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CN103572085A - Preparation method of TiAl-base alloy - Google Patents

Preparation method of TiAl-base alloy Download PDF

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Publication number
CN103572085A
CN103572085A CN201310555751.5A CN201310555751A CN103572085A CN 103572085 A CN103572085 A CN 103572085A CN 201310555751 A CN201310555751 A CN 201310555751A CN 103572085 A CN103572085 A CN 103572085A
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CN
China
Prior art keywords
powder
tial
low
preparation
base alloy
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
CN201310555751.5A
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Chinese (zh)
Inventor
李达人
韩胜利
崔利群
蔡一湘
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.)
Guangzhou Research Institute of Non Ferrous Metals
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Guangzhou Research Institute of Non Ferrous Metals
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Filing date
Publication date
Application filed by Guangzhou Research Institute of Non Ferrous Metals filed Critical Guangzhou Research Institute of Non Ferrous Metals
Priority to CN201310555751.5A priority Critical patent/CN103572085A/en
Publication of CN103572085A publication Critical patent/CN103572085A/en
Pending legal-status Critical Current

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Abstract

The invention discloses a preparation method of a TiAl-base alloy. The preparation method is characterized by comprising the following steps: (1) evenly mixing TiAl3 powder with the granularity of 300 meshes and Ti powder with the granularity of 500 meshes at a mass ratio of (1:2)-(1:5); (2) performing cold pressing on the mixture under a pressure of 800MPa so as to obtain billets and encapsulating the billets into a low-carbon steel sleeve when the vacuum degree is 5*10<-2>Pa; (3) heating the cold-pressed billets with the low-carbon steel sleeve to 1050-1250 DEG C at a heating speed of 50 DEG C/min, and putting the cold-pressed billets with the low-carbon steel sleeve into a mold to extrude and form after carrying out heat preservation for 30-60 minutes. The preparation method is simple in process and low in cost; the problem of high cost of a pre-alloying method is solved; meanwhile, the problem of volume expansion when the TiAl alloy is prepared from Ti and Al elements by a powder method is avoided; the TiAl-base alloy with high compactness and even and fine tissue can be obtained.

