CN106891549A - A kind of preparation facilities of MULTILAYER COMPOSITE eccentric abrasion prevention coiled rod - Google Patents
A kind of preparation facilities of MULTILAYER COMPOSITE eccentric abrasion prevention coiled rod Download PDFInfo
- Publication number
- CN106891549A CN106891549A CN201710010065.8A CN201710010065A CN106891549A CN 106891549 A CN106891549 A CN 106891549A CN 201710010065 A CN201710010065 A CN 201710010065A CN 106891549 A CN106891549 A CN 106891549A
- Authority
- CN
- China
- Prior art keywords
- resin
- layer
- fiber
- rod
- winding
- 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
- 239000002131 composite material Substances 0.000 title claims abstract description 42
- 238000005299 abrasion Methods 0.000 title claims abstract description 31
- 230000002265 prevention Effects 0.000 title claims abstract description 29
- 238000002360 preparation method Methods 0.000 title claims abstract description 27
- 229920005989 resin Polymers 0.000 claims abstract description 92
- 239000011347 resin Substances 0.000 claims abstract description 88
- 239000000835 fiber Substances 0.000 claims abstract description 80
- 238000004804 winding Methods 0.000 claims abstract description 49
- 229920001187 thermosetting polymer Polymers 0.000 claims abstract description 40
- 238000005507 spraying Methods 0.000 claims abstract description 30
- 238000001746 injection moulding Methods 0.000 claims abstract description 24
- 238000009954 braiding Methods 0.000 claims abstract description 23
- 238000002347 injection Methods 0.000 claims abstract description 21
- 239000007924 injection Substances 0.000 claims abstract description 21
- 239000011159 matrix material Substances 0.000 claims abstract description 18
- 238000007711 solidification Methods 0.000 claims abstract description 18
- 230000008023 solidification Effects 0.000 claims abstract description 18
- 239000000853 adhesive Substances 0.000 claims abstract description 15
- 230000001070 adhesive effect Effects 0.000 claims abstract description 15
- 230000003068 static effect Effects 0.000 claims abstract description 14
- 238000010438 heat treatment Methods 0.000 claims description 25
- 238000005086 pumping Methods 0.000 claims description 19
- 238000001816 cooling Methods 0.000 claims description 13
- 239000000203 mixture Substances 0.000 claims description 10
- 238000007493 shaping process Methods 0.000 claims description 10
- 238000011417 postcuring Methods 0.000 claims description 7
- 239000003292 glue Substances 0.000 claims description 6
- 239000007921 spray Substances 0.000 claims description 4
- 238000001125 extrusion Methods 0.000 claims description 3
- 238000000576 coating method Methods 0.000 abstract description 14
- 239000011248 coating agent Substances 0.000 abstract description 13
- 230000000694 effects Effects 0.000 abstract description 6
- 238000005259 measurement Methods 0.000 abstract description 2
- 238000000034 method Methods 0.000 description 13
- 239000003365 glass fiber Substances 0.000 description 12
- 239000000463 material Substances 0.000 description 11
- 229920000049 Carbon (fiber) Polymers 0.000 description 10
- 239000004917 carbon fiber Substances 0.000 description 10
- 229910052751 metal Inorganic materials 0.000 description 10
- 239000002184 metal Substances 0.000 description 10
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 10
- 229920001567 vinyl ester resin Polymers 0.000 description 9
- 229910052799 carbon Inorganic materials 0.000 description 7
- 239000003822 epoxy resin Substances 0.000 description 7
- 239000011152 fibreglass Substances 0.000 description 7
- 229920000647 polyepoxide Polymers 0.000 description 7
- 229920002748 Basalt fiber Polymers 0.000 description 6
- 229920006231 aramid fiber Polymers 0.000 description 6
- 229920001169 thermoplastic Polymers 0.000 description 6
- 239000004416 thermosoftening plastic Substances 0.000 description 6
- 229920006305 unsaturated polyester Polymers 0.000 description 6
- 230000007797 corrosion Effects 0.000 description 5
- 238000005260 corrosion Methods 0.000 description 5
- 230000001965 increasing effect Effects 0.000 description 5
