发明名称 |
Device for realizing belt-grinding operation on metal piece of aircraft turbo shaft engine, has driving roller fixed in path to support abrasive support between transmitting reel and guide roller, and between guide roller and take-up reel |
摘要 |
<p>The device has a transmitting reel (3), a take-up reel (7) and a guide roller (6) of an abrasive support (2) i.e. ribbon shaped abrasive support, where the reels and the guide roller are positioned in order to define a rectilinear section on a path that is utilized for a belt-grinding operation on a metal piece (1). A driving roller (4) is placed in the path to support the support between the transmitting reel and the guide roller, and between the guide roller and the take-up reel. An adjusting roller (8) is placed on the path of the support between the driving roller and one of the reels. An independent claim is also included for a method for belt-grinding a metal piece along a rectilinear section located between two roller guides.</p> |
申请公布号 |
FR2952564(A1) |
申请公布日期 |
2011.05.20 |
申请号 |
FR20090058157 |
申请日期 |
2009.11.18 |
申请人 |
SNECMA |
发明人 |
BRIDET PASCAL;NAYAR PIERRE, MARCEL, EMILIEN |
分类号 |
B24B9/00;B24B21/16 |
主分类号 |
B24B9/00 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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