发明公开
EP2121225A1 PROCEDE D'ASSEMBLAGE DE DEUX ENSEMBLES, TELS QUE DES ENSEMBLES DE FUSELAGE D'AERONEF
有权
![PROCEDE D'ASSEMBLAGE DE DEUX ENSEMBLES, TELS QUE DES ENSEMBLES DE FUSELAGE D'AERONEF](/ep/2009/11/25/EP2121225A1/abs.jpg.150x150.jpg)
基本信息:
- 专利标题: PROCEDE D'ASSEMBLAGE DE DEUX ENSEMBLES, TELS QUE DES ENSEMBLES DE FUSELAGE D'AERONEF
- 专利标题(英):Method for assembling two assemblies such aircraft fuselage assemblies
- 专利标题(中):程序对两种安装ANORNDNUNGEN如飞机船体安排
- 申请号:EP08716866.2 申请日:2008-02-15
- 公开(公告)号:EP2121225A1 公开(公告)日:2009-11-25
- 发明人: HOUIS, Jean-Luc , COHEN BACRI, Gérard
- 申请人: Airbus Operations
- 申请人地址: 316 Route de Bayonne 31060 Toulouse FR
- 专利权人: Airbus Operations
- 当前专利权人: Airbus Operations
- 当前专利权人地址: 316 Route de Bayonne 31060 Toulouse FR
- 代理机构: Ilgart, Jean-Christophe
- 优先权: FR0753303 20070216
- 国际公布: WO2008101873 20080828
- 主分类号: B23B49/02
- IPC分类号: B23B49/02 ; B21J15/02
摘要:
The invention relates to a method for assembling two assemblies, e.g. aircraft fuselage assemblies, using a plurality of fixation members. The method comprises drilling openings in an overlap area using a drilling tool and through a corresponding centring opening (36) formed in a drilling grid (34) rigidly mounted on said overlap area, wherein the drilling tool includes a bearing mandrel as well as an expansible ring (56) in tight contact with the mandrel along a conical contact surface. According to the invention, a relative movement is applied between the expansible ring and the mandrel in order to create, after locking the ring in the centring opening, a displacement of the mandrel, bearing against the overlap area, through the centring opening and in the direction of the overlap area in order to apply a pressure thereon.
公开/授权文献:
IPC结构图谱:
B | 作业;运输 |
--B23 | 机床;不包含在其他类目中的金属加工 |
----B23B | 车削;镗削 |
------B23B49/00 | 为钻头在镗床或钻床中定位或导向用的测量或校准装置;用于指示镗孔或钻孔时钻头折断的装置;被镗或钻的孔的定心装置 |
--------B23B49/02 | .镗(钻)模或镗(钻)套 |