- 238000004519 manufacturing process Methods 0.000 description 5
- 239000004593 Epoxy Substances 0.000 description 4
- 238000005452 bending Methods 0.000 description 4
- 230000002708 enhancing effect Effects 0.000 description 4
- 239000004814 polyurethane Substances 0.000 description 4
- 229920005749 polyurethane resin Polymers 0.000 description 4
- KXGFMDJXCMQABM-UHFFFAOYSA-N 2-methoxy-6-methylphenol Chemical compound [CH]OC1=CC=CC([CH])=C1O KXGFMDJXCMQABM-UHFFFAOYSA-N 0.000 description 3
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 3
- 238000005253 cladding Methods 0.000 description 3
- 239000007788 liquid Substances 0.000 description 3
- 150000002739 metals Chemical class 0.000 description 3
- 229920001568 phenolic resin Polymers 0.000 description 3
- 239000005011 phenolic resin Substances 0.000 description 3
- 229920003023 plastic Polymers 0.000 description 3
- 239000004033 plastic Substances 0.000 description 3
- 229920002635 polyurethane Polymers 0.000 description 3
- 230000000717 retained effect Effects 0.000 description 3
- 210000002435 tendon Anatomy 0.000 description 3
- XOOUIPVCVHRTMJ-UHFFFAOYSA-L zinc stearate Chemical compound [Zn+2].CCCCCCCCCCCCCCCCCC([O-])=O.CCCCCCCCCCCCCCCCCC([O-])=O XOOUIPVCVHRTMJ-UHFFFAOYSA-L 0.000 description 3
- WFUGQJXVXHBTEM-UHFFFAOYSA-N 2-hydroperoxy-2-(2-hydroperoxybutan-2-ylperoxy)butane Chemical group CCC(C)(OO)OOC(C)(CC)OO WFUGQJXVXHBTEM-UHFFFAOYSA-N 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 2
- 230000007547 defect Effects 0.000 description 2
- 238000007598 dipping method Methods 0.000 description 2
- 229920006241 epoxy vinyl ester resin Polymers 0.000 description 2
- 239000004744 fabric Substances 0.000 description 2
- UHOVQNZJYSORNB-UHFFFAOYSA-N monobenzene Natural products C1=CC=CC=C1 UHOVQNZJYSORNB-UHFFFAOYSA-N 0.000 description 2
- 238000000465 moulding Methods 0.000 description 2
- 239000007787 solid Substances 0.000 description 2
- 230000008646 thermal stress Effects 0.000 description 2
- 240000009087 Crescentia cujete Species 0.000 description 1
- 235000005983 Crescentia cujete Nutrition 0.000 description 1
- JOYRKODLDBILNP-UHFFFAOYSA-N Ethyl urethane Chemical compound CCOC(N)=O JOYRKODLDBILNP-UHFFFAOYSA-N 0.000 description 1
- 239000004705 High-molecular-weight polyethylene Substances 0.000 description 1
- 235000009797 Lagenaria vulgaris Nutrition 0.000 description 1
- 239000004677 Nylon Substances 0.000 description 1
- 235000014676 Phragmites communis Nutrition 0.000 description 1
- 239000004698 Polyethylene Substances 0.000 description 1
- 150000001721 carbon Chemical class 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 238000009833 condensation Methods 0.000 description 1
- 230000005494 condensation Effects 0.000 description 1
- 230000006866 deterioration Effects 0.000 description 1
- 238000009826 distribution Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000003628 erosive effect Effects 0.000 description 1
- 238000000605 extraction Methods 0.000 description 1
- 239000003733 fiber-reinforced composite Substances 0.000 description 1
- 238000001914 filtration Methods 0.000 description 1
- 239000011521 glass Substances 0.000 description 1
- 238000005470 impregnation Methods 0.000 description 1
- 239000012948 isocyanate Substances 0.000 description 1
- 150000002513 isocyanates Chemical class 0.000 description 1
- 238000002386 leaching Methods 0.000 description 1
- 230000007774 longterm Effects 0.000 description 1
- 125000002496 methyl group Chemical group [H]C([H])([H])* 0.000 description 1
- 229920001778 nylon Polymers 0.000 description 1
- 239000003129 oil well Substances 0.000 description 1
- -1 polyethylene Polymers 0.000 description 1
- 229920000573 polyethylene Polymers 0.000 description 1
- 239000012783 reinforcing fiber Substances 0.000 description 1
- 239000011435 rock Substances 0.000 description 1
- 239000000243 solution Substances 0.000 description 1
- 150000005846 sugar alcohols Polymers 0.000 description 1
- 238000004781 supercooling Methods 0.000 description 1
- 238000004381 surface treatment Methods 0.000 description 1
- 229920002803 thermoplastic polyurethane Polymers 0.000 description 1
