CN1948413A - Low heat expansion high temperature adhesion agent - Google Patents
Low heat expansion high temperature adhesion agent Download PDFInfo
- Publication number
- CN1948413A CN1948413A CN 200610145666 CN200610145666A CN1948413A CN 1948413 A CN1948413 A CN 1948413A CN 200610145666 CN200610145666 CN 200610145666 CN 200610145666 A CN200610145666 A CN 200610145666A CN 1948413 A CN1948413 A CN 1948413A
- Authority
- CN
- China
- Prior art keywords
- carbon
- high temperature
- adhesive
- agent
- heat expansion
- 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.)
- Granted
Links
Landscapes
- Adhesives Or Adhesive Processes (AREA)
- Braking Arrangements (AREA)
Abstract
This invention relates to a lower heat expansion high temperature adhesive, and its components ratio is that phosphoric acid: water: aluminium hydroxide: silicon dioxide or French chalinoplasty: carbon fiber powder equals to 5-10ml:1-10ml:0.2-1g:2-10g:0.5-3g. The carbon/carbon composite jobs bonded by this adhesive have high combination intensity, and it can tolerate the change from 900DEG C to room temperature, and also its stickiness point has better anti-oxidation nature.
Description
Technical field
The present invention is a kind of high temperature adhesive of low-thermal-expansion, relates to the bonding technology of low thermal expansion material.
Background technology
Though organic adhesion agent cohesive strength height, non-refractory.So the bonding of high-temperature material generally adopts inorganic adhesive, phosphoric acid salt and waterglass adhesive are the inorganic adhesives that two classes are often used.The very low material of this class thermal expansivity of carbon/carbon composite but they are difficult to bond.
The field of carbon/carbon composite consumption maximum is an aircraft carbon/carbon composite brake flange, compares with powder metallurgy/steel brake facing, and the density of carbon/carbon composite brake flange is low, long service life.The brake flange that when the carbon/carbon composite brake flange wears up to certain thickness, should more renew, for making full use of the charcoal/carbon/carbon brake disc that reaches wear limit thickness, the brake disc bonding of thinner thickness can be reused together, greatly reduce production cost like this, and can satisfy the requirement of aircraft brake again.Enough bonding strengths should be arranged charcoal/carbon/carbon brake disc after the bonding so that following process, and especially (anti-oxidation thermal treatment temp is sometimes up to 900 ℃) do not ftracture in anti-oxidation heat treatment process.The organic adhesion agent use temperature is low, is difficult to above 700 ℃; The common inorganic adhesive coefficient of expansion and the coefficient of expansion difference of carbon/carbon composite are big, are difficult to bear thermal shocking.
Chinese patent CN162344A, denomination of invention: the carbon/carbon compound material brake disc bonding process, a kind of binding agent that is mixed with by resol, norbide, silicon-dioxide, silica flour, boron trioxide has been proposed, can stand high cryogenic thermal shocking.But the processing to synvaren not only needs to be heated to higher temperature, and needs pressurization in treating processes.Resol has adverse influence to environment, workmen in the brushing process, and at high temperature still discharges deleterious gas.
Summary of the invention
The present invention designs the high temperature adhesive that a kind of low-thermal-expansion is provided at problems of the prior art just, its objective is and guarantee bonded workpiece at high low temperature circulation time that room temperature to 900 ℃ still has good viscosifying power.And can not produce irritant gas, guarantee good operating environment, and this adhesive solidification treatment temp low (200～300 ℃), do not need special pressure exerting device.
The objective of the invention is to be achieved through the following technical solutions:
The high temperature adhesive of this kind low-thermal-expansion, its composition and proportioning are: phosphoric acid: water: aluminium hydroxide: silicon-dioxide or Magnesium Silicate q-agent: charcoal fiber dust=5～10mi: 1～10ml: 0.2～1g: 2～10g: 0.5～3g.
