Forming method of large-concentration-ratio upset forging components made of titanium alloy
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- SHENYANG LIMING AERO-ENGINE GROUP CORPORATION
- Publication Date
- 2016-02-17
Smart Images
Figure 1 Figure 2 Figure 3
Abstract
Description
technical field
[0001] The invention belongs to the field of metal plastic forming, in particular to a forming method of a titanium alloy top forging with a large aggregation ratio. Background technique
[0002] Upset forgings are divided into rod forgings with thick parts, forgings with through holes or non-through holes without rods, extrusions, pipe upsetting forgings, etc.
[0003] Among stainless steel forgings, the aggregation ratio of rod forgings with thick parts (that is, the ratio of the length of the thick part to the diameter of the bar) can reach more than 10. However, the aggregation ratio of titanium alloy top forgings is relatively small, generally 1.2 to 1.4, which is only suitable for upsetting of general parts or blanking of small and medium blades. This is because the metal fluidity of titanium alloy itself is poor, and its toughness is also lower than that of stainless steel.
[0004] At present, some aeroengines use titanium alloy blade mounting plate...