CN107917125A - A kind of jointing of non-metal board - Google Patents
A kind of jointing of non-metal board Download PDFInfo
- Publication number
- CN107917125A CN107917125A CN201610886424.1A CN201610886424A CN107917125A CN 107917125 A CN107917125 A CN 107917125A CN 201610886424 A CN201610886424 A CN 201610886424A CN 107917125 A CN107917125 A CN 107917125A
- Authority
- CN
- China
- Prior art keywords
- metal
- pieces
- board
- boards
- jointing
- 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
- 229910052755 nonmetal Inorganic materials 0.000 title claims abstract description 65
- 229910052751 metal Inorganic materials 0.000 claims abstract description 37
- 239000002184 metal Substances 0.000 claims abstract description 37
- 239000002131 composite material Substances 0.000 claims abstract description 18
- 238000010276 construction Methods 0.000 claims abstract description 9
- 239000000463 material Substances 0.000 claims abstract description 9
- 230000003014 reinforcing effect Effects 0.000 claims abstract description 3
- 229920000049 Carbon (fiber) Polymers 0.000 claims description 35
- 239000004917 carbon fiber Substances 0.000 claims description 35
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical group C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 claims description 35
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 claims description 12
- 239000010935 stainless steel Substances 0.000 claims description 11
- 229910001220 stainless steel Inorganic materials 0.000 claims description 11
- 238000005192 partition Methods 0.000 claims description 10
- 229910000679 solder Inorganic materials 0.000 claims description 10
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims description 7
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 claims description 7
- 239000010949 copper Substances 0.000 claims description 7
- 229910052802 copper Inorganic materials 0.000 claims description 7
- 238000005476 soldering Methods 0.000 claims description 7
- 239000010936 titanium Substances 0.000 claims description 7
- 229910052719 titanium Inorganic materials 0.000 claims description 7
- 238000003466 welding Methods 0.000 claims description 6
- 229910052759 nickel Inorganic materials 0.000 claims description 5
- 229910052593 corundum Inorganic materials 0.000 claims description 4
- 239000010431 corundum Substances 0.000 claims description 4
- 239000000203 mixture Substances 0.000 claims description 3
- 229910010271 silicon carbide Inorganic materials 0.000 claims description 3
- 229910045601 alloy Inorganic materials 0.000 claims description 2
- 239000000956 alloy Substances 0.000 claims description 2
- PCHJSUWPFVWCPO-UHFFFAOYSA-N gold Chemical compound [Au] PCHJSUWPFVWCPO-UHFFFAOYSA-N 0.000 claims description 2
- 239000010931 gold Substances 0.000 claims description 2
- 229910052737 gold Inorganic materials 0.000 claims description 2
- 230000000694 effects Effects 0.000 abstract description 4
- 238000009413 insulation Methods 0.000 abstract description 3
- 230000007613 environmental effect Effects 0.000 abstract 1
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 34
- 229910052799 carbon Inorganic materials 0.000 description 33
- 239000000835 fiber Substances 0.000 description 9
- 239000000758 substrate Substances 0.000 description 7
- 238000010438 heat treatment Methods 0.000 description 6
- 238000005219 brazing Methods 0.000 description 5
- 238000000034 method Methods 0.000 description 4
- 230000004048 modification Effects 0.000 description 4
- 238000012986 modification Methods 0.000 description 4
- 229910001069 Ti alloy Inorganic materials 0.000 description 3
- 238000001816 cooling Methods 0.000 description 3
- 230000015572 biosynthetic process Effects 0.000 description 2
- 230000007797 corrosion Effects 0.000 description 2
- 238000005260 corrosion Methods 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 239000011159 matrix material Substances 0.000 description 2
- 238000002844 melting Methods 0.000 description 2
- 230000008018 melting Effects 0.000 description 2
- BQCADISMDOOEFD-UHFFFAOYSA-N Silver Chemical compound [Ag] BQCADISMDOOEFD-UHFFFAOYSA-N 0.000 description 1
- 239000004411 aluminium Substances 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000009792 diffusion process Methods 0.000 description 1
- 230000002708 enhancing effect Effects 0.000 description 1
- 239000011094 fiberboard Substances 0.000 description 1
- 229910002804 graphite Inorganic materials 0.000 description 1
- 239000010439 graphite Substances 0.000 description 1
- 230000017525 heat dissipation Effects 0.000 description 1
- 239000011261 inert gas Substances 0.000 description 1
