CN86103384A - Permeation process of molybdenum or molybdenum alloy oxidation resistant coating and products thereof - Google Patents
Permeation process of molybdenum or molybdenum alloy oxidation resistant coating and products thereof Download PDFInfo
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- CN86103384A CN86103384A CN86103384.1A CN86103384A CN86103384A CN 86103384 A CN86103384 A CN 86103384A CN 86103384 A CN86103384 A CN 86103384A CN 86103384 A CN86103384 A CN 86103384A
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Abstract
A kind of permeation process that is used for the oxidation resistant coating of molybdenum or molybdenum alloy.It also can be used for niobium or niobium alloy, stainless steel and superalloy.
This coating is by granularity＜300 purpose silica flours, chromium powder, iron powder, or silica flour, chromium powder, vanadium powder, or silica flour, chromium powder, titanium valve and a certain proportion of zapon varnish, vinyl acetic monomer spray on the part of molybdenum or molybdenum alloy after mixing; Drying and vacuum high-temperature thermal treatment diffuse to form.
Present method technology is simple, and the coating of oozing system is even, firm, and anti-glass etch.
Description
A kind of coating of protecting molybdenum or molybdenum alloy high temperature oxidation is oozed system technology.
Generally, the system of oozing of the high-temperature oxidation resistant coating of molybdenum or molybdenum alloy all adopts bag to ooze method or the slip bag oozes method, forms protective coating by solid phase diffusion.See outstanding " high-temperature oxidation resistant coating " (High Temperature Oxidation-Resistant Coatings) books such as G.M.Pound.Bag oozes method, be to be imbedded in the magazine that the metal charge powder is housed by the molybdenum part of the system of oozing under 982～1200 ℃ high temperature, to experience 12～24 hours, even the repeatedly thermal treatment of longer time, between molybdenum part surface and metal charge powder, produce solid phase diffusion and form coating.The slip bag oozes method also just before part is imbedded magazine, is coated with one deck slip on piece surface earlier, and that other technologies and bag ooze method is identical.As seen, these two kinds of technologies are more complicated all, and needs huge magazine and a large amount of material powder so that part is embedded in wherein, these two kinds of methods ooze time of system all very tediously long, power consumption is big, cost is high.And for complex-shaped big parts, the homogeneity of coat-thickness is difficult for guaranteeing the antioxidant property instability.
The objective of the invention is to study simple, the processing ease, with low cost of a kind of technology, molybdenum that antioxidant property is good under the high temperature or molybdenum alloy ooze the method for system coating, to overcome the deficiency of prior art.
The key step of present method is:
At first, preparation coating.
1# coating: composition and weight proportion are:
Material powder: 100 grams.Contain
Silica flour 40～90%
Chromium powder 5～30%
Iron powder 5～30%
Zapon varnish: 10～30 grams
Vinyl acetic monomer: 100～150 milliliters
2# coating: composition and weight proportion are:
Material powder: 100 grams.Contain
Silica flour 40～60%
Chromium powder 20～30%
Vanadium powder 20～30%
Zapon varnish: 10～30 grams
Vinyl acetic monomer: 100～150 milliliters
3# coating: composition and weight proportion are:
Material powder: 100 grams.Contain
Silica flour 60～80%
Chromium powder 20～30%
Titanium valve 5～10%
Zapon varnish: 10～30 grams
Vinyl acetic monomer: 100～150 milliliters
More than the preparation of three kinds of coating material powder also can adopt the metal in the above-mentioned material powder is prefabricated into alloy in proportion, make powder then.The purity of various powder or metal should be higher than 99.9%.The metal or alloy powder particle size should＜300 orders.Each composition is answered thorough mixing during preparation coating.
Then, one of above-mentioned coating is sprayed on the piece surface under the ejection pressure of 0.6～1atm with the spray wheel.
Three, putting into baking oven dries.Temperature is 100～120 ℃, and soaking time is 1 hour.
Four, take out part from baking oven, putting into vacuum tightness is 10
-3-10
-4Carry out high-temperature heat treatment in the vacuum high temperature furnace of mmhg, can feed rare gas element in the stove, as argon gas, furnace temperature should be controlled at the eutectic point that is close to or higher than metal in the material powder, and generally at 1300～1550 ℃, soaking time is 3～30 minutes.
Five, with behind the stove naturally cooling, the system of oozing is finished.
This method of oozing the system coating because coating is molten state, produces liquid-solid phase with matrix and diffuses to form coating, compares with solid-solid phase diffusion, and the reliability and stability of coating improve greatly, and antioxidant property is good.The coating of oozing system in this way can be applied to the various molybdenums of temperature up to 1600 ℃ or electrode, temperature tube, crucible and other molybdenums or the molybdenum alloy goods of molybdenum alloy.This method of oozing the system coating also can be used for niobium or niobium alloy, stainless steel or superalloy.
