CN104972031A - Titanium alloy forging process - Google Patents

Titanium alloy forging process Download PDF

Info

Publication number
CN104972031A
CN104972031A CN201510351434.0A CN201510351434A CN104972031A CN 104972031 A CN104972031 A CN 104972031A CN 201510351434 A CN201510351434 A CN 201510351434A CN 104972031 A CN104972031 A CN 104972031A
Authority
CN
China
Prior art keywords
titanium alloy
blank
forging process
alloy forging
workpiece
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
Application number
CN201510351434.0A
Other languages
Chinese (zh)
Inventor
陈文建
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to CN201510351434.0A priority Critical patent/CN104972031A/en
Publication of CN104972031A publication Critical patent/CN104972031A/en
Pending legal-status Critical Current

Links

Abstract

The invention relates to a titanium alloy forging process. The titanium alloy forging process comprises the following steps that 1, the surface of titanium alloy is treated, the titanium alloy is pre-heated for 15 minutes at 110 DEG C, and the surface of the titanium alloy is painted with protective agents; 2, a titanium alloy blank is arranged in a furnace to be heated, the temperature is 1,000 DEG C, heat preservation is carried out for 0.5 hour, the furnace temperature rises to 1,200 DEG C, and heat preservation is carried out for two hours; 3, the blank is forged to be formed; 4, the blank is naturally cooled, and then the surface protective agents are removed; and 5, a titanium alloy workpiece is checked. The titanium alloy forging process is reasonable in process path design, simple and feasible, production efficiency is greatly improved, and meanwhile the surface quality of the titanium alloy workpiece is improved.

Description

A kind of titanium alloy smithing technological
Technical field
The present invention relates to technical field of forging, be specifically related to a kind of titanium alloy smithing technological.
Background technology
Forging is that one utilizes metal forming machinery to apply pressure to metal stock, makes it produce plastic deformation to obtain the processing method with certain mechanical performance, definite shape and size forging, one of two large parts of forging and stamping (forging and punching press).At mechanical field, forging is widely used in all many-sides, and the processing of a lot of metal alloy also adopts forging mode to carry out, as titanium alloy workpiece.But in existing titanium alloy smithing technological, due to the various problems that technological design exists, process cycle is longer, takes time and effort, and production efficiency is low, and the quality of titanium alloy workpiece is also barely satisfactory.
Summary of the invention
For solving the above-mentioned problems in the prior art, the invention provides a kind of titanium alloy smithing technological.
Technique effect of the present invention is achieved through the following technical solutions:
A kind of titanium alloy smithing technological, comprises the following steps:
Step one: titanium alloy surface process, 110 DEG C of preheatings 15 minutes, at titanium alloy surface brushing protective agent;
Step 2: titanium alloy blank shove charge heated, temperature 1000 DEG C, is incubated 0.5 hour, then furnace temperature is risen to 1200 DEG C, is incubated 2 hours;
Step 3: blank forging is shaping;
Step 4: carry out surface-protective agent removal after naturally being cooled by blank;
Step 5: titanium alloy workpiece is checked.
The invention has the beneficial effects as follows:
A kind of titanium alloy smithing technological disclosed in this invention, Process Route Planning is reasonable, simple, greatly improves production efficiency, also improves the surface quality of titanium alloy simultaneously.
Detailed description of the invention
The present invention is realized by following detailed description of the invention:
A kind of titanium alloy smithing technological, comprises the following steps:
Step one: titanium alloy surface process, 110 DEG C of preheatings 15 minutes, at titanium alloy surface brushing protective agent;
Step 2: titanium alloy blank shove charge heated, temperature 1000 DEG C, is incubated 0.5 hour, then furnace temperature is risen to 1200 DEG C, is incubated 2 hours;
Step 3: blank forging is shaping;
Step 4: carry out surface-protective agent removal after naturally being cooled by blank;
Step 5: titanium alloy workpiece is checked.
Last it is noted that the foregoing is only the preferred embodiments of the present invention, be not limited to the present invention, although with reference to previous embodiment to invention has been detailed description, for a person skilled in the art, it still can be modified to the technical scheme described in foregoing embodiments, or carries out equivalent replacement to wherein portion of techniques feature.Within the spirit and principles in the present invention all, any amendment done, equivalent replacement, improvement etc., all should be included within protection scope of the present invention.

