
基本信息:
- 专利标题: 小弯曲半径航空导管弯管成型模及其成型方法
- 专利标题(英):Small-bending-radius aviation conduit bend forming die and forming method thereof
- 申请号:CN201410256531.7 申请日:2014-06-11
- 公开(公告)号:CN104043734A 公开(公告)日:2014-09-17
- 发明人: 张伟强 , 李兴云
- 申请人: 沈阳飞机工业(集团)有限公司
- 申请人地址: 辽宁省沈阳市皇姑区陵北街1号
- 专利权人: 沈阳飞机工业(集团)有限公司
- 当前专利权人: 沈阳飞机工业(集团)有限公司
- 当前专利权人地址: 辽宁省沈阳市皇姑区陵北街1号
- 代理机构: 沈阳杰克知识产权代理有限公司
- 代理人: 孙玲
- 主分类号: B21D37/10
- IPC分类号: B21D37/10 ; B21D9/01
The invention relates to a small-bending-radius aviation conduit bend forming die and a forming method thereof. The small-bending-radius aviation conduit bend forming die comprises an upper die and a lower die, wherein a cavity formed after the upper die and the lower die are buckled is in a bent conduit shape, the two ends of the cavity are respectively provided with a limiting table, the limiting tables are provided with guide sleeve coaxial with the two ends of the cavity, a flexible central spindle is arranged in one guide sleeve and is connected with a low pressure piston through a connecting rod, a gasket is arranged in the other guide sleeve, the outer end face of the gasket is matched with a high pressure piston, and the low pressure piston and the high pressure piston are respectively in coaxial sliding fit with the corresponding guide sleeves. The forming die and the method thereof solve the processing difficult problem about forming of a small-bending-radius aviation conduit and realize the forming of the aviation conduit in a stable state, the phenomena of cracking, wrinkling and necking do not easily occur during forming, and a high-quality stable and efficient shaping processing method of small-bending-radius aviation conduit parts is realized.
IPC结构图谱:
B | 作业;运输 |
--B21 | 基本上无切削的金属机械加工;金属冲压 |
----B21D | 金属板或管、棒或型材的基本无切削加工或处理;冲压 |
------B21D37/00 | 作为本小类所包括的机器的部件的工具 |
--------B21D37/10 | .模具组;导向支柱 |