Fig. 1, Fig. 2 are molybdenum electrode or the molybdenum alloy electrode of the system of oozing after the coating.
Fig. 3, Fig. 4 are the sectional views of Fig. 1, Fig. 2.(1), (3) be coating, (2), (4) are molybdenum electrode matrix or molybdenum alloy electrode matrix.
Embodiment: the system of oozing of molybdenum test piece oxidation resistant coating.
(1) be 99.9% with purity, granularity＜300 purposes, 90 gram silica flours, 5 gram chromium powders, 5 gram iron powders are put into ball grinding cylinder and are mixed.
(2) with 100 above-mentioned material powder of gram and 20 gram zapon varnishs, 120 milliliters of vinyl acetic monomers mix and make slip.
(3) slip evenly is being sprayed in the molybdenum test piece under 0.6～1atm with spraying to swing.
(4) will spray good molybdenum test piece and be placed on baking oven inherence 100
+ 20 ℃Temperature under the oven dry 1 hour.
(5) will dry by the fire good test piece and put into high-temperature vacuum furnace, and make furnace temperature rise to 1300 ℃ and be incubated 30 minutes then from room temperature.
(6) with behind the stove naturally cooling, the system of oozing is finished.
Following test has been carried out in the molybdenum test piece of oozing the system coating more than the process.Test one: molybdenum is the high-temperature oxidation resistance test in air.
The molybdenum test piece that is impregnated with coating is clipped between two electrodes, in air, switches on, make test piece oxidation test temperature reach 1200～1700 ℃.Table one is the high-temperature oxidation resistance of molybdenum protective coating.
Table one:
Test two: the anti-oxidant test of molybdenum protective coating in glass metal.
The corundum crucible internal heating to 1500 that various frits are housed is put in the molybdenum test piece that is impregnated with coating respectively ℃ made glass melting, be incubated 48 hours, take out the test piece that is surrounded by glass after cooling, destroy the glass in the test piece then, check the coating on test piece surface, as seen the gloss of coating is constant, and the surface is intact.Illustrate that this coating has the ability of anti-glass etch, therefore, this coating can be used for the antioxidant defense of various molybdenum parts in the glass melting pond.
Table two is the anti-etch performance of molybdenum protective coating in glass metal.
Table two:
Claims (8)
1, the permeation process of a kind of molybdenum or molybdenum alloy coating.The invention is characterized in that this method includes the following step:
(1) by following composition and weight proportion preparation coating.
Material powder: 100 grams.Contain
Silica flour 40～90%
Chromium powder 5～30%
Iron powder 5～30%
The material powder also can be made prealloy by above composition and proportioning, clays into power then.
Zapon varnish: 10～30 grams
Vinyl acetic monomer: 100～150 milliliters
(2) under the ejection pressure of 0.6～1atm, above-mentioned coating is sprayed on the piece surface.
(3) putting into baking oven dries.
(4) putting into vacuum tightness again is 10
-3～10
-4Carry out high-temperature heat treatment in the vacuum high temperature furnace of mmhg, furnace temperature should be controlled at by near or be higher than the temperature of eutectic point in the material powder.Be incubated 3～30 minutes.
(5) with behind the stove naturally cooling, the system of oozing is finished.
2, the permeation process of a kind of molybdenum or molybdenum alloy coating.The invention is characterized in that this method includes the following step:
(1) by following composition and weight proportion preparation coating.
Material powder: 100 grams.Contain
Silica flour 40～60%
Chromium powder 20～30%
Vanadium powder 20～30%
The material powder also can be made prealloy by above composition and proportioning, clays into power then.
Zapon varnish: 10～30 grams
Vinyl acetic monomer: 100～150 milliliters
(2)～(5) with claim 1 in identical.
3, the permeation process of a kind of molybdenum or molybdenum alloy coating.The invention is characterized in that this method includes the following step:
(1) by following composition and weight proportion preparation coating.
Material powder: 100 grams.Contain
Silica flour 60～80%
Chromium powder 20～30%
Titanium valve 5～10%
The material powder also can be made prealloy by above composition and proportioning, clays into power then.
Zapon varnish: 10～30 grams
Vinyl acetic monomer: 100～150 milliliters.
(2)～(5) with claim 1 in identical.
4, according to claim 1,2 or 3 molybdenum or the permeation process of molybdenum alloy.It is characterized in that the heat treated temperature of high-temperature vacuum is 1300～1550 ℃.
5, according to claim 1,2,3 or 4 molybdenum or the permeation process of molybdenum alloy.The temperature that it is characterized in that oven drying is 100～120 ℃, and soaking time is 1 hour.
6,, it is characterized in that feeding in the high-temperature vacuum heat treatment furnace rare gas element according to claim 1,2,3,4 or 5 permeation process.
