CN107009687A - A kind of combined sleeve and manufacture method and with shaft sleeve and manufacture method - Google Patents
A kind of combined sleeve and manufacture method and with shaft sleeve and manufacture method Download PDFInfo
- Publication number
- CN107009687A CN107009687A CN201710141267.6A CN201710141267A CN107009687A CN 107009687 A CN107009687 A CN 107009687A CN 201710141267 A CN201710141267 A CN 201710141267A CN 107009687 A CN107009687 A CN 107009687A
- Authority
- CN
- China
- Prior art keywords
- sleeve
- layer
- combined
- combined sleeve
- plug
- 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
- 238000000034 method Methods 0.000 title claims abstract description 27
- 238000004519 manufacturing process Methods 0.000 title claims abstract description 23
- 229920000049 Carbon (fiber) Polymers 0.000 claims abstract description 28
- 239000004917 carbon fiber Substances 0.000 claims abstract description 28
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 claims abstract description 28
- 239000003365 glass fiber Substances 0.000 claims abstract description 24
- 229910052751 metal Inorganic materials 0.000 claims abstract description 22
- 239000002184 metal Substances 0.000 claims abstract description 22
- 239000000806 elastomer Substances 0.000 claims abstract description 19
- 229920001971 elastomer Polymers 0.000 claims abstract description 19
- 239000000919 ceramic Substances 0.000 claims abstract description 17
- 239000011152 fibreglass Substances 0.000 claims abstract description 17
- 229920002430 Fibre-reinforced plastic Polymers 0.000 claims abstract description 15
- 230000015572 biosynthetic process Effects 0.000 claims abstract description 13
- 239000000463 material Substances 0.000 claims abstract description 9
- 238000013022 venting Methods 0.000 claims abstract description 4
- 239000011521 glass Substances 0.000 claims description 8
- 239000007921 spray Substances 0.000 claims description 7
- 238000005507 spraying Methods 0.000 claims description 7
- 229910000831 Steel Inorganic materials 0.000 claims description 6
- 102000004142 Trypsin Human genes 0.000 claims description 6
- 108090000631 Trypsin Proteins 0.000 claims description 6
- 239000010959 steel Substances 0.000 claims description 6
- 239000012588 trypsin Substances 0.000 claims description 6
- 239000000956 alloy Substances 0.000 claims description 5
- 229910052574 oxide ceramic Inorganic materials 0.000 claims description 5
- 239000011224 oxide ceramic Substances 0.000 claims description 5
- 229920000742 Cotton Polymers 0.000 claims description 4
- 229910045601 alloy Inorganic materials 0.000 claims description 4
- 239000011230 binding agent Substances 0.000 claims description 3
- 239000013536 elastomeric material Substances 0.000 claims description 3
- 238000003780 insertion Methods 0.000 claims description 3
- 230000037431 insertion Effects 0.000 claims description 3
- TWNQGVIAIRXVLR-UHFFFAOYSA-N oxo(oxoalumanyloxy)alumane Chemical compound O=[Al]O[Al]=O TWNQGVIAIRXVLR-UHFFFAOYSA-N 0.000 claims description 3
- 238000005498 polishing Methods 0.000 claims description 3
- 239000000843 powder Substances 0.000 claims description 3
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 claims 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 claims 1
- 229910052804 chromium Inorganic materials 0.000 claims 1
- 239000011651 chromium Substances 0.000 claims 1
- 238000007648 laser printing Methods 0.000 claims 1
- 229910052760 oxygen Inorganic materials 0.000 claims 1
- 239000001301 oxygen Substances 0.000 claims 1
- UONOETXJSWQNOL-UHFFFAOYSA-N tungsten carbide Chemical compound [W+]#[C-] UONOETXJSWQNOL-UHFFFAOYSA-N 0.000 claims 1
- 238000010586 diagram Methods 0.000 description 5
- 230000005540 biological transmission Effects 0.000 description 3
- 238000000576 coating method Methods 0.000 description 3
- 238000007639 printing Methods 0.000 description 3
- 230000003014 reinforcing effect Effects 0.000 description 3
- 241001080061 Talides Species 0.000 description 2
- WGLPBDUCMAPZCE-UHFFFAOYSA-N Trioxochromium Chemical compound O=[Cr](=O)=O WGLPBDUCMAPZCE-UHFFFAOYSA-N 0.000 description 2
- 239000003795 chemical substances by application Substances 0.000 description 2
- 229910000423 chromium oxide Inorganic materials 0.000 description 2
- 238000004891 communication Methods 0.000 description 2
- 230000008602 contraction Effects 0.000 description 2
- 239000004744 fabric Substances 0.000 description 2
- 238000007751 thermal spraying Methods 0.000 description 2
- 229910000838 Al alloy Inorganic materials 0.000 description 1
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 229910010293 ceramic material Inorganic materials 0.000 description 1
- 239000011248 coating agent Substances 0.000 description 1
- 238000010288 cold spraying Methods 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005265 energy consumption Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000003628 erosive effect Effects 0.000 description 1
- 239000000945 filler Substances 0.000 description 1
- PCHJSUWPFVWCPO-UHFFFAOYSA-N gold Chemical compound [Au] PCHJSUWPFVWCPO-UHFFFAOYSA-N 0.000 description 1