- 229920005992 thermoplastic resin Polymers 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/28—Shaping operations therefor
- B29C70/40—Shaping or impregnating by compression not applied
- B29C70/50—Shaping or impregnating by compression not applied for producing articles of indefinite length, e.g. prepregs, sheet moulding compounds [SMC] or cross moulding compounds [XMC]
- B29C70/52—Pultrusion, i.e. forming and compressing by continuously pulling through a die
- B29C70/523—Pultrusion, i.e. forming and compressing by continuously pulling through a die and impregnating the reinforcement in the die
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/28—Shaping operations therefor
- B29C70/40—Shaping or impregnating by compression not applied
- B29C70/50—Shaping or impregnating by compression not applied for producing articles of indefinite length, e.g. prepregs, sheet moulding compounds [SMC] or cross moulding compounds [XMC]
- B29C70/52—Pultrusion, i.e. forming and compressing by continuously pulling through a die
- B29C70/521—Pultrusion, i.e. forming and compressing by continuously pulling through a die and impregnating the reinforcement before the die
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C35/00—Heating, cooling or curing, e.g. crosslinking or vulcanising; Apparatus therefor
- B29C35/02—Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/28—Shaping operations therefor
- B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/28—Shaping operations therefor
- B29C70/40—Shaping or impregnating by compression not applied
- B29C70/50—Shaping or impregnating by compression not applied for producing articles of indefinite length, e.g. prepregs, sheet moulding compounds [SMC] or cross moulding compounds [XMC]
- B29C70/52—Pultrusion, i.e. forming and compressing by continuously pulling through a die
- B29C70/525—Component parts, details or accessories; Auxiliary operations
- B29C70/528—Heating or cooling
-
- E—FIXED CONSTRUCTIONS
- E21—EARTH OR ROCK DRILLING; MINING
- E21B—EARTH OR ROCK DRILLING; OBTAINING OIL, GAS, WATER, SOLUBLE OR MELTABLE MATERIALS OR A SLURRY OF MINERALS FROM WELLS
- E21B17/00—Drilling rods or pipes; Flexible drill strings; Kellies; Drill collars; Sucker rods; Cables; Casings; Tubings
- E21B17/20—Flexible or articulated drilling pipes, e.g. flexible or articulated rods, pipes or cables
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C35/00—Heating, cooling or curing, e.g. crosslinking or vulcanising; Apparatus therefor
- B29C35/02—Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould
- B29C2035/0283—Thermal pretreatment of the plastics material
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Life Sciences & Earth Sciences (AREA)
- Physics & Mathematics (AREA)
- Geology (AREA)
- Mining & Mineral Resources (AREA)
- Health & Medical Sciences (AREA)
- Oral & Maxillofacial Surgery (AREA)
- Thermal Sciences (AREA)
- Environmental & Geological Engineering (AREA)
- Fluid Mechanics (AREA)
- General Life Sciences & Earth Sciences (AREA)
- Geochemistry & Mineralogy (AREA)
- Moulding By Coating Moulds (AREA)
Abstract
The present invention relates to a kind of preparation facilities of MULTILAYER COMPOSITE eccentric abrasion prevention coiled rod.Its technical scheme is：Adhesive pouring nozzle is housed in the bottom of injection molding, injector is by the adhesive pouring nozzle of bottom to injection molding inside resin by injection Matrix adhesive；One layer of enhanced winding layer or braiding layer are woven using braider or wrapping machine between internal layer longitudinal fiber and outer layer longitudinal fiber, a thermosetting resin spraying equipment and solidification equipment are provided between the draw-gear and coiler device of injecting pultrusion equipment.The resin that the injection spraying equipment that the present invention is used is sprayed is through measuring pump accurate measurement, it is ensured that the uniformity of coating thickness；The application of static blender can ensure being sufficiently mixed for resin, and the uniformity to product properties plays a key effect；Thermostat ensures that the proterties of spraying resin is consistent；Nozzle is specially designed, it is ensured that the consistency of thickness of coating around the body of rod；Two ends filter both can guarantee that and filtered out Excess resin, ensure that the thickness of spray-on coating.