- 239000007769 metal material Substances 0.000 description 1
- 229910052758 niobium Inorganic materials 0.000 description 1
- 239000010955 niobium Substances 0.000 description 1
- GUCVJGMIXFAOAE-UHFFFAOYSA-N niobium atom Chemical compound [Nb] GUCVJGMIXFAOAE-UHFFFAOYSA-N 0.000 description 1
- 239000003870 refractory metal Substances 0.000 description 1
- 230000000630 rising effect Effects 0.000 description 1
- 229910052709 silver Inorganic materials 0.000 description 1
- 239000004332 silver Substances 0.000 description 1
- 238000005728 strengthening Methods 0.000 description 1
- 238000003786 synthesis reaction Methods 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
- F16B5/00—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them
- F16B5/0004—Joining sheets, plates or panels in abutting relationship
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
- F16B5/00—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them
- F16B5/02—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them by means of fastening members using screw-thread
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16S—CONSTRUCTIONAL ELEMENTS IN GENERAL; STRUCTURES BUILT-UP FROM SUCH ELEMENTS, IN GENERAL
- F16S1/00—Sheets, panels, or other members of similar proportions; Constructions comprising assemblies of such members
- F16S1/02—Sheets, panels, or other members of similar proportions; Constructions comprising assemblies of such members designated for being secured together edge to edge, e.g. at an angle; Assemblies thereof
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B15/00—Layered products comprising a layer of metal
- B32B15/04—Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B15/00—Layered products comprising a layer of metal
- B32B15/18—Layered products comprising a layer of metal comprising iron or steel
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B15/00—Layered products comprising a layer of metal
- B32B15/20—Layered products comprising a layer of metal comprising aluminium or copper
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
- B32B2262/10—Inorganic fibres
- B32B2262/106—Carbon fibres, e.g. graphite fibres
Abstract
A kind of jointing of non-metal board, it is made of two pieces of non-metal boards and the metal layer being located between two pieces of non-metal boards, the metal layer is penetrated into after fusing in the body hole of non-metal board, it is integrally fixed with two pieces of non-metal boards, composite construction is formed, also passes through screw bolt reinforcing between the joint of two pieces of non-metal boards and metal layer.The present invention greatly improves the integral strength of structure strength and stiffness are big, high temperature resistant, the entirety of good heat-insulation effect using can be formed under material less, light, and low to the susceptibility of environmental change, will not be influenced be subject to environment.
Description
Technical field
The present invention relates to composite plate structure field, particularly a kind of jointing of non-metal board.
Background technology
Existing carbon fibre material is due to excellent with high temperature resistant, rapid heat dissipation, low, the corrosion-resistant and light weight of linear expansion coefficient etc.
Point, is widely used in the fields such as space flight, nuclear industry, military affairs.
《Material engineering》Deliver that " carbon fibre composite is connected with metal and joint mechanical property on December 15th, 2007
The text of test " one, mentions and being mentioned in the connection method to the metal such as carbon fibre composite and metallic copper, titanium, niobium, aluminium, such as text
The connection mode of carbon fibre composite and titanium alloy is：First expand on carbon fibre composite surface and ooze, deposit 3 μm of a thickness
Metal gradient layer Ni, makes to form diffusion layer between them, carrys out the modification of the carbon fibre composite surface before butt welding, then redeposited
One layer 2 μm of TC4 titanium alloy layers, take high vacuum technique 2 × 103Under the vacuum of Pa, with silver-based kupper solder at 800 ~ 850 DEG C
At a temperature of heat, the connection of carbon fibre composite and titanium alloy can be achieved after cooling.However, this connection is only reason
To a kind of research method of material on, it is only intended to obtain the good interface of carbon fibre composite and titanium, is not belonging to be molded
Structure, this structure cannot be used for the fields such as building, heating equipment.