- 239000010931 gold Substances 0.000 description 1
- 229910052737 gold Inorganic materials 0.000 description 1
- 238000010147 laser engraving Methods 0.000 description 1
- 239000007769 metal material Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000007747 plating Methods 0.000 description 1
- 229910052573 porcelain Inorganic materials 0.000 description 1
- 239000002994 raw material Substances 0.000 description 1
- 238000004513 sizing Methods 0.000 description 1
- 238000003860 storage Methods 0.000 description 1
Classifications
-
- 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
- B32B1/00—Layered products having a non-planar shape
- B32B1/08—Tubular products
-
- 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
- B32B17/00—Layered products essentially comprising sheet glass, or glass, slag, or like fibres
- B32B17/06—Layered products essentially comprising sheet glass, or glass, slag, or like fibres comprising glass as the main or only constituent of a layer, next to another layer of a specific 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
- B32B17/00—Layered products essentially comprising sheet glass, or glass, slag, or like fibres
- B32B17/06—Layered products essentially comprising sheet glass, or glass, slag, or like fibres comprising glass as the main or only constituent of a layer, next to another layer of a specific material
- B32B17/067—Layered products essentially comprising sheet glass, or glass, slag, or like fibres comprising glass as the main or only constituent of a layer, next to another layer of a specific material of fibres or filaments
-
- 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
- B32B33/00—Layered products characterised by particular properties or particular surface features, e.g. particular surface coatings; Layered products designed for particular purposes not covered by another single class
-
- 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
- B32B37/00—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
- B32B37/02—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by a sequence of laminating steps, e.g. by adding new layers at consecutive laminating stations
-
- 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
- B32B38/00—Ancillary operations in connection with laminating processes
-
- 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
- B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
- B32B5/02—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer
-
- 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
- B32B9/00—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00
- B32B9/005—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00 comprising one layer of ceramic material, e.g. porcelain, ceramic tile
-
- 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
- B32B9/00—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00
- B32B9/005—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00 comprising one layer of ceramic material, e.g. porcelain, ceramic tile
- B32B9/007—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00 comprising one layer of ceramic material, e.g. porcelain, ceramic tile comprising carbon, e.g. graphite, composite carbon
-
- 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
- B32B9/00—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00
- B32B9/04—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00 comprising such particular substance as the main or only constituent of a layer, which is next to another layer of the same or of a different material
- B32B9/047—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00 comprising such particular substance as the main or only constituent of a layer, which is next to another layer of the same or of a different material made of fibres or filaments
-
- 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
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C13/00—Rolls, drums, discs, or the like; Bearings or mountings therefor
-
- 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
- B32B2255/00—Coating on the layer surface
- B32B2255/02—Coating on the layer surface on fibrous or filamentary layer
-
- 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
- B32B2255/00—Coating on the layer surface
- B32B2255/20—Inorganic coating
- B32B2255/205—Metallic coating
-
- 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
- B32B2262/101—Glass fibres
-
- 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
- B32B2307/00—Properties of the layers or laminate
- B32B2307/50—Properties of the layers or laminate having particular mechanical properties
- B32B2307/536—Hardness
-
- 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
- B32B2307/00—Properties of the layers or laminate
- B32B2307/50—Properties of the layers or laminate having particular mechanical properties
- B32B2307/554—Wear resistance
-
- 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
- B32B2307/00—Properties of the layers or laminate
- B32B2307/50—Properties of the layers or laminate having particular mechanical properties
- B32B2307/558—Impact strength, toughness