The described high temperature adhesive of technical solution of the present invention is a kind of phosphate adhesive of modification, be characterized in having added in common phosphate adhesive charcoal fiber dust and silicon-dioxide or Magnesium Silicate q-agent powder, its effect is to guarantee that bonded low-thermal-expansion workpiece ℃ still has good viscosifying power from room temperature to 900.
It is in order to reduce the thermal expansivity of high-temp glue, to make it the thermal expansivity near bonded workpiece such as carbon/carbon composite that this kind tackiness agent adds the charcoal fiber dust.The adding of silicon-dioxide (or Magnesium Silicate q-agent) powder is in order to improve the cohesive strength of workpiece.
Solidify after this kind tackiness agent can bond at ambient temperature, solidification value is 200-300 ℃ again, and in 1～5 hour treatment time, lacked set time when temperature was high, and set time was long when temperature was low.
Embodiment
The composition and the proportioning of this high temperature adhesive are: phosphoric acid: water: aluminium hydroxide: silicon-dioxide or Magnesium Silicate q-agent: charcoal fiber dust=10ml: 2ml: 0.5g: 4g: 1g.
When the above-mentioned high temperature adhesive of preparation, earlier aluminium hydroxide is dissolved in the phosphoric acid fully, phosphoric acid adopts 85% phosphoric acid, needs to be heated to about 140 ℃ in this process, and aluminium hydroxide is transparence liquid after dissolving in phosphoric acid fully.In the solution with pulverous silicon-dioxide or Magnesium Silicate q-agent and charcoal fiber dust adding phosphoric acid and aluminium hydroxide, can use after stirring then.
The powder that the charcoal fiber dust produces in the time of can using carbon/carbon composite mechanical workout leaches thinner powder through screening and gets final product; Also can pulverize by carbon/carbon composite, ball milling obtains; Also can grind use by the charcoal felt.
Usually the tackiness agent viscosity that makes is unfavorable for depositing and constructing of tackiness agent too greatly, can add an amount of water and adjust viscosity, the prolonged preservation with tackiness agent of being convenient to construct.
With the above-mentioned adhesive bonds carbon/carbon composite goods that prepare, it is of a size of 18mm * 18mm * 18mm, is cured processing afterwards, and the solidification treatment temperature is 250 ℃, soaking time 2 hours.
Carbon/carbon composite bonded product after above-mentioned processing, 900 ℃ were heated back 1 hour in air, were cooled to room temperature rapidly and still combined, and still had quite high bonding strength.
Claims (2)
1. the high temperature adhesive of a low-thermal-expansion, it is characterized in that: the composition and the proportioning of this tackiness agent are:
Phosphoric acid: water: aluminium hydroxide: silicon-dioxide or Magnesium Silicate q-agent: charcoal fiber dust=5～10ml: 1～10ml: 0.2～1g: 2～10g: 0.5～3g.
2. the high temperature adhesive of low-thermal-expansion according to claim 1, it is characterized in that: the composition and the proportioning of this tackiness agent are:
Phosphoric acid: water: aluminium hydroxide: silicon-dioxide or Magnesium Silicate q-agent: charcoal fiber dust=10ml: 2ml: 0.5g: 4g: 1g.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNB2006101456661A CN100410342C (en) | 2006-11-24 | 2006-11-24 | Low heat expansion high temperature adhesion agent |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNB2006101456661A CN100410342C (en) | 2006-11-24 | 2006-11-24 | Low heat expansion high temperature adhesion agent |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN1948413A true CN1948413A (en) | 2007-04-18 |
| CN100410342C CN100410342C (en) | 2008-08-13 |
Family
ID=38018040
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CNB2006101456661A Active CN100410342C (en) | 2006-11-24 | 2006-11-24 | Low heat expansion high temperature adhesion agent |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN100410342C (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101760176B (en) * | 2010-01-22 | 2011-02-16 | 侯永忠 | Coke oven sealant prepared by fly ash and preparation method and application thereof |