Description
Technical field
The present invention relates to a kind of eccentric abrasion prevention coiled rod and its preparation facilities, more particularly to a kind of MULTILAYER COMPOSITE eccentric abrasion prevention
The preparation facilities of coiled rod.
Background technology
Because the Oil Reservoir Types developed become increasingly complex, while the continuous deterioration being continuously increased with well ore deposit environment of well depth,
Corrosion and eccentric wear problem turn into oil extraction in oil field technique problem demanding prompt solution.Because possessing the corrosion resistant feature of high-strength light, institute
Have started to progressively replace traditional metal sucker rod with composite sucker rod.The composite sucker rod for using at present is mainly wrapped
Include glass fiber reinforced plastic oil pumping rod and the major class of carbon fibre reinforced composite coiled rod two.Glass fiber reinforced plastic oil pumping rod is increased using glass fibre
Prepared by the pultrude process one-shot forming of heat-flash thermosetting resin, have been widely used, but as the modern reliability requirement for recovering the oil is continuous
Improve, glass fiber reinforced plastic oil pumping rod can not meet requirement, be primarily present problems with, 1, the resistance to eccentric wear of sucker rod it is bad；2nd, fatigue
Insufficient strength；3rd, respectively there is a metal joint at the equal fixed length of glass fiber reinforced plastic oil pumping rod, two ends, should using metal sucker rod between root and root
Metal box cupling is attached, and due to complex structure, difficulty of processing is big, expensive.Each glass fiber reinforced plastic oil pumping rod uses two
Individual metal joint, the cost of the two metal joints is far above a cost for the fiberglass body of rod；Pumped with conventional metals in addition
Bar compares, and except shank portion has changed material, the other parts of whole rod string have no change, conventional metals sucker rod
Column joint is more, and the de- probability that breaks is high, and substantially, the box cupling problem serious with oil pipe eccentric wear is not resolved piston effect.It is Chinese special
Sharp CN1417449 discloses a kind of preparation method of Anti-wear oil pumping rod, and the method is secondary in molded oil pumping bar body
The anti-abrading block of the materials such as injection moulding nylon, the covering material that reduction is used reduces continuous cladding cost and process complexity, but
Its injection abrasionproof block size is smaller, and relatively independent is distributed in the body of rod, anti-abrading block often occurs and departs from the body of rod, " sugared calabash occurs
Reed " phenomenon.In addition, its body of rod fixed length, it is impossible to which it is more to solve conventional metals rod connector, break-off accident rate is big, and piston effect is big
Etc. defect；And installed additional on the less body of rod of size anti-bias abrading block be can not solve it is inclined between metal joint and box cupling and oil pipe
Mill problem, and this is only the emphasis that sucker rod, pipe eccentric wear need to solve.CN101396874 discloses a kind of eccentric abrasion prevention and is combined
The preparation method and device of material sucker rod, its preparation method are on molded composite oil pumping club shaft, using leaching
Stain crosses the eccentric abrasion prevention layer of the abrasion resistant fibrous continuous-winding forming spiral tendon shape such as the aramid fiber of resin adhesive liquid, High molecular weight polyethylene, with
Reach eccentric abrasion prevention effect.The eccentric abrasion prevention layer of its spiral tendon shape, due to being with abrasion resistant fibrous enhancing thermosetting resin, thus while fine
