing automatically collars on pins previously inserted in the structure. The head comprises: a collar installation tool; a collar supply to supply collars to the collar installation tool; a tool actuating device; a linear displacement device to linearly move the tool during the threading operation; a withdrawal device arranged to withdraw the second part of the collars; a control arrangement configured to automatically perform the installation of collars on pins and after this the withdrawal of the second part of the collars, using tools and collars appropriate for the pins. Also a robot having as end-effector the head and to a method of riveting two components of an aircraft fuselage are provided.
Abstract translation: 铆钉装置的头部,用于Hi-Lite型铆钉,其至少两个部件组件用于自动地将套环安装在先前插入结构中的销上。 头部包括:衣领安装工具; 一个领子供应,以提供领子安装工具的领子; 工具致动装置; 线性位移装置,用于在穿线操作期间线性地移动工具; 撤回装置,其布置成撤回所述套环的第二部分; 控制装置被配置为自动地执行在销上的套环的安装,并且在这之后使用适合于销的工具和套环撤回套环的第二部分。 还提供了具有端部执行器头部的机器人和铆接飞行器机身的两个部件的方法。
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公开(公告)号:US09296076B2
公开(公告)日:2016-03-29
申请号:US13771379
申请日:2013-02-20
Applicant: Airbus Operations S.L.
Inventor: Jorge Juan Soto Martinez , Juan Francisco Garcia Amado , Marta Gimenez Olazabal , Jose Gorrotxategi Txurruka , Jokin Lekunberri Urkidi , Jon Ander Altamira Ugarte
IPC: B23P15/28 , B21J15/14 , B23P19/06 , B25B21/00 , B25B23/14 , B64F5/00 , B25J15/00 , B21J15/02 , B21J15/32 , B25J19/00 , B25J9/16 , B25J11/00 , B23Q16/00 , B23P19/10 , B25B1/04 , B23P19/04 , B23P19/00 , F16B31/02
CPC classification number: B23P19/06 , B21J15/022 , B21J15/142 , B21J15/32 , B23P19/001 , B23P19/005 , B23P19/006 , B23P19/04 , B23P19/10 , B23P2700/01 , B23Q16/00 , B25B1/04 , B25B21/002 , B25B23/1415 , B25J9/1697 , B25J11/005 , B25J11/007 , B25J15/0019 , B25J19/0058 , B64F5/10 , F16B31/021 , G05B2219/45088 , G05B2219/45126 , Y10T29/49622 , Y10T29/49908 , Y10T29/49948 , Y10T29/49956 , Y10T29/53078 , Y10T29/53091 , Y10T29/53096 , Y10T29/53774 , Y10T29/53991
Abstract: A head of a riveting device—for Hi-Lite type rivets—of at least two components of a structure for installing automatically collars on pins previously inserted in the structure. The head comprises: a collar installation tool; a collar supply to supply collars to the collar installation tool; a tool actuating device; a linear displacement device to linearly move the tool during the threading operation; a withdrawal device arranged to withdraw the second part of the collars; a control arrangement configured to automatically perform the installation of collars on pins and after this the withdrawal of the second part of the collars, using tools and collars appropriate for the pins. Also a robot having as end-effector the head and to a method of riveting two components of an aircraft fuselage are provided.
Abstract translation: 铆钉装置的头部,用于Hi-Lite型铆钉,其至少两个部件组件用于自动地将套环安装在先前插入结构中的销上。 头部包括:衣领安装工具; 一个领子供应,以提供领子安装工具的领子; 工具致动装置; 线性位移装置,用于在穿线操作期间线性地移动工具; 撤回装置,其布置成撤回所述套环的第二部分; 控制装置被配置为自动地执行在销上的套环的安装,并且在这之后使用适合于销的工具和套环撤回套环的第二部分。 还提供了具有端部执行器头部的机器人和铆接飞行器机身的两个部件的方法。
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