The content of the invention
A kind of high temperature resistant is provided the purpose of the present invention is overcoming the above-mentioned deficiency of the prior art, intensity is high, heat-insulated and lead
The jointing of the good non-metal board of thermal effect.
The technical scheme is that：A kind of jointing of non-metal board, by two pieces of non-metal boards and is located in two pieces
Metal layer composition between non-metal board, the metal layer is penetrated into after fusing in the body hole of non-metal board, non-with two pieces
Metallic plate is integrally fixed, and forms composite construction, also passes through bolt between the joint of two pieces of non-metal boards and metal layer
Reinforce.
Advantages of the present invention is：By the sandwiched metal layer between two pieces of non-metal boards, under using material less, light
It can form that strength and stiffness are big, high temperature resistant, the entirety of good heat-insulation effect, greatly improve the integral strength of structure, and to environment
The susceptibility of change is low, will not be influenced be subject to environment.By in the joint of two pieces of non-metal boards by screw bolt reinforcing, into one
Walk reinforced joint at bonding strength so that the junction of two pieces of non-metal boards is not easy to loosen or is broken, especially suitable for high temperature,
Operation under high intensity environment.
Further, the metal layer is penetrated into the body hole of non-metal board by being brazed after fusing.By being brazed into
Type, can make being more uniformly stressed for total, and then improve strength of joint.
Further, the solder used in the soldering uses copper, titanium or nickel metal, and the fusing point of solder is less than the molten of metal layer
Point.In this way, the composite construction of the present invention can be caused first to be melted in hot environment operation and than metal layer, moistening is formed
Surface, enables metal layer rapid melting, equably penetrates into the body hole of non-metal board, so that total stress
It is more uniform.
Further, the joint of the bolt and two pieces of non-metal boards is integral by Welding, so that non-gold
Belong on the basis that plate is reinforced with metal layer, further improve bonding strength.
Further, the material of the metal layer is stainless steel, copper, titanium, nickel or alloy.Metal layer selects dystectic metal
Material so that the three-layer composite board of formation can be used for hot environment under, i.e., in high temperature environments operation when, will not cause metal layer
The phenomenon for producing fusing and causing plate body to loosen occurs, applied widely, and can greatly improve the integral strength of structure.
Further, the bolt exposes the surface of non-metal board, and or sinks to below the surface of non-metal board or and surface
Concordantly.
Further, composite construction heatproof >=1200 DEG C.
Further, the thickness of the joint of two pieces of non-metal boards is more than the thickness of two pieces of non-metal board other positions,
The joint of two pieces of non-metal boards and the other positions of two pieces of non-metal boards form step structure, so as to greatly improve joint
Intensity, prevent to be broken.
Further, one of non-metal board joint in two pieces of non-metal boards is equipped with step so that two pieces non-
Metallic plate is adapted connection in joint, and metal layer is located between the step surface of two pieces of non-metal boards.Due to metal layer sandwiched
It is between the step surface of two pieces of non-metal boards, i.e., L-shaped, it can preferably connect two pieces of non-metal boards so that two pieces are nonmetallic
Loosening will not be produced after plate connection, improves the support strength of joint.
Further, two pieces of non-metal boards are hollow-core construction.In this way, the lightweight of non-metal board and then can be improved.
Further, it is equipped with spaced partition plate in the cavity of the non-metal board.Partition plate cannot be only used for strengthening hollow
The intensity of non-metal board, the passage for being alternatively arranged as conducting heat or cooling down etc..