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C29/00—Alloys based on carbides, oxides, nitrides, borides, or silicides, e.g. cermets, or other metal compounds, e.g. oxynitrides, sulfides
- C22C29/02—Alloys based on carbides, oxides, nitrides, borides, or silicides, e.g. cermets, or other metal compounds, e.g. oxynitrides, sulfides based on carbides or carbonitrides
- C22C29/06—Alloys based on carbides, oxides, nitrides, borides, or silicides, e.g. cermets, or other metal compounds, e.g. oxynitrides, sulfides based on carbides or carbonitrides based on carbides, but not containing other metal compounds
- C22C29/08—Alloys based on carbides, oxides, nitrides, borides, or silicides, e.g. cermets, or other metal compounds, e.g. oxynitrides, sulfides based on carbides or carbonitrides based on carbides, but not containing other metal compounds based on tungsten carbide
-
- 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
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C2206/00—Materials with ceramics, cermets, hard carbon or similar non-metallic hard materials as main constituents
- F16C2206/40—Ceramics, e.g. carbides, nitrides, oxides, borides of a metal
- F16C2206/42—Ceramics, e.g. carbides, nitrides, oxides, borides of a metal based on ceramic oxides
-
- 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
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C2206/00—Materials with ceramics, cermets, hard carbon or similar non-metallic hard materials as main constituents
- F16C2206/40—Ceramics, e.g. carbides, nitrides, oxides, borides of a metal
- F16C2206/42—Ceramics, e.g. carbides, nitrides, oxides, borides of a metal based on ceramic oxides
- F16C2206/44—Ceramics, e.g. carbides, nitrides, oxides, borides of a metal based on ceramic oxides based on aluminium oxide (Al2O3)
-
- 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
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C2208/00—Plastics; Synthetic resins, e.g. rubbers
- F16C2208/10—Elastomers; Rubbers
-
- 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
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C2220/00—Shaping
- F16C2220/28—Shaping by winding impregnated fibres
-
- 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
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C2223/00—Surface treatments; Hardening; Coating
- F16C2223/02—Mechanical treatment, e.g. finishing
-
- 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
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C2223/00—Surface treatments; Hardening; Coating
- F16C2223/02—Mechanical treatment, e.g. finishing
- F16C2223/06—Mechanical treatment, e.g. finishing polishing
-
- 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
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C2223/00—Surface treatments; Hardening; Coating
- F16C2223/30—Coating surfaces
- F16C2223/42—Coating surfaces by spraying the coating material, e.g. plasma spraying
-
- 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
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C2226/00—Joining parts; Fastening; Assembling or mounting parts
- F16C2226/10—Force connections, e.g. clamping
- F16C2226/14—Force connections, e.g. clamping by shrink fit, i.e. heating and shrinking part to allow assembly
Landscapes
- Engineering & Computer Science (AREA)
- Ceramic Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Laminated Bodies (AREA)
Abstract
The present invention relates to a kind of combined sleeve and manufacture method and with shaft sleeve and manufacture method, combined sleeve is followed successively by jacket layer in fiberglass, elastomer layer, glass fibre reinforced plastic structure layer, carbon fiber structural back-up coat, metal bonding layer and ceramics work top layer from the inside to the outside, and combined sleeve gapless, which is fitted tightly on sleeve plug, forms band shaft sleeve.Manufacture method with shaft sleeve comprises the following steps：Compressed air is passed through so that the inwall expansion of combined sleeve, combined sleeve set is attached on sleeve plug into sleeve plug by air admission hole；Venting compressed air, gapless is fitted tightly over the roller outer surface formation integrative-structure of sleeve plug after the inside resilience of combined sleeve.The combined sleeve of the present invention is from heavy and light, intensity, rigidity and good toughness, and thickness is not by pipe profile specification limit system, and material and manufacturing cost are low, and easy to loading and unloading quick between sleeve plug.
Description
Technical field
The present invention relates to a kind of sleeve, more particularly to a kind of combined sleeve and manufacture method and with shaft sleeve and manufacturer
Method.
Background technology
(7) as shown in Figure 1 are made the roller body of conventional belt beaming roller cylinder of steel pipe or aluminium-alloy pipe section bar, then in roller
Plating or thermal spraying hard metal or ceramic material on surface (be made behind 8) as shown in Figure 1 metal or ceramic roll surface guiding (or
Conduction, transmission) tape spool roller.
