CN106238642A - A kind of process of titanium alloy steel forging - Google Patents
A kind of process of titanium alloy steel forging Download PDFInfo
- Publication number
- CN106238642A CN106238642A CN201610603530.4A CN201610603530A CN106238642A CN 106238642 A CN106238642 A CN 106238642A CN 201610603530 A CN201610603530 A CN 201610603530A CN 106238642 A CN106238642 A CN 106238642A
- Authority
- CN
- China
- Prior art keywords
- titanium alloy
- alloy steel
- forging
- heated
- incubated
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21J—FORGING; HAMMERING; PRESSING METAL; RIVETING; FORGE FURNACES
- B21J5/00—Methods for forging, hammering, or pressing; Special equipment or accessories therefor
- B21J5/02—Die forging; Trimming by making use of special dies ; Punching during forging
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21J—FORGING; HAMMERING; PRESSING METAL; RIVETING; FORGE FURNACES
- B21J1/00—Preparing metal stock or similar ancillary operations prior, during or post forging, e.g. heating or cooling
- B21J1/06—Heating or cooling methods or arrangements specially adapted for performing forging or pressing operations
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21J—FORGING; HAMMERING; PRESSING METAL; RIVETING; FORGE FURNACES
- B21J3/00—Lubricating during forging or pressing
Abstract
The invention provides the process of a kind of titanium alloy steel forging, comprise the steps: 1) titanium alloy steel is warming up to 180 DEG C in box type heater, carry out being incubated 20 min, spray lubricant, the blank after spraying is dried 15min in 100 DEG C of environment；2) titanium alloy steel and mould are heated separately to 1200 and 1500 DEG C, heat 20 min, soaking 10 min；3) again mould being heated to 950 DEG C, mold cavity location put into by the titanium alloy steel that would be heated to 950 DEG C, is incubated 10 min；4) the forging post processing of air cooling is used.The process of a kind of titanium alloy steel forging that the present invention provides, by experimental results demonstrate, using the method stock utilization is 60%, visible, the improvement of technique can be significantly increased stock utilization, reduce and machine man-hour, for meeting the high-tech areas such as Aero-Space, the demand of titanium alloy fine forging is laid a good foundation.
Description
Technical field
The present invention relates to steel technical field, particularly relate to the process of a kind of titanium alloy steel forging.
Background technology
Steel and iron industry is from forming the development having obtained till now advancing by leaps and bounds, and in these steel, considerable quantity is through machine
Field and the occasion of all trades and professions is served in tool processing with the form of part.Along with the cutting speed of machining is increasingly faster,
The technique of steel be it is also proposed higher requirement.
Summary of the invention
For solving the problems referred to above present in prior art and practical situation, the invention provides a kind of titanium alloy steel forging
Process, it is characterised in that comprise the steps:
1) titanium alloy steel is warming up to 180 DEG C in box type heater, carries out being incubated 20 min, spray lubricant,
Blank after spraying is dried 15min in 100 DEG C of environment；
2) titanium alloy steel and mould are heated separately to 1200 and 1500 DEG C, heat 20 min, soaking 10 min；
3) again mould being heated to 950 DEG C, mold cavity location put into by the titanium alloy steel that would be heated to 950 DEG C, is incubated 10
min；
4) the forging post processing of air cooling is used.
Beneficial effect:
The process of a kind of titanium alloy steel forging that the present invention provides, by experimental results demonstrate, uses the method material profit
It is 60% by rate, it is seen then that the improvement of technique can be significantly increased stock utilization, reduces and machine man-hour, for meeting aviation boat
It etc. high-tech area the demand of titanium alloy fine forging is laid a good foundation.
Detailed description of the invention
Technical solution of the present invention is described in detail below.
The process of a kind of titanium alloy steel forging, it is characterised in that comprise the steps:
1) titanium alloy steel is warming up to 180 DEG C in box type heater, carries out being incubated 20 min, spray lubricant,
Blank after spraying is dried 15min in 100 DEG C of environment；
2) titanium alloy steel and mould are heated separately to 1200 and 1500 DEG C, heat 20 min, soaking 10 min；
3) again mould being heated to 950 DEG C, mold cavity location put into by the titanium alloy steel that would be heated to 950 DEG C, is incubated 10
min；
4) the forging post processing of air cooling is used.