Further, it is fine can be but not limited to carbon fiber board, carborundum plate, corundum plate or synthesis for two pieces of non-metal boards
Plate is tieed up, is preferably carbon fiber board, since carbon fiber board is using graphite fibre or carbon fiber as enhancing phase, there is high temperature resistant, dissipate
The advantages that hot fast, linear expansion coefficient is low, intensity is high, corrosion-resistant and light weight；In addition, carbon fiber board is easily molded, it is easy to process,
And cost is low, although corundum plate also can high temperature resistant, be not easy to be molded.
Further, the material carbon fiber reinforced carbon matrix composite material of the carbon fiber board.
The jointing of the present invention, since for compound plank frame, modularization, can be used directly, highly practical,
And suitable in the environment of any high-temp and high-strength, such as building, heating equipment field.
Brief description of the drawings
Fig. 1 is the structure diagram of 1 jointing of the embodiment of the present invention；
Fig. 2 is the dimensional structure diagram of 1 carbon of the embodiment of the present invention/carbon plate.
Embodiment
The present invention is described in further details below with reference to Figure of description and specific embodiment.
Embodiment 1
As depicted in figs. 1 and 2：A kind of jointing of non-metal board, carbon/carbon plate is by two pieces of carbon fiber boards 1 and is located in two pieces
Metal layer composition between carbon fiber board 1, metal layer is penetrated into after fusing in the body hole of carbon fiber board 1, with two pieces of carbon fibres
Dimension plate 1 is integrally fixed, and is also reinforced between the joint of two pieces of carbon fiber boards 1 and metal layer by bolt 3.
In the present embodiment, metal layer is preferably stainless steel substrates 2, because stainless steel is refractory metal, in high temperature environments
It is not easy to melt, and stainless steel has the chance rustless characteristic of water, if for building or other fields, can extend using the longevity
Life.The thickness of the joint of two pieces of carbon fiber boards 1 of the present embodiment is more than the thickness of two pieces of carbon fiber board other positions, two pieces of carbon fibres
Tie up the joint of plate 1 and form step structure with the other positions of two pieces of carbon fiber boards；And wherein one in two pieces of carbon fiber boards 1
Block carbon fiber board joint is equipped with step 4, its contact cross-section is L-shaped, and stainless steel substrates 2 are located in the step of two pieces of carbon fiber boards 1
Between face so that stainless steel substrates 2 are also L-shaped, and two pieces of carbon fiber boards 1 are adapted connection in joint.Bolt 3 is fixed on step
Between face.
Overlap after two pieces of 1 sandwiched stainless steel substrates 2 of carbon fiber board, heated by soldering, make the pricker of joint
Material heating fusing, the solder after fusing causes 2 rapid melting of stainless steel substrates, penetrates into the body hole of carbon fiber board 1, to be cooled
Three-layer composite board structure is formed afterwards.Wherein, carbon fiber board 1 is carbon fiber reinforced carbon matrix composite material；Solder is using copper-based.
Bolt 3 and the joint of two pieces of carbon fiber boards 1 are integral by Welding, i.e., solder is injected at bolt hole.
In order to improve the lightweight of carbon fiber board 1, the carbon fiber board 1 of the present embodiment is cored slab, and the sky of carbon fiber board 1
Intracavitary is equipped with spaced partition plate 5, and partition plate 5 is connected with the upper and lower surface of carbon fiber board 1；And carbon fiber board 1 is upper
Surface and the lower surface sandwiched stainless steel substrates 2 between the upper and lower surface of another carbon fiber board 1, and it is whole to be brazed into one respectively
Body, the joint of upper and lower surface are reinforced by bolt 3.Wherein, the bolt 3 of upper surface is dormant bolt, sinks to carbon
The surface of fiberboard 1 and and flush, the bolt 3 of lower surface is plain bolt.