Its shortcoming is：The big roller of external diameter is from weight weight, and machine high energy consumption, the roller efficiency of loading and unloading is low, and product is advised
Lattice are various, using the pipe profile of the existing specification of in the market, and the product of some specifications is difficult the pipe profile for finding matching, and raw material are damaged
Consumption is big, and costs of manufacturing and transportation is high, and storage floor space is big.
The content of the invention
The technical problems to be solved by the invention are to provide a kind of combined sleeve and manufacture method, from heavy and light, intensity, rigidity
And good toughness, thickness is not by pipe profile specification limit system, and handling are quick, and material and manufacturing cost are low.
The technical solution adopted for the present invention to solve the technical problems is to provide a kind of combined sleeve, during the combined sleeve is in
Hollow round column shape, the combined sleeve is followed successively by jacket layer in fiberglass, elastomer layer, glass fibre reinforced plastic structure layer, carbon fiber from the inside to the outside
Fabric reinforcing layer, metal bonding layer and ceramics work top layer.
Another technical scheme that its technical problem of present invention solution is used is to provide a kind of manufacture of above-mentioned combined sleeve
Method, comprises the following steps：
(1) jacket layer in coiling fiberglass：By die mandrel coiling glass fibre cotton yarn tape and solidify, jacket layer list in fiberglass
Side 0.7~1.7mm of thickness；
(2) coiling elastomer layer：Jacket layer outer wrap elastomeric material formation elastomer layer, elasticity in fiberglass after hardening
1~2mm of body layer one-sided thickness；
(3) coiling glass fibre reinforced plastic structure layer：Coiling glass fiber tape or glass fiber formation glass outside elastomer layer
Steel structural layer；
(4) coiling carbon fiber structural back-up coat：Reinforced in the outer coiling carbon fiber formation carbon fiber structural of glass fibre reinforced plastic structure layer
Layer；
(5) spray metal binder course：In carbon fiber structural back-up coat trypsin method point molten metal formation metal bonding layer；
(6) ceramic coated work top layer：Ceramics work top layer is formed in metal bonding layer trypsin method ceramic powder；
(7) outer surface to combined sleeve polished, polishing.
As the further improvement to above-mentioned embodiment, the sprayed on material of the step (6) is oxide ceramics or conjunction
Gold.
As the further improvement to above-mentioned embodiment, the oxide ceramics is chromium oxide or aluminum oxide.
As the further improvement to above-mentioned embodiment, the alloy is Talide.
Another technical problem to be solved by this invention is to provide a kind of band shaft sleeve and manufacture method, easy to loading and unloading.
The technical solution adopted for the present invention to solve the technical problems is to provide a kind of band using above-mentioned combined sleeve
Shaft sleeve, including sleeve plug, the sleeve plug include the roller support of roller and the left and right sides, a side of the sleeve plug
The air admission hole connected with middle cavity is provided with the roller support in face, the roller support of another side of the sleeve plug is internal to be provided with
The outlet passageway inside the venthole of some inside and outside insertions, the roller support is provided with the outlet passageway of cavity connection, the roller
It is in communication with the outside by the venthole on roller, the combined sleeve gapless is fitted tightly over the roller appearance of sleeve plug
Face.
As the further improvement to above-mentioned embodiment, the outer surface of the combined sleeve passes through laser engraving decorative pattern figure
Printing sleeve is made in case.
Another technical scheme that its technical problem of present invention solution is used is to provide a kind of manufacture of above-mentioned coaxial sleeve
Method, comprises the following steps：
(1) compressed air is passed through into sleeve plug by air admission hole so that the inwall expansion of combined sleeve, combined sleeve
Set is attached on sleeve plug；
(2) venting compressed air, gapless is fitted tightly over the roller appearance of sleeve plug after the inside resilience of combined sleeve
Face forms integrative-structure.