Dimension is that, with antiwear characteristic, but after forming composite with thermosetting resin, its wear resistance decrease is a lot, and the life-span can not
How much is extension.In addition to its eccentric abrasion prevention for possessing spiral tendon shape layer, its shortcoming is as common glass fiber reinforced plastic oil pumping rod.China
Patent CN1461870 discloses a kind of carbon fibre reinforced composite coiled rod and preparation method, uses carbon fiber to increase
Strong material, and integral coating is constituted by transversely arranged aramid fiber or superhigh molecular weight polyethylene fibers beam and longitudinal glass fibre
It is compound, enhancing sucker rod transverse direction interlaminar shear strength is mainly solved, there is longitudinal splitting in oil well so as to avoid sucker rod
Problem, while also improving the resistance to eccentric wear and intensity of the body of rod.But the sucker rod is using pultrusion, an overall processing of cladding
Method（Including putting silk-resin pickup glue-clad cladding-preforming-solidification-coiling operation）, clad is fabric enhancing
Thermosetting resin, not only increases material cost, and the resistance to eccentric wear of fabric clad is not ideal enough.Further, since
The carbon fibre reinforced composite coiled rod cross sectional shape is rectangle or ellipse, and its thickness only has 3~5mm, is being answered
When removing well operations with special equipment, the material of retained part cannot almost be selected, and can only be clamped using two-piece type, left and right
Direction cannot be spacing, it is easy to which the phenomenon that the body of rod deflects away from retained part occurs.Therefore its special implement retained part of going into the well
Structure and developing material difficulty are larger, as the technical bottleneck in carbon fibre reinforced composite coiled rod application, limitation
The product large-scale promotion application.Patent of invention CN200910272324.X discloses a kind of coiled rod, using unidirectional
Reinforcing fiber pultrusion, the method for coating thermoplastic wearing layer, it is poor to there is radial compressive property in its structure, and thermoplastic wear resistant layer is hard
Degree is not high, the defect such as anti-wear performance is poor, it is impossible to meet long-term use and job requirements.
Chinese patent literature number is 103075112A, and patent name is《A kind of fibre reinforced composites eccentric abrasion prevention is continuous
Sucker rod and its preparation facilities and method》, it is a patent of invention that our company declared on November 30th, 2012, its technical side
Case is that to be covered with one layer of thermoplastic at one section or several sections of the outer surface of the fiber-reinforced resin matrix composite body of rod wear-resisting
Layer, the fiber that the body of rod is used is made up of one kind of glass fibre, carbon fiber or basalt fibre, resin matrix be epoxy resin,
One kind of polyurethane resin or vinyl ester resin.By being provided with a plastic extrusion between draw-gear and coiler device
Machine and cooling device, the one layer of thermoplastic of surface attachment using plastic extruder at a section or several sections of the shaping oil pumping body of rod
Wearing layer, then through apparatus for supercooling cooling treatment, forms fibre reinforced composites eccentric abrasion prevention coiled rod.Beneficial effect
It is：The excellent corrosion-resistant and resistance to eccentric wear performance of sucker rod is imparted, joint quantity is greatly reduced again, de- probability is resolved in reduction
And piston effect, in addition, its production efficiency is high, it is easy to operate.Its problem for existing is, because the thermoplastic for using is wear-resisting
Layer, its bending property and radially, axially compressive property is slightly more inferior；In addition, temperature tolerance, wear resistence are also than thermosetting wearing layer
Performance is weaker.