The fusing point of the present embodiment stainless steel substrates 2 is more than 1300 DEG C, available for high-temperature operation.Such as can be by the carbon/carbon plate
As the heated platen in brazing device, temperature during due to soldering work piece is very high, which can be used for clamping to be brazed
Workpiece.The concrete structure of heated platen can be：Including top board and lower platen, and top board and lower platen are the present embodiment
Carbon/the carbon plate, is equipped with heating element in top board and lower platen, and top board can move up and down, and top board is pressed when declining
Tight workpiece to be welded, when rising, unclamp workpiece to be welded.The side arrangement of top board and lower platen has reflecting plate, and reflecting plate presses two
Plate links together, so as to form the welding chamber of closing.When the heating element in top board and lower platen carries out soldering work piece
During heating, add thermogenetic heat dispersed by partition plate so that the surface of workpiece to be welded is heated evenly, and is welded and is connected in chamber
There is pipeline, pipeline can lead to inert gas to welding intracavitary.After to be heated, brazing device had a power failure workpiece is cooled down i.e.
Can.By the temperature tolerance and bearing strength that applied to heated platen, are greatly improved heated platen.
Above-described embodiment is a kind of applicating example to invention carbon/carbon plate, it will thus be seen that carbon/carbon plate of the present invention
With the advantages that high temperature resistant, intensity is high, good heat-insulation effect.Certainly, carbon/carbon plate of the invention can be also used for other field, such as
Building field, the construction etc. for beam, column, floor, it may also be used for the field of other high temperature or high-strength working.
Carbon/the carbon plate of the present embodiment can more than 1200 DEG C of high temperature resistant.
Embodiment 2
Difference lies in the metal layer of the present embodiment is titanium metal plate, and solder is using Ni-based with embodiment 1.
The other the same as in Example 1.
Embodiment 3
Difference lies in the metal layer of the present embodiment is nickel sheet metal, and solder is using copper-based with embodiment 1.
The other the same as in Example 1.
Embodiment 4
Difference lies in one end of partition plate and the lower surface of carbon fiber board connect, and the other end is suspended on carbon fiber board with embodiment 1
Cavity in；And the setting of partition plate is so that the both ends of carbon fiber board are in semi-closed state.
Or illustrated using the brazing device of embodiment 1, the carbon/carbon plate of the present embodiment is used in brazing device
During heated platen, after to be heated, usually brazing device had a power failure workpiece is cooled down, but in order to accelerate cooling velocity,
Cold air can be passed through to the hanging part in partition plate top, further to be cooled down to workpiece, and that part blocked by partition plate can
For gathering heat, prevent heat from distributing, in order to save energy for soldering next time.
The structure of the present embodiment carbon/carbon plate is used for heated platen, can not only greatly improve heated platen temperature tolerance and
Bearing strength, moreover it is possible to save heat and recycled.
Be due to the diaphragm structure of the present embodiment it will be appreciated by those skilled in the art that, not again with other attached drawings into
Row represents.
Embodiment 5
Difference lies in replaced two pieces of carbon fiber boards by two pieces of carborundum plates, the other the same as in Example 1 with embodiment 1.
Embodiment 6
Difference lies in replaced two pieces of carbon fiber boards by two blocks of corundum plates, the other the same as in Example 1 with embodiment 1.
It these are only the preferred embodiment of the present invention, be not intended to limit the invention, it is clear that those skilled in the art can
To carry out various changes, modification without departing from the spirit and scope of the present invention to the present invention.If these modifications to the present invention
Within the scope of belonging to the claims in the present invention and its equivalent technologies with modification, protection scope of the present invention is belonged to.
Claims (10)
- A kind of 1. jointing of non-metal board, it is characterised in that by two pieces of non-metal boards and be located in two pieces of non-metal boards it Between metal layer composition, the metal layer penetrates into the body hole of non-metal board after fusing, fixed with two pieces of non-metal boards Integrally, composite construction is formed, also passes through screw bolt reinforcing between the joint of two pieces of non-metal boards and metal layer.
