
基本信息:
- 专利标题: 一种高温合金整体叶环叶片铣削加工方法
- 申请号:CN201611068988.0 申请日:2016-11-29
- 公开(公告)号:CN106513804B 公开(公告)日:2019-07-05
- 发明人: 韩德印 , 徐一鸣 , 杨楠 , 张莹 , 吴军
- 申请人: 中国航发沈阳黎明航空发动机有限责任公司
- 申请人地址: 辽宁省沈阳市大东区东塔街6号
- 专利权人: 中国航发沈阳黎明航空发动机有限责任公司
- 当前专利权人: 中国航发沈阳黎明航空发动机有限责任公司
- 当前专利权人地址: 辽宁省沈阳市大东区东塔街6号
- 代理机构: 沈阳优普达知识产权代理事务所
- 代理人: 俞鲁江
- 主分类号: B23C3/18
- IPC分类号: B23C3/18
The invention discloses a milling method of a blade of a high-temperature alloy whole blade ring. The method comprises following steps: firstly, a manufacturing procedure is selected, and the milling technology path of the whole blade ring comprises air inlet end rough milling slotting, exhaust end rough milling slotting, air inlet end blade type and flow way accurate milling and exhaust end blade type and flow way accurate milling; secondly, according to the length and the maximum thickness of the blade of the whole blade ring blade type, the machining allowance reserved for accurate milling after rough milling slotting is determined; thirdly, a tool is selected, wherein during rough milling, an end milling cutter of phi 6R0.5 to phi 6R1.5 is selected for machining, and during accurate milling, a taper ball head milling cutter with the shrinking neck is selected for machining; fourthly, cutting parameters are selected; fifthly, the accurate milling step is selected. Machining of the blade of the high-temperature alloy blade ring part is effectively achieved, the method can ensure that the machined part has the good surface quality and meets the design required form and location tolerance, and the method also can be applied to milling of complex curve deep cavities.
公开/授权文献:
- CN106513804A 一种高温合金整体叶环叶片铣削加工方法 公开/授权日:2017-03-22
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 |
----B23C | 铣削 |
------B23C3/00 | 特殊工件的铣削;特殊铣削加工;其所用机床 |
--------B23C3/16 | .加工在两个方向上弯曲的表面 |
----------B23C3/18 | ..用于螺旋桨,透平叶片或叶轮的成型加工 |