Claims (1)

1. a titanium alloy smithing technological, is characterized in that: comprise the following steps:
Step one: titanium alloy surface process, 110 DEG C of preheatings 15 minutes, at titanium alloy surface brushing protective agent;
Step 2: titanium alloy blank shove charge heated, temperature 1000 DEG C, is incubated 0.5 hour, then furnace temperature is risen to 1200 DEG C, is incubated 2 hours;
Step 3: blank forging is shaping;
Step 4: carry out surface-protective agent removal after naturally being cooled by blank;
Step 5: titanium alloy workpiece is checked.
CN201510351434.0A 2015-06-24 2015-06-24 Titanium alloy forging process Pending CN104972031A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201510351434.0A CN104972031A (en) 2015-06-24 2015-06-24 Titanium alloy forging process

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201510351434.0A CN104972031A (en) 2015-06-24 2015-06-24 Titanium alloy forging process

Publications (1)

Publication Number Publication Date
CN104972031A true CN104972031A (en) 2015-10-14

Family

ID=54269306

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201510351434.0A Pending CN104972031A (en) 2015-06-24 2015-06-24 Titanium alloy forging process

Country Status (1)

Country Link
CN (1) CN104972031A (en)

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101294265A (en) * 2008-05-12 2008-10-29 中国航空工业第一集团公司北京航空材料研究院 Titanium alloy smithing technological parameter testing method
CN101624668A (en) * 2009-08-05 2010-01-13 浙江民泰钛合金有限公司 Beta-titanium alloy with low cost and easy production and manufacture method thereof
CN101733348A (en) * 2009-12-22 2010-06-16 沈阳黎明航空发动机(集团)有限责任公司 Isothermal forging method for titanium alloy blade
CN102764839A (en) * 2012-08-06 2012-11-07 河北中泊防爆工具集团有限公司 Titanium alloy forging process
CN102839297A (en) * 2012-09-27 2012-12-26 哈尔滨工业大学 High-temperature titanium alloy and preparation method thereof
CN103722108A (en) * 2013-12-06 2014-04-16 陕西宏远航空锻造有限责任公司 Titanium alloy blade forging method

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101294265A (en) * 2008-05-12 2008-10-29 中国航空工业第一集团公司北京航空材料研究院 Titanium alloy smithing technological parameter testing method
CN101624668A (en) * 2009-08-05 2010-01-13 浙江民泰钛合金有限公司 Beta-titanium alloy with low cost and easy production and manufacture method thereof
CN101733348A (en) * 2009-12-22 2010-06-16 沈阳黎明航空发动机(集团)有限责任公司 Isothermal forging method for titanium alloy blade
CN102764839A (en) * 2012-08-06 2012-11-07 河北中泊防爆工具集团有限公司 Titanium alloy forging process
CN102839297A (en) * 2012-09-27 2012-12-26 哈尔滨工业大学 High-temperature titanium alloy and preparation method thereof
CN103722108A (en) * 2013-12-06 2014-04-16 陕西宏远航空锻造有限责任公司 Titanium alloy blade forging method

Similar Documents

Publication Publication Date Title
MX353547B (en) Thermomechanical processing of high strength non-magnetic corrosion resistant material.
CN103706743B (en) Die-forging forming process of titanium-alloy forged drum piece
CN102989986A (en) Forging technology of large TC4 alloy drum forged piece
CN105014314A (en) Wheel hub forging technology
EP2581160A3 (en) System and method of manufacturing a structure with a high performance metal alloy
CN109248979A (en) A kind of flange forging method
CN102764839B (en) Titanium alloy forging process
MX344480B (en) Method for reshaping forged parts.
CN104972031A (en) Titanium alloy forging process
CN104972037A (en) Forging technology used for improving surface quality of forge piece
CN104972032A (en) Steering knuckle forging process
CN105695699A (en) Micro-deformation vacuum heat treatment process for 40CrNi steel gear
CN104971963A (en) Slab forging process
CN104438885A (en) High-precision bending die manufacturing method
CN105880925A (en) Outer hexagonal bolt machining process
CN104972030A (en) Locomotive connecting rod forging process
CN103643016A (en) Production method of motorcycle lower yoke plate
CN104972036A (en) Workpiece forging process
CN103639647B (en) The production technology of motorcycle lower link plate
CN103014245A (en) Heat treatment workpiece correction treatment method
CN104959497A (en) Forging technology for stainless steel
CN104972033A (en) Piston rod forging technology
CN103484637A (en) Heat-treatment workpiece correction treatment method
CN103551480B (en) A kind of finish forge mould for mount pad forging and finish forge method
CN105081168A (en) Machining method of thin-wall metal pipe

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: 20151014

RJ01 Rejection of invention patent application after publication