Beneficial effect
In the combined sleeve of the present invention, jacket layer has certain elasticity tension in fiberglass, with compressible resilience
Elastomer layer can in heat absorbing glass steel jacket layer expansion and contraction, middle glass fibre reinforced plastic structure layer is used as agent structure layer branch
Intensity, rigidity and the toughness of support set cylinder, carbon fiber structural back-up coat have very small thermal coefficient of expansion as supplementary structure, made
Glass fibre reinforced plastic structure layer is reinforced by the compressing of carbon fiber when heated, temperature can only inwardly expand when raising, and it expands change
Shape amount is absorbed by elastomer layer, and the thermal coefficient of expansion of carbon fiber is minimum, it is adaptable to which carbon fiber and metal make this by spraying coating process
Two kinds of materials are combined well, the characteristics of metal bonding layer has again and the good spraying of ceramics is combined, ceramics work top layer conduct
The characteristics of working lining has hard, wear-resisting.The combined sleeve of the present invention is from heavy and light, and intensity, rigidity and good toughness, thickness is not managed
Section bar specification is limited, and material and manufacturing cost are low, and easy to loading and unloading quick between sleeve plug.
Brief description of the drawings
Fig. 1 is the structural representation of existing tape spool roller.
Fig. 2 is the vertical section structure schematic diagram of combined sleeve of the present invention.
Fig. 3 is the cross-sectional configuration schematic diagram of combined sleeve of the present invention.
The mplifying structure schematic diagram that Fig. 4 is J in Fig. 3.
Fig. 5 is the vertical section structure schematic diagram of sleeve plug of the present invention.
Fig. 6 is the vertical section structure schematic diagram of the invention with shaft sleeve.
Embodiment
With reference to specific embodiment, the present invention is expanded on further.It should be understood that these embodiments are merely to illustrate the present invention
Rather than limitation the scope of the present invention.In addition, it is to be understood that after the content of the invention lectured has been read, people in the art
Member can make various changes or modifications to the present invention, and these equivalent form of values equally fall within the application appended claims and limited
Scope.
A kind of combined sleeve as in Figure 2-4, the combined sleeve is in hollow cylindrical, and combined sleeve is from the inside to the outside successively
For jacket layer in fiberglass 1, elastomer layer 2, glass fibre reinforced plastic structure layer 3, carbon fiber structural back-up coat 4, metal bonding layer 5 and potter
Make top layer 6.
Jacket layer 1 has certain elasticity tension in fiberglass, and glass can be absorbed with compressible elastic elastomer layer 2
The expansion and contraction of jacket layer 1 in glass steel.Middle glass fibre reinforced plastic structure layer 3 as agent structure layer stop sleeve intensity, rigidity
And toughness, its wall thickness sets according to sleeve outer diameter.As supplementary structure layer, its main function is to reinforce to carbon fiber structural back-up coat 4
Glass fibre reinforced plastic structure layer 3, because fiberglass has larger thermal coefficient of expansion (fiberglass thermal coefficient of expansion：2.7~7.2 × 10-6/
DEG C), and carbon fiber has very small thermal coefficient of expansion (the carbon fiber thermal coefficient of expansion：0.7×10-6/ DEG C) characteristic, it is fine by carbon
Dimension fabric reinforcing layer 4 is reinforced, in thermal spraying (Thermal Spray) or cold spraying (Gas Dynamic Spray/Gas
Daynamic Cold Spray) (hereinafter referred to as：Spraying) when glass fibre reinforced plastic structure layer 3 by carbon fiber structural back-up coat 4 reinforcing
Compressing, temperature can only inwardly be expanded when raising, and its dilatancy amount is absorbed by elastomer layer 2.The thermal coefficient of expansion pole of carbon fiber
It is small, it is adaptable to which that carbon fiber and metal make two kinds of materials combine well by spraying coating process, and metal bonding layer 5 has and made pottery again
Porcelain well sprays the characteristics of combining.The characteristics of ceramics work top layer 6 has hard, wear-resisting as working lining.
A kind of manufacture method of combined sleeve is provided below, comprises the following steps：
(1) jacket layer 1 in coiling fiberglass：By die mandrel coiling glass fibre cotton yarn tape, its cotton yarn tape around controlling angle root
Determined according to sleeve diameter size, the 0.7~1.7mm of one-sided thickness of jacket layer 1 in fiberglass, and carry out curing process.
(2) coiling elastomer layer 2：The outer wrap elastomeric material of jacket layer 1 formation elastomer layer 2 in fiberglass after hardening,
1~2mm of elastomer layer one-sided thickness.
(3) coiling glass fibre reinforced plastic structure layer 3：In the outer coiling glass fiber tape of elastomer layer 2 or glass fiber formation glass
Glass steel structural layer 3, depending on its coiling thickness is according to roller diameter size.