- 2. the jointing of non-metal board according to claim 1, it is characterised in that the metal layer is by soldering through fusing Penetrate into afterwards in the body hole of non-metal board；Or the solder used in the soldering uses copper, titanium or nickel metal, and solder is molten Fusing point of the point less than metal layer.
- 3. the jointing of non-metal board according to claim 1, it is characterised in that the bolt and two pieces of non-metal boards Joint is integral by Welding.
- 4. the jointing of non-metal board according to claim 1, it is characterised in that the material of the metal layer is stainless Steel, copper, titanium, nickel or alloy.
- 5. according to the jointing of any one of claim 1 ~ 4 non-metal board, it is characterised in that the bolt exposes non-gold Belong to the surface of plate, and or sink to below the surface of non-metal board or and flush.
- 6. according to the jointing of any one of claim 1 ~ 4 non-metal board, it is characterised in that the composite construction heatproof ≥1200℃。
- 7. according to the jointing of any one of claim 1 ~ 4 non-metal board, it is characterised in that two pieces of non-metal boards The thickness of joint be more than the thickness of two pieces of non-metal board other positions, the joint of two pieces of non-metal boards and two pieces it is nonmetallic The other positions of plate form step structure.
- 8. according to the jointing of any one of claim 1 ~ 4 non-metal board, it is characterised in that two pieces of non-metal boards In one of non-metal board joint be equipped with step so that two pieces of non-metal boards are adapted connection, metal layer in joint It is located between the step surface of two pieces of non-metal boards.
- 9. according to the jointing of any one of claim 1 ~ 4 non-metal board, it is characterised in that two pieces of non-metal boards It is hollow-core construction；Or it is equipped with spaced partition plate in the cavity of the non-metal board.
- 10. according to the jointing of any one of claim 1 ~ 4 non-metal board, it is characterised in that described two pieces nonmetallic Plate is carbon fiber board, carborundum plate, corundum plate or pressboard.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610886424.1A CN107917125A (en) | 2016-10-11 | 2016-10-11 | A kind of jointing of non-metal board |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610886424.1A CN107917125A (en) | 2016-10-11 | 2016-10-11 | A kind of jointing of non-metal board |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107917125A true CN107917125A (en) | 2018-04-17 |
Family
ID=61891875
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610886424.1A Pending CN107917125A (en) | 2016-10-11 | 2016-10-11 | A kind of jointing of non-metal board |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107917125A (en) |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101424372A (en) * | 2007-10-23 | 2009-05-06 | 泰勒斯公司 | Structural device for improving the resistance of a structure to heat elongation |
| CN102357694A (en) * | 2011-09-02 | 2012-02-22 | 上海朝日低碳新能源有限公司 | Method for realizing welding of carbon fiber with metal |
| CN103003018A (en) * | 2010-03-16 | 2013-03-27 | 法国原子能及替代能源委员会 | Method of joining parts made of SiC-based materials by non-reactive brazing with addition of a reinforcement, brazing compositions and joint and assembly that are obtained by such a method |
| CN106134320B (en) * | 2010-04-27 | 2013-10-30 | 西安航天动力研究所 | A kind of pottery of soft graphite+soldering combined sealing structure and metal method of attachment |
| CN104175012A (en) * | 2014-08-22 | 2014-12-03 | 奇瑞汽车股份有限公司 | Carbon fiber material and metal material welding method |
| EP2698224B1 (en) * | 2012-08-16 | 2017-03-08 | Helmholtz-Zentrum Geesthacht Zentrum für Material- und Küstenforschung GmbH | Method for the manufacture of a joint between a metal structure and a plastic composite structure |
-
2016
- 2016-10-11 CN CN201610886424.1A patent/CN107917125A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101424372A (en) * | 2007-10-23 | 2009-05-06 | 泰勒斯公司 | Structural device for improving the resistance of a structure to heat elongation |