Family Cites Families (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2722185B1 (en) * | 1994-07-07 | 1996-09-27 | Rhone Poulenc Chimie | CONCENTRATED SUSPENSION OF PRECIPITATION SILICA, METHODS FOR THE PREPARATION THEREOF, AND USES THEREOF |
| CN1120059A (en) * | 1994-09-16 | 1996-04-10 | 淄博市新材料研究所 | Inorganic binder and its preparation method and usage |
-
2006
- 2006-11-24 CN CNB2006101456661A patent/CN100410342C/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101760176B (en) * | 2010-01-22 | 2011-02-16 | 侯永忠 | Coke oven sealant prepared by fly ash and preparation method and application thereof |
Also Published As
| Publication number | Publication date |
|---|---|
| CN100410342C (en) | 2008-08-13 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN102814759B (en) | A kind of diamond-resin grinding wheel and preparation method thereof | |
| CN101307212B (en) | High temperature resistant inorganic adhesive | |
| CN102814747B (en) | A kind of CBN resin wheel and preparation method thereof | |
| CN102399522B (en) | Organic/inorganic composite adhesive | |
| CN101417315A (en) | Phosphate binder for casting | |
| CN102674871A (en) | Low-temperature high-strength ceramic bond and preparation method thereof | |
| CN107686704A (en) | A kind of composite artificial board adhesive | |
| CN100410342C (en) | Low heat expansion high temperature adhesion agent | |
| CN102814761B (en) | A kind of white fused alumina resin wheel and preparation method thereof | |
| CN103465178A (en) | Ceramic organic composite binder for cubic boron nitride grinding wheels | |
| CN102634320B (en) | Material of high-wear-resistance ceramic automobile brake block and preparation method thereof | |
| CN102814757B (en) | A kind of pink fused alumina resin wheel and preparation method thereof | |
| CN110509193A (en) | A kind of universal joint alley mill preparation method of nano-grade ceramic binding agent | |
| CN109015420A (en) | A kind of measuring tool processing grinding abrasive disk | |
| CN108838909B (en) | Ceramic superhard grinding wheel for grinding double end faces of stainless steel product and preparation method thereof | |
| CN106346375B (en) | Ceramic Composite bonding agent and its cubic boron nitride abrasive wheel and preparation method for cubic boron nitride abrasive wheel | |
| CN103042475B (en) | Stainless steel and titanium alloy screen cloth matrix ceramic grinding wheel for grinding | |
| CN105199285A (en) | Toughened cyanoacrylate composition | |
| CN110005735A (en) | A kind of high-speed train braking friction block and preparation method thereof | |
| CN103056785A (en) | Method for preparing vitrified grinding wheels with metal matrixes for grinding stainless steel and titanium alloys | |
| CN103042473B (en) | Screen cloth matrix ceramic grinding wheel used for grinding stone, glass or tungsten-molybdenum alloy | |
| CN108747857B (en) | High-speed self-sharpening CBN grinding wheel for machining unbquenched alloy steel workpiece and preparation method thereof | |
| CN1058978A (en) | The high temperature resistant inorganic composite adhesive | |
| CN110387107A (en) | A kind of preparation method of magnetic abrasive grain | |
| CN103880332A (en) | Preparation and use method of heating curing type wear-resistant composite ceramic coating |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| ASS | Succession or assignment of patent right |
Owner name: BEIJING BAIMTEC MATERIAL CO., LTD. Free format text: FORMER OWNER: BEIJING BAIMU AERONAUTIC MATERIAL HIGH-TECHNOLOGY CO., LTD. Effective date: 20150121 |
|
| C41 | Transfer of patent application or patent right or utility model | ||
| COR | Change of bibliographic data |
Free format text: CORRECT: ADDRESS; FROM: 100095 HAIDIAN, BEIJING TO: 100000 HAIDIAN, BEIJING |
|
| TR01 | Transfer of patent right |
Effective date of registration: 20150121 Address after: 100000 Beijing city Haidian District Yongxiang Road No. 5 Building 1 room 206 2 Patentee after: BEIJING YOUCAI BAIMU AVIATION EQUIPMENT CO., LTD. Address before: 100095 box 81, box 63, Beijing Patentee before: Beijing Baimu Aeronautic Material High-Technology Co., Ltd. |