(4) coiling carbon fiber structural back-up coat 4：Add in the outer coiling carbon fiber formation carbon fiber structural of glass fibre reinforced plastic structure layer 3
One of Gu layer 4, the one-sided thickness of carbon fiber structural back-up coat 4 is determined according to sleeve diameter and length, and it is acted on：Strengthen tube-in-tube structure
Rigidity and intensity, the two of effect：Because the carbon fiber thermal coefficient of expansion is minimum, with the preferable associativity of spraying metal materials.
(5) spray metal binder course 5：In the trypsin method point molten metal of carbon fiber structural back-up coat 4 formation metal bonding layer
5。
(6) ceramic coated work top layer 6：Ceramics work top layer 6, spraying are formed in the trypsin method ceramic powder of metal bonding layer 5
Material be oxide ceramics (for example：Chromium oxide or aluminum oxide) or other alloy materials are (for example：Talide), ceramics
The work one-sided thickness of top layer 6 is determined according to different product requirement.
(7) outer surface to combined sleeve polished, polishing.
A kind of band shaft sleeve using above-mentioned combined sleeve as shown in Figure 5 and Figure 6, including sleeve plug 9, cover tube filler
Rod 9 includes the roller support 902 of roller 901 and the left and right sides.It is provided with and middle cavity in the roller support 902 of one side of sleeve plug 9
The outlet passageway connected with middle cavity is provided with inside the air admission hole 903 of connection, the roller support 902 of another side of sleeve plug 9
904, the outlet passageway 904 inside the venthole 905 of some inside and outside insertions, roller support 902 is provided with roller 901 and passes through roller 901
On venthole 905 be in communication with the outside.Combined sleeve gapless is fitted tightly over the outer surface of roller 901 of sleeve plug 9.It is compound
The outer surface of sleeve can carve floral designs or regular ink cell using laser carving (erosion), form printing roller or quantitative transmission oil
The tape spool printing sleeve or tape spool reticulate pattern rolle rsleeve of ink (or quantitatively various coating mediums such as transmission sizing material).
A kind of manufacture method with shaft sleeve is provided below, comprises the following steps：
(1) compressed air is passed through into sleeve plug 9 by air admission hole 903 so that the inwall expansion of combined sleeve, is combined
Sleeve set is on sleeve plug 9；
(2) venting compressed air, gapless is fitted tightly over the roller 901 of sleeve plug 9 after the inside resilience of combined sleeve
Outer surface forms integrative-structure.
Claims (8)
1. a kind of combined sleeve, the combined sleeve is in hollow cylindrical, it is characterised in that：The combined sleeve is from the inside to the outside successively
For jacket layer in fiberglass (1), elastomer layer (2), glass fibre reinforced plastic structure layer (3), carbon fiber structural back-up coat (4), metal bonding layer
(5) and ceramics work top layer (6).
2. a kind of manufacture method of the combined sleeve described in claim 1, comprises the following steps：
(1) jacket layer (1) in coiling fiberglass：By die mandrel coiling glass fibre cotton yarn tape and solidify, jacket layer (1) in fiberglass
0.7~1.7mm of one-sided thickness；
(2) coiling elastomer layer (2)：Jacket layer (1) outer wrap elastomeric material formation elastomer layer in fiberglass after hardening
(2), 1~2mm of elastomer layer one-sided thickness；
(3) coiling glass fibre reinforced plastic structure layer (3)：In the outer coiling glass fiber tape of elastomer layer (2) or glass fiber formation glass
Glass steel structural layer (3)；
(4) coiling carbon fiber structural back-up coat (4)：Add in the outer coiling carbon fiber formation carbon fiber structural of glass fibre reinforced plastic structure layer (3)
Gu layer (4)；
(5) spray metal binder course (5)：In carbon fiber structural back-up coat (4) trypsin method point molten metal formation metal bonding layer
(5)；
(6) ceramic coated work top layer (6)：Ceramics work top layer (6) is formed in metal bonding layer (5) trypsin method ceramic powder；
(7) outer surface to combined sleeve polished, polishing.
3. a kind of manufacture method of combined sleeve according to claim 2, it is characterised in that：The spraying of the step (6)
Material is oxide ceramics or alloy.
4. a kind of manufacture method of combined sleeve according to claim 3, it is characterised in that：The oxide ceramics is oxygen
Change chromium or aluminum oxide.