The content of the invention
The drawbacks described above that the purpose of the present invention exists aiming at prior art, there is provided a kind of MULTILAYER COMPOSITE eccentric abrasion prevention is continuous
The preparation facilities of sucker rod, is to be covered with one layer in a section or several sections of the outer surface of the fiber-reinforced resin matrix composite body of rod
Thermosetting wearing layer, using winding+pultrude process, or braiding+pultrude process, not give only excellent corrosion-resistant of sucker rod and
Resistance to eccentric wear performance, and with fabulous bending property and radially, axially compressive property, and wear resistence improves 30%, temperature tolerance is most
Up to 190 DEG C.
A kind of MULTILAYER COMPOSITE eccentric abrasion prevention coiled rod, in the outer surface of the fiber-reinforced resin matrix composite body of rod
One section or several sections is covered with one layer of thermosetting wearing layer（D）, described thermosetting wearing layer（D）For polyurethane, fluororine-carbon coating, it is modified
One kind in epoxy resin, vinyl ester resinses, unsaturated polyester (UP), phenolic resin is made, thermosetting wearing layer（D）Thickness be
0.5~10mm, the fiber that the described fiber-reinforced resin matrix composite body of rod is used is glass fibre, carbon fiber or the Black Warrior
One or more of rock fiber is made, using MULTILAYER COMPOSITE winding and pultrusion or braiding and the manufacturing process of pultrusion, by it is interior to
Outer is successively internal layer longitudinal fiber（A）, winding layer or braiding layer（B）, outer layer longitudinal fiber（C）, all winding layers, braiding layer and
Longitudinal fiber is the one kind in carbon fiber, glass fibre, basalt fibre, aramid fiber, and the resin matrix for using is epoxy
One kind of resin, polyurethane resin or vinyl ester resin, the continuous length of the body of rod being made is 0~5000m.
A kind of preparation facilities of MULTILAYER COMPOSITE eccentric abrasion prevention coiled rod that the present invention is mentioned, including put guide frame（1）, preheating
System（2）, wrapping machine or braider（3）, injector（5）, injection molding（4）, equipment for cooling die（6）, pultrusion die（7）、
Mold heating device（8）, control section（9）, post-curing heating stove（10）, draw-gear（11）, coiler device（14）Composition note
Pultrusion equipment is penetrated, in injection molding（4）Bottom be equipped with one or two adhesive pouring nozzles（4.1）, it is true that top is equipped with one or two
Empty mouth（4.2）, vacuum nozzle（4.2）External vacuum tube, vacuum tube is connected with vacuum tank；Described injector（5）By bottom
Adhesive pouring nozzle（4.1）To injection molding inside resin by injection Matrix adhesive（4.3）；In internal layer longitudinal fiber（A）It is fine with outer layer longitudinal direction
Dimension（C）Between use braider or wrapping machine（2）Braiding one layer of enhanced winding layer or braiding layer（B）, inject pultrusion and set
Standby draw-gear（11）And coiler device（14）Between be provided with a thermosetting resin spraying equipment（12）And solidification equipment
（13）, using thermosetting resin spraying equipment（12）In one section or several sections of the shaping oil pumping body of rod one layer of thermosetting of surface attachment
Wearing layer, then by solidification equipment（13）Solidification, forms fibre reinforced composites eccentric abrasion prevention coiled rod；Described heat
Thermosetting resin spraying equipment（12）Including resin pump（12a）, static blender（12b）, filter（12c）, resin cavity（12d）、
Filter（12e）, nozzle（12f）, heater（12g）, resin pump（12a）Output end be connected to static blender（12b）, it is quiet
State blender（12b）Lower end pass through filter（12c）With resin cavity（12d）Connection, static blender（12b）Outside be provided with
Heater（12g）, filter（12c）Lower end be provided with nozzle（12f）, described resin cavity（12d）Both sides be provided with filter
（12e）.