Description

A kind of preparation method of TiAl base alloy
Technical field
The invention belongs to high-temperature structural material preparing technical field, relate in particular to a kind of preparation method of TiAl base alloy.
Background technology
TiAl base alloy has the essential series of features of high-temperature structural material, has caused numerous scientific research personnel's attention, and various countries have also dropped into a large amount of human and material resources, financial resources are studied, and has obtained some achievements.TiAl base alloy has the outstanding advantages such as density is light, high temperature resistance, resistance to oxidation, shows very wide application prospect in aerospace field, becomes the preferred material of advanced military aircraft engine pneumatic plant and low-pressure turbine blade.
Precision-investment casting is current most widely used TiAl base Alloy Forming technology, can once cast part complex-shaped, thin-walled, and foundry goods has high dimensional precision and low surfaceness.CN101457331A adopts a consumable to add induction suspending investment cast and makes blank, and blank obtains TiAl alloy bar material after jacket-Intermittent pneumatic compression.But casting time exists the chemical activity of melt strong, gravity head is little, fill the problems such as type mobility is not high.
It is raw material that powder metallurgic method be take simple substance or powdered alloy, adopt conventional plastic processing method to carry out consolidation to powder, and then through sintering, can directly obtain the TiAl base alloy product of desired shape, realize the near-net forming of product simultaneously, thereby avoided follow-up plastic working or mechanical workout to TiAl base alloy, and the alloy obtaining compare with casting organize more even, tiny.Powder metallurgy is prepared TiAl base alloy prior can be divided into element powders method and pre-alloyed powder method by raw material powder.Ti, Al element powders legal system are during for TiAl base alloy, and the inclined to one side spread coefficient between Ti, Al element differs greatly, and generate Frenkel hole, in pressureless sintering process, generate TiAl 3the middle phenomenon that causes mutually blank generation volumetric expansion.Pre-alloyed powder method compare with element powders method composition evenly, oxygen and foreign matter content is low, mechanical property is good, but raw material powder cost is high.It is raw material that CN101240382A be take Ti powder, Al powder and other microelement powder, and cold-press moulding has obtained high dense TiAl-base alloy after 1200 ~ 1400 ℃ of sintering.But Al is different from Ti spread coefficient, in sintering process, easily produce volumetric expansion, the homogeneity of ingredients of alloy and homogeneity of structure are difficult to guarantee.
Summary of the invention
The object of this invention is to provide a kind of density high, homogeneous microstructure is tiny, the preparation method of the TiAl base alloy of good mechanical properties.
Preparation method's step of TiAl base alloy of the present invention is as follows:
1. by 300 object TiAl 3powder mixes according to mass ratio 1:2 ~ 1:5 with 500 object Ti powder;
2. under 800MPa pressure, be cold-pressed into after base, in vacuum tightness 5 * 10 -2under Pa, enclose low-carbon (LC) steel bushing;
3. with the heat-up rate of 50 ℃/min, the blank of colding pressing with low-carbon (LC) steel bushing is warming up to 1050 ~ 1250 ℃, is incubated after 30 ~ 60min, put into mould extrusion molding.
Compared with prior art, beneficial effect of the present invention is that the present invention adopts Ti and TiAl 3for raw material, avoided Ti, Al element powders method to generate TiAl 3, therefore can there is not Study of Volume Expansion in the reaction of middle phase.The invention solves the problem of prealloy method raw material powder cost costliness, with lower cost, prepare density and be greater than 98%, ultimate compression strength is at 1717 ~ 2102MPa, the TiAl base alloy of average grain size below 40 μ m.
Embodiment
Embodiment mono-
By 300 object TiAl 3powder and 500 object Ti powder are 1:2 batching in mass ratio, on mixed powder machine, mixes the powder that obtains mixing for 72 hours; The powder mixing, under 800MPa pressure, is cold-pressed into after base, in vacuum tightness 5 * 10 -2under Pa, enclose low-carbon (LC) steel bushing; Heat-up rate with 50 ℃/min is warming up to 1050 ℃ by the blank of colding pressing with low-carbon (LC) steel bushing, after insulation 30min, puts into mould extrusion molding, makes density 98%, average grain size 20 μ m, the TiAl base alloy of ultimate compression strength 1800MPa.
Embodiment bis-
By 300 object TiAl 3powder and 500 object Ti powder are 1:3 batching in mass ratio, on mixed powder machine, mixes the powder that obtains mixing for 72 hours; The powder mixing, under 800MPa pressure, is cold-pressed into after base, in vacuum tightness 5 * 10 -2under Pa, enclose low-carbon (LC) steel bushing; Heat-up rate with 50 ℃/min is warming up to 1050 ℃ by the blank of colding pressing with low-carbon (LC) steel bushing, after insulation 30min, puts into mould extrusion molding, makes density 98%, average grain size 20 μ m, the TiAl base alloy of ultimate compression strength 1850MPa.
Embodiment tri-
By 300 object TiAl 3powder and 500 object Ti powder are 1:2 batching in mass ratio, on mixed powder machine, mixes the powder that obtains mixing for 72 hours; The powder mixing, under 800MPa pressure, is cold-pressed into after base, in vacuum tightness 5 * 10 -2under Pa, enclose low-carbon (LC) steel bushing; Heat-up rate with 50 ℃/min is warming up to 1150 ℃ by the blank of colding pressing with low-carbon (LC) steel bushing, after insulation 30min, puts into mould extrusion molding, makes density 99%, average grain size 25 μ m, the TiAl base alloy of ultimate compression strength 2102MPa.
Embodiment tetra-
By 300 object TiAl 3powder and 500 object Ti powder are 1:2 batching in mass ratio, on mixed powder machine, mixes the powder that obtains mixing for 72 hours; The powder mixing, under 800MPa pressure, is cold-pressed into after base, in vacuum tightness 5 * 10 -2under Pa, enclose low-carbon (LC) steel bushing; Heat-up rate with 50 ℃/min is warming up to 1200 ℃ by the blank of colding pressing with low-carbon (LC) steel bushing, after insulation 30min, puts into mould extrusion molding, makes density 98.5%, average grain size 35 μ m, the TiAl base alloy of ultimate compression strength 2010MPa.
Embodiment five
By 300 object TiAl 3powder and 500 object Ti powder are 1:5 batching in mass ratio, on mixed powder machine, mixes the powder that obtains mixing for 72 hours; The powder mixing, under 800MPa pressure, is cold-pressed into after base, in vacuum tightness 5 * 10 -2under Pa, enclose low-carbon (LC) steel bushing; Heat-up rate with 50 ℃/min is warming up to 1200 ℃ by the blank of colding pressing with low-carbon (LC) steel bushing, after insulation 60min, puts into mould
Extrusion molding, makes density 98%, average grain size 40 μ m, the TiAl base alloy of ultimate compression strength 1717MPa.