5. a kind of manufacture method of combined sleeve according to claim 3, it is characterised in that：The alloy is that tungsten carbide is hard
Matter alloy.
6. a kind of band shaft sleeve of the combined sleeve described in usage right requirement 1, including sleeve plug (9), the sleeve plug
(9) the roller support (902) of roller (901) and the left and right sides is included, it is characterised in that：One side of the sleeve plug (9)
The air admission hole (903) connected with middle cavity, the roller support of another side of the sleeve plug (9) are provided with roller support (902)
(902) internal be provided with is provided with going out for some inside and outside insertions on the outlet passageway (904) connected with middle cavity, the roller (901)
Stomata (905), the internal outlet passageway (904) of the roller support (902) passes through the venthole (905) on roller (901) and the external world
Connection, the combined sleeve gapless is fitted tightly over roller (901) outer surface of sleeve plug (9).
7. a kind of band shaft sleeve according to claim 4, it is characterised in that：The outer surface of the combined sleeve passes through laser
Printing sleeve is made in carved pattern pattern.
8. the manufacture method with shaft sleeve described in a kind of claim 4, comprises the following steps：
(1) compressed air is passed through into sleeve plug (9) by air admission hole (903) so that the inwall expansion of combined sleeve, is combined
Sleeve set is on sleeve plug (9)；
(2) venting compressed air, gapless is fitted tightly over the roller (901) of sleeve plug (9) after the inside resilience of combined sleeve
Outer surface forms integrative-structure.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710141267.6A CN107009687A (en) | 2017-03-10 | 2017-03-10 | A kind of combined sleeve and manufacture method and with shaft sleeve and manufacture method |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710141267.6A CN107009687A (en) | 2017-03-10 | 2017-03-10 | A kind of combined sleeve and manufacture method and with shaft sleeve and manufacture method |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107009687A true CN107009687A (en) | 2017-08-04 |
Family
ID=59440578
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710141267.6A Pending CN107009687A (en) | 2017-03-10 | 2017-03-10 | A kind of combined sleeve and manufacture method and with shaft sleeve and manufacture method |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107009687A (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109049912A (en) * | 2018-09-26 | 2018-12-21 | 澳科利高新技术（无锡）有限公司 | Honeycomb composite roll and its processing method |
| CN109049946A (en) * | 2018-09-26 | 2018-12-21 | 澳科利高新技术（无锡）有限公司 | Paste version sleeve and its processing method and patch version roller and its handling method |
| CN109703177A (en) * | 2019-01-30 | 2019-05-03 | 上海运成印刷机械配件有限公司 | A kind of printing rolle rsleeve |
| CN112248638A (en) * | 2020-10-30 | 2021-01-22 | 绍兴万印新材料科技有限公司 | Processing method of carbon fiber sleeve anilox roller |
| CN113217305A (en) * | 2021-05-17 | 2021-08-06 | 广州赛特新能源科技发展有限公司 | Composite shaft of wind driven generator and wind driven generator |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE2628830A1 (en) * | 1976-06-26 | 1978-01-05 | Maschf Augsburg Nuernberg Ag | Vibrator roller for printing machine - is a hollow cylinder having vulcanised ink transferring coating |
| DE3525045A1 (en) * | 1985-07-13 | 1987-01-22 | Paul Sauer Druckwalzenfabriken | Impression cylinder |
| CN1443114A (en) * | 2000-03-17 | 2003-09-17 | 白昼国际有限公司 | Flexographic printing system and bridge mandrel |
| CN202370993U (en) * | 2011-11-14 | 2012-08-08 | 上海澳科利印刷机械有限公司 | Composite material roller |
| CN103770444A (en) * | 2013-09-10 | 2014-05-07 | 淄博朗达复合材料有限公司 | Easy-installation high-strength carbon fiber printing cylinder support |
| CN203651105U (en) * | 2013-11-26 | 2014-06-18 | 上海澳科利印刷机械有限公司 | Composite roller or rolling barrel or sleeve |
-
2017
- 2017-03-10 CN CN201710141267.6A patent/CN107009687A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE2628830A1 (en) * | 1976-06-26 | 1978-01-05 | Maschf Augsburg Nuernberg Ag | Vibrator roller for printing machine - is a hollow cylinder having vulcanised ink transferring coating |