Above-mentioned nozzle（12f）By resin flow channel（12h）With injection orifice plate（12i）Composition, described resin flow channel（12h）
Using 360 degree of helical structures, orifice plate is sprayed（12i）Using taper star jet orifice structure.
Above-mentioned wrapping machine includes control system（3a）, servomotor（3b）, reductor（3c）, twin shaft exchange system
（3d）, wind fiber holding tray（3e）, tensioning apparatus（3f）, fiber placement axle（3g）, servomotor（3b）By reductor
（3c）Connection twin shaft exchange system（3d）, twin shaft exchange system（3d）Two ends connect respectively winding fiber holding tray（3e）, twine
Around fiber holding tray（3e）Outside pass through tensioning apparatus（3f）Connection fiber places axle（3g）.
Above-mentioned braider includes control system（3a）, servomotor（3b）, reductor（3c）, tensioning apparatus（3f）, it is fine
Dimension places axle（3g）, winding split axle drive system（3h）, winding axle exchange system（3i）, servomotor（3b）By reductor
（3c）Connection winding split axle drive system（3h）, wind split axle drive system（3h）With winding axle exchange system（3i）Connection, twines
Around axle exchange system（3i）Outside passes through tensioning apparatus（3f）Connection fiber places axle（3g）.
A kind of preparation method of MULTILAYER COMPOSITE eccentric abrasion prevention coiled rod that the present invention is mentioned, comprises the following steps and is made：
（a）From putting guide frame（1）Multiple fibre is drawn, in draw-gear（11）Traction under by injection molding（4）, injection molding
（4）It is interior full of injector（5）The resin matrix glue of injection（4.3）, resin matrix is epoxy resin, vinyl ester resin or poly-
Urethane resin；
（b）In internal layer longitudinal fiber（A）With outer layer longitudinal fiber（C）Between use braider or wrapping machine（2）One layer of increasing of braiding
Strong winding layer or braiding layer（B）, wherein, by wrapping machine（3）One or more layers 0.1~2mm thickness is wound, winding angle is
15~85 ° of winding layer；Or use braider（3）In internal layer longitudinal fiber（A）With outer layer longitudinal fiber（C）Between, winding
One or more layers thickness is 0.1~2mm, and intersecting angle is 15~85 ° of braiding layer；
（b）Through injection molding（4）The fibre bundle of interior glue dipping is again by pultrusion die（7）Curing molding, pultrusion die（7）'s
Porch is provided with equipment for cooling die（6）, for reducing die entrance temperature, it is to avoid mold temperature is conducted to injection molding（5）；
In pultrusion die（7）Surrounding, equipment for cooling die（6）Behind, mold heating device is distributed with（8）, in 2~4 sections of heating, Gu
Change temperature between 95~180 DEG C, heating mode in gradient, between 0.08~1.5 m/min, pultrusion goes out multiple pultrusion speed
The condensation material body of rod；The composite body of rod that pultrusion goes out enters post-curing heating stove（9）Thermal stress treatment and solidify afterwards are carried out, it is solid afterwards
Change terminates, by draw-gear（11）；
（c）In the draw-gear of injection extruding equipment（11）And coiler device（14）Between, a set thermosetting resin spray is set
Automatic doubler surface glouer device（12）And solidification equipment（13）, using thermosetting resin spraying equipment（12）One section on the shaping oil pumping body of rod
Or several sections one layer of thermosetting wearing layer of surface attachment, then by solidification equipment（13）；After through fully solidification, filled using winding
Put（11）By it on the disk of a diameter of 1.5m~3.5m.