| CN103003018A (en) * | 2010-03-16 | 2013-03-27 | 法国原子能及替代能源委员会 | Method of joining parts made of SiC-based materials by non-reactive brazing with addition of a reinforcement, brazing compositions and joint and assembly that are obtained by such a method |
| CN106134320B (en) * | 2010-04-27 | 2013-10-30 | 西安航天动力研究所 | A kind of pottery of soft graphite+soldering combined sealing structure and metal method of attachment |
| CN102357694A (en) * | 2011-09-02 | 2012-02-22 | 上海朝日低碳新能源有限公司 | Method for realizing welding of carbon fiber with metal |
| EP2698224B1 (en) * | 2012-08-16 | 2017-03-08 | Helmholtz-Zentrum Geesthacht Zentrum für Material- und Küstenforschung GmbH | Method for the manufacture of a joint between a metal structure and a plastic composite structure |
| CN104175012A (en) * | 2014-08-22 | 2014-12-03 | 奇瑞汽车股份有限公司 | Carbon fiber material and metal material welding method |
Non-Patent Citations (1)
| Title |
|---|
| 王少星: "碳纤维复合材料与金属连接及接头力学性能测试分析", 《科技创新导报》 * |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| Zhan et al. | Comparison between hybrid laser-MIG welding and MIG welding for the invar36 alloy | |
| JP4549473B2 (en) | Method of manufacturing a composite structural member capable of being thermally highly loaded | |
| JP2009192264A (en) | Method for manufacturing high-temperature load equipment for jointing carbon material and copper alloy material metallurgically | |
| JP5302539B2 (en) | Monoblock cooling device components | |
| CN105346161A (en) | Tungsten/transition layer/steel composite material and low-temperature and low-pressure active diffusion connection preparation method thereof | |
| Han et al. | Joining processes of CFRP‐Al sheets in automobile lightweighting technologies: A review | |
| CN101935226B (en) | Process for soldering SiO2f/SiO2 composite ceramic and metal material | |
| KR20100056841A (en) | Joining method between fe-based steel alloys and ti/ti-based alloys having a bonding strength higher than those of base metals by using interlayers | |
| CN106695043A (en) | Carbon base material and copper brazing connection method | |
| CN102689096A (en) | Method for laser-induced self-propagating connection between carbon fiber reinforced aluminum-based composite and metal | |
| CN102689090A (en) | Friction stir welding method for magnesium and aluminum alloy medium plate | |
| AT9173U1 (en) | FIRST WALL COMPONENT WITH RINGSEGMENT | |
| CN104690385A (en) | Composite interlayer and method for brazing metal with ceramic and ceramic matrix composite material by utilizing same | |
| CN105798449A (en) | Method for diffusion connection of high-niobium TiAl alloy by using composite metal foil | |
| CN102643104A (en) | Diffusion bonding method of zirconium diboride-silicon carbide composite material and metal alloy | |
| CN111014867B (en) | Laser brazing method for titanium alloy and ceramic dissimilar materials | |
| CN104074128B (en) | A kind of antitorque assembling composite beam of steel box and manufacture method thereof | |
| CN104085148A (en) | Iron-carbon-chromium-niobium-tungsten-boron alloy system wear-resistant coating and preparation method thereof | |
| CN107914090A (en) | A kind of reinforcement structure of high temperature resistant non-metal board | |
| CN106735668A (en) | A kind of soldering connecting method of W/CuCrZr polings module | |
| CN107917125A (en) | A kind of jointing of non-metal board | |
| CN113085229B (en) | Device and method for repairing layered damage of carbon fiber reinforced thermosetting resin-based composite material | |
| Greuner et al. | Results of high heat flux testing of W/CuCrZr multilayer composites with percolating microstructure for plasma-facing components | |
| CN103406642A (en) | Cold-welding restoring method for tooth surface notches of presser iron-casting press roll shell | |
| CN107488043A (en) | Multilayer complex films, its preparation method and the application as carborundum and its composite connecting material |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20180417 |
|
| RJ01 | Rejection of invention patent application after publication |