Claims (1)

1. a preparation method for TiAl base alloy, is characterized in that preparation method's step is as follows:
1. by 300 object TiAl 3powder and 500 object Ti powder in mass ratio 1:2 ~ 1:5 mix;
2. under 800MPa pressure, be cold-pressed into after base, in vacuum tightness 5 * 10 -2under Pa, enclose low-carbon (LC) steel bushing;
3. with the heat-up rate of 50 ℃/min, the blank of colding pressing with low-carbon (LC) steel bushing is warming up to 1050 ~ 1250 ℃, is incubated after 30 ~ 60min, put into mould extrusion molding.
CN201310555751.5A 2013-11-11 2013-11-11 Preparation method of TiAl-base alloy Pending CN103572085A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201310555751.5A CN103572085A (en) 2013-11-11 2013-11-11 Preparation method of TiAl-base alloy

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201310555751.5A CN103572085A (en) 2013-11-11 2013-11-11 Preparation method of TiAl-base alloy

Publications (1)

Publication Number Publication Date
CN103572085A true CN103572085A (en) 2014-02-12

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107287459A (en) * 2017-05-23 2017-10-24 中国航发北京航空材料研究院 A kind of fine grain titanium aluminium powder forming method

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH06100969A (en) * 1992-09-18 1994-04-12 Toyota Central Res & Dev Lab Inc Production of ti-al intermetallic compound sintered body
JPH07197145A (en) * 1993-12-28 1995-08-01 Toyota Central Res & Dev Lab Inc Production of titanium aluminum base intermetallic compound sintered body
EP0926252A1 (en) * 1997-12-26 1999-06-30 Ishikawajima-Harima Heavy Industries Co., Ltd. Titanium aluminide for precision casting and method of casting titanium aluminide
CN1632148A (en) * 2003-12-24 2005-06-29 中国科学院金属研究所 Method for preparing titanium-aluminum base alloy

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH06100969A (en) * 1992-09-18 1994-04-12 Toyota Central Res & Dev Lab Inc Production of ti-al intermetallic compound sintered body
JPH07197145A (en) * 1993-12-28 1995-08-01 Toyota Central Res & Dev Lab Inc Production of titanium aluminum base intermetallic compound sintered body
EP0926252A1 (en) * 1997-12-26 1999-06-30 Ishikawajima-Harima Heavy Industries Co., Ltd. Titanium aluminide for precision casting and method of casting titanium aluminide
CN1632148A (en) * 2003-12-24 2005-06-29 中国科学院金属研究所 Method for preparing titanium-aluminum base alloy

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107287459A (en) * 2017-05-23 2017-10-24 中国航发北京航空材料研究院 A kind of fine grain titanium aluminium powder forming method

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Application publication date: 20140212