
基本信息:
- 专利标题: 一种钛合金及其环形锻件的成形方法
- 专利标题(英):Titanium alloy and annular titanium alloy forge piece forming method
- 申请号:CN201410303011.7 申请日:2014-06-30
- 公开(公告)号:CN104148554A 公开(公告)日:2014-11-19
- 发明人: 魏志坚 , 王龙祥 , 欧阳斌 , 田云 , 李艳英 , 夏春林 , 成陆祥 , 叶康源
- 申请人: 贵州安大航空锻造有限责任公司
- 申请人地址: 贵州省安顺市西秀区黄果树大街东段322号
- 专利权人: 贵州安大航空锻造有限责任公司
- 当前专利权人: 贵州安大航空锻造有限责任公司
- 当前专利权人地址: 贵州省安顺市西秀区黄果树大街东段322号
- 主分类号: B21J5/00
- IPC分类号: B21J5/00 ; B21H1/06 ; C22C14/00 ; C22F1/18
The invention discloses titanium alloy and an annular titanium alloy forge piece forming method. The chemical element content of the titanium alloy comprises, by weight, 7.50%-7.80% of A1, 1.00%-2.00% of Mo, 2.60%-2.80% of Zr, 2.60%-2.80% of Sn, 0.50%-1.50% of W, 0.10%-0.25% of Si, no more than 0.15% of Fe, no more than 0.10% of Cu, no more than 0.10% of Cr, no more than 0.10% of C, no more than 0.15% of O, no more than 0.04% of N, no more than 0.012% of H, and the balance Ti. The annular titanium alloy forge piece forming method comprises the following steps that after the titanium alloy is fed, and blanking is conducted at the temperature 30 DEG C below the phase transformation point; forming is conducted at the temperature 20 DEG C above the phase transformation point, and water cooling is conducted till the allay reaches the indoor temperature; double annealing is conducted on the materials obtained through the above two steps. The annular titanium alloy forge piece has the high-temperature tensile strength which can meet the use conditions and is large in affluence measure at the temperature ranging from 500 DEG C to 550 DEG C and can replace TC 25 to be used for manufacturing compressor parts and the like.
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 |
----B21J | 锻造;锤击;压制;铆接;锻造炉 |
------B21J5/00 | 锻压、锤击或压制的方法;其专用设备或附件 |