7, round bar shape molybdenum that uses in a kind of glass production or molybdenum alloy electrode is characterized in that the surface is oozed to be shaped on 1# coating.
8, plate shape molybdenum electrode of using in a kind of glass production or molybdenum alloy electrode is characterized in that the surface is oozed to be shaped on 1# coating.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 86103384 CN1014617B (en) | 1986-05-16 | 1986-05-16 | Permeation process of preparation of anti-oxidation coating used for molybdenum or its alloy |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 86103384 CN1014617B (en) | 1986-05-16 | 1986-05-16 | Permeation process of preparation of anti-oxidation coating used for molybdenum or its alloy |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN86103384A true CN86103384A (en) | 1987-11-18 |
| CN1014617B CN1014617B (en) | 1991-11-06 |
Family
ID=4802056
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 86103384 Expired CN1014617B (en) | 1986-05-16 | 1986-05-16 | Permeation process of preparation of anti-oxidation coating used for molybdenum or its alloy |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN1014617B (en) |
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN100540744C (en) * | 2007-12-18 | 2009-09-16 | 中南大学 | The preparation method of niobic alloy high temperature antioxidation silicide coating |
| CN101665943B (en) * | 2009-09-25 | 2011-03-23 | 东华大学 | Preparation method of molybdenum and molybdenum alloy surface anti-oxidation coat |
| CN102165087B (en) * | 2008-10-16 | 2013-11-27 | 博格华纳公司 | Group 5 metal source carbide coated steel article and method for making same |
| CN103643201A (en) * | 2014-01-13 | 2014-03-19 | 沈阳建筑大学 | Mo-based Mo+Si+Cr+Fe coating layer composite material and preparation method thereof |
| CN104831231A (en) * | 2015-05-11 | 2015-08-12 | 长安大学 | Method for preparing anti-oxidation permeated layer on surface of molybdenum or molybdenum alloy |
| CN109295412A (en) * | 2018-10-17 | 2019-02-01 | 中国航发航空科技股份有限公司 | A kind of aero-engine high temperature alloy slurry process aluminizing method |
| CN109666886A (en) * | 2018-12-28 | 2019-04-23 | 河南科技大学 | A kind of preparation method of molybdenum base material surface oxidation-resistant coating |
| CN109722665A (en) * | 2018-12-28 | 2019-05-07 | 河南科技大学 | A kind of preparation method of molybdenum base material surface protection coating |
| CN115558831A (en) * | 2022-10-25 | 2023-01-03 | 北京酷捷科技有限公司 | Chromium-molybdenum composite material and preparation method and application thereof |
-
1986
- 1986-05-16 CN CN 86103384 patent/CN1014617B/en not_active Expired
Cited By (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN100540744C (en) * | 2007-12-18 | 2009-09-16 | 中南大学 | The preparation method of niobic alloy high temperature antioxidation silicide coating |
| CN102165087B (en) * | 2008-10-16 | 2013-11-27 | 博格华纳公司 | Group 5 metal source carbide coated steel article and method for making same |
| CN103556109A (en) * | 2008-10-16 | 2014-02-05 | 博格华纳公司 | Group 5 metal source carbide coated steel article and method for making same |
| CN103556109B (en) * | 2008-10-16 | 2016-02-24 | 博格华纳公司 | The steel article of the 5th race's source metal carbide coating and manufacture method thereof |
| CN101665943B (en) * | 2009-09-25 | 2011-03-23 | 东华大学 | Preparation method of molybdenum and molybdenum alloy surface anti-oxidation coat |
| CN103643201A (en) * | 2014-01-13 | 2014-03-19 | 沈阳建筑大学 | Mo-based Mo+Si+Cr+Fe coating layer composite material and preparation method thereof |
| CN104831231A (en) * | 2015-05-11 | 2015-08-12 | 长安大学 | Method for preparing anti-oxidation permeated layer on surface of molybdenum or molybdenum alloy |
| CN109295412A (en) * | 2018-10-17 | 2019-02-01 | 中国航发航空科技股份有限公司 | A kind of aero-engine high temperature alloy slurry process aluminizing method |
| CN109666886A (en) * | 2018-12-28 | 2019-04-23 | 河南科技大学 | A kind of preparation method of molybdenum base material surface oxidation-resistant coating |
| CN109722665A (en) * | 2018-12-28 | 2019-05-07 | 河南科技大学 | A kind of preparation method of molybdenum base material surface protection coating |
| CN115558831A (en) * | 2022-10-25 | 2023-01-03 | 北京酷捷科技有限公司 | Chromium-molybdenum composite material and preparation method and application thereof |
Also Published As
| Publication number | Publication date |
|---|---|
| CN1014617B (en) | 1991-11-06 |
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