Beneficial effect:
The process of a kind of titanium alloy steel forging that the present invention provides, by experimental results demonstrate, uses the method material profit
It is 60% by rate, it is seen then that the improvement of technique can be significantly increased stock utilization, reduces and machine man-hour, for meeting aviation boat
It etc. high-tech area the demand of titanium alloy fine forging is laid a good foundation.
Finally it is noted that the foregoing is only the preferred embodiments of the present invention, it is not limited to the present invention,
Although being described in detail the present invention with reference to previous embodiment, for a person skilled in the art, it still may be used
So that the technical scheme described in foregoing embodiments to be modified, or wherein portion of techniques feature is carried out equivalent.
All within the spirit and principles in the present invention, any modification, equivalent substitution and improvement etc. made, should be included in the present invention's
Within protection domain.
Claims (1)
1. the process of a titanium alloy steel forging, it is characterised in that comprise the steps:
1) titanium alloy steel is warming up to 180 DEG C in box type heater, carries out being incubated 20 min, spray lubricant,
Blank after spraying is dried 15min in 100 DEG C of environment；
2) titanium alloy steel and mould are heated separately to 1200 and 1500 DEG C, heat 20 min, soaking 10 min；
3) again mould being heated to 950 DEG C, mold cavity location put into by the titanium alloy steel that would be heated to 950 DEG C, is incubated 10
min；
4) the forging post processing of air cooling is used.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610603530.4A CN106238642A (en) | 2016-07-28 | 2016-07-28 | A kind of process of titanium alloy steel forging |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610603530.4A CN106238642A (en) | 2016-07-28 | 2016-07-28 | A kind of process of titanium alloy steel forging |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106238642A true CN106238642A (en) | 2016-12-21 |
Family
ID=57604481
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610603530.4A Pending CN106238642A (en) | 2016-07-28 | 2016-07-28 | A kind of process of titanium alloy steel forging |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106238642A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110814251A (en) * | 2019-11-14 | 2020-02-21 | 西安三角防务股份有限公司 | Forging method of large TC18 titanium alloy die forging for landing gear |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101074469A (en) * | 2007-06-12 | 2007-11-21 | 燕山大学 | Forged (rolled) abrasive austenic permanganic steel and its manufacture |
| CN101332484A (en) * | 2007-06-25 | 2008-12-31 | 宝山钢铁股份有限公司 | Die forging method of high-temperature alloy |
| CN102071367A (en) * | 2010-11-24 | 2011-05-25 | 南京迪威尔重型锻造股份有限公司 | Steel forging manufacturing process for deep-sea Christmas tree equipment connectors |
| CN103074523A (en) * | 2013-01-31 | 2013-05-01 | 安徽工业大学 | Mould material for detecting high-temperature fatigue performance and preparation method of mould material |
| CN103381459A (en) * | 2013-06-03 | 2013-11-06 | 上海齐耀动力技术有限公司 | Die forging technology for barrel body of high temperature alloy steel heater |
-
2016
- 2016-07-28 CN CN201610603530.4A patent/CN106238642A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101074469A (en) * | 2007-06-12 | 2007-11-21 | 燕山大学 | Forged (rolled) abrasive austenic permanganic steel and its manufacture |
| CN101332484A (en) * | 2007-06-25 | 2008-12-31 | 宝山钢铁股份有限公司 | Die forging method of high-temperature alloy |
| CN102071367A (en) * | 2010-11-24 | 2011-05-25 | 南京迪威尔重型锻造股份有限公司 | Steel forging manufacturing process for deep-sea Christmas tree equipment connectors |
| CN103074523A (en) * | 2013-01-31 | 2013-05-01 | 安徽工业大学 | Mould material for detecting high-temperature fatigue performance and preparation method of mould material |
| CN103381459A (en) * | 2013-06-03 | 2013-11-06 | 上海齐耀动力技术有限公司 | Die forging technology for barrel body of high temperature alloy steel heater |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110814251A (en) * | 2019-11-14 | 2020-02-21 | 西安三角防务股份有限公司 | Forging method of large TC18 titanium alloy die forging for landing gear |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20161221 |
|
| RJ01 | Rejection of invention patent application after publication |