| DE3525045A1 (en) * | 1985-07-13 | 1987-01-22 | Paul Sauer Druckwalzenfabriken | Impression cylinder |
| CN1443114A (en) * | 2000-03-17 | 2003-09-17 | 白昼国际有限公司 | Flexographic printing system and bridge mandrel |
| CN202370993U (en) * | 2011-11-14 | 2012-08-08 | 上海澳科利印刷机械有限公司 | Composite material roller |
| CN103770444A (en) * | 2013-09-10 | 2014-05-07 | 淄博朗达复合材料有限公司 | Easy-installation high-strength carbon fiber printing cylinder support |
| CN203651105U (en) * | 2013-11-26 | 2014-06-18 | 上海澳科利印刷机械有限公司 | Composite roller or rolling barrel or sleeve |
Non-Patent Citations (1)
| Title |
|---|
| 陆维强: "《轮转机组式凹版印刷机》", 30 April 2014 * |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109049912A (en) * | 2018-09-26 | 2018-12-21 | 澳科利高新技术（无锡）有限公司 | Honeycomb composite roll and its processing method |
| CN109049946A (en) * | 2018-09-26 | 2018-12-21 | 澳科利高新技术（无锡）有限公司 | Paste version sleeve and its processing method and patch version roller and its handling method |
| WO2020062691A1 (en) * | 2018-09-26 | 2020-04-02 | 澳科利高新技术（无锡）有限公司 | Honeycomb-structured laminated sleeve and manufacturing method therefor |
| CN109703177A (en) * | 2019-01-30 | 2019-05-03 | 上海运成印刷机械配件有限公司 | A kind of printing rolle rsleeve |
| CN112248638A (en) * | 2020-10-30 | 2021-01-22 | 绍兴万印新材料科技有限公司 | Processing method of carbon fiber sleeve anilox roller |
| CN113217305A (en) * | 2021-05-17 | 2021-08-06 | 广州赛特新能源科技发展有限公司 | Composite shaft of wind driven generator and wind driven generator |
| CN113217305B (en) * | 2021-05-17 | 2022-05-13 | 广州赛特新能源科技发展有限公司 | Composite shaft of wind driven generator and wind driven generator |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN107009687A (en) | A kind of combined sleeve and manufacture method and with shaft sleeve and manufacture method | |
| CN103322854B (en) | A kind of composite launching tube and preparation method thereof | |
| EP2004372B1 (en) | Composite mandrel | |
| DE69935759T2 (en) | GUN RUNNING WITH SMALL CALIBER | |
| JP5016646B2 (en) | Heat-resistant roll, manufacturing method thereof, and manufacturing method of plate glass using the same | |
| CN104015345B (en) | Supertension composites gas cylinder winding shaping process method | |
| CN202370993U (en) | Composite material roller | |
| CN108115066B (en) | forging cloth with heat preservation and lubrication functions and application method thereof | |
| ITMI20002138A1 (en) | PERFECT SLEEVE FOR SUBSIDIARY CYLINDER OF AN INDIRECT OR OFFSET PRINTING MACHINE | |
| CN102039336A (en) | Core for arcing and processing of bumper | |
| CN203651105U (en) | Composite roller or rolling barrel or sleeve | |
| CN101954422B (en) | Spinning deviation-correcting method for punching-pulling steel bottle tube wall thickness | |
| CN113862773B (en) | Long-life guide cylinder and preparation method thereof | |
| CN104118195B (en) | A kind of light durable type print roller | |
| US20050153821A1 (en) | Method of making a metal outer surface about a composite or polymer cylindrical core | |
| CN103015107B (en) | Fuzzing roller rolled by carbon fiber composite material in two-step method | |
| CN207042761U (en) | Applicator roll | |
| US20080241446A1 (en) | Composite material and methods of filament winding, pultrusion and open molding that material | |
| CN102161069B (en) | Forming method of no-material-head shaft piece by cross wedge rolling | |
| US6666807B2 (en) | Coating rod for paper manufacturing machines | |
| CN108119705B (en) | Reducing bamboo winding pipe structure and preparation method thereof | |
| CN211854905U (en) | Heat-insulating cylinder prefabricated body for pressurizing sintering furnace | |
| CN109049912A (en) | Honeycomb composite roll and its processing method | |
| CN103557380B (en) | Abrasion-proof pipe and preparation method thereof | |
| CN105690796A (en) | Manufacturing method of carbon fiber and glass fiber composite material javelin |
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: 20170804 |
|
| RJ01 | Rejection of invention patent application after publication |