The beneficial effects of the invention are as follows：Sucker rod of the invention, in continuous sucker rod made of fiber reinforced composition pultrusion work
Winding layer or braiding layer are increased on the basis of skill, radial strength and axial compression strength is increased, bending property is improve, dropped
Low bending diameter；Continuous one section or interrupted several sections of thermosetting wearing layers of surface spraying, impart the excellent corrosion resistant of sucker rod
Erosion and resistance to eccentric wear performance, improve 30% compared with existing thermoplastic wearing layer, and temperature tolerance is more preferably, can reach 190 DEG C；
In addition, using special spraying equipment, different from common spraying equipment, the resin that this injection spraying equipment is sprayed
Through measuring pump accurate measurement, it is ensured that the uniformity of coating thickness；The application of static blender can ensure being sufficiently mixed for resin,
Uniformity to product properties plays a key effect；Thermostat ensures that the proterties of spraying resin is consistent；Nozzle is through special
Design, it is ensured that the consistency of thickness of coating around the body of rod；The design of two ends filter both can guarantee that and filtered out Excess resin,
Ensure that the thickness of spray-on coating；
The preparation method that also present invention is provided, it is solid using winding pultrusion, braiding pultrusion, injection pultrusion and thermosetting resin spraying
Change assembling process, the continuous-stable of continuous sucker rod made of fiber reinforced composition body of rod production can be greatly improved, match somebody with somebody
Close special spray equipment, it is ensured that position distribution of the thermosetting resin wearing layer on oil pumping club shaft surface meets design need
Ask, the combination of wearing layer and the body of rod is completed online, and production efficiency is high, and bond strength is big, it is to avoid layering, the hair of obscission
It is raw.
Brief description of the drawings
Accompanying drawing 1 is the cross section structure figure of coiled rod of the invention；
Accompanying drawing 2 is the schematic flow sheet of preparation facilities of the invention；
Accompanying drawing 3 is the structural representation of injection molding in injection pultrude process of the invention；
Accompanying drawing 4 is the structural representation of wrapping machine in winding pultrude process of the invention；
Accompanying drawing 5 is the structural representation of braider in braiding pultrude process of the invention；
Accompanying drawing 6 is the structural representation of spraying equipment in thermoplastic resin spraying coating process of the invention；
Accompanying drawing 7 is the sectional view of the nozzle segment of spraying equipment of the invention；
Accompanying drawing 8 is the M-M structure charts of the nozzle segment of spraying equipment of the invention；
In upper figure：Put guide frame 1, pretreatment heating furnace 2, wrapping machine or braider 3, injector, 5, injection molding 4, mould cooling
Device 6, pultrusion die 7, mold heating device 8, control section 9, post-curing heating stove 10, draw-gear 11, thermosetting resin
Spraying equipment 12, solidification equipment 13, coiler device 14；
Internal layer longitudinal fiber A, winding layer or braiding layer B, outer layer longitudinal fiber C, thermosetting wearing layer D；
Control system 3a, servomotor 3b, reductor 3c, twin shaft exchange system 3d wind fiber holding tray 3e, tensioning apparatus
3f, fiber places axle 3g, winds split axle drive system 3h, winding axle exchange system 3i；Adhesive pouring nozzle 4.1, vacuum nozzle 4.2, resin
Matrix adhesive 4.3；Resin pump 12a, static blender 12b, filter 12c, resin cavity 12d, filter 12e, nozzle 12f, plus
Hot device 12g, resin flow channel 12h, injection orifice plate 12i, oil pumping club shaft 12j.
Specific embodiment
Referring to the drawings 1, a kind of MULTILAYER COMPOSITE eccentric abrasion prevention coiled rod that the present invention is mentioned, in fiber-reinforced resin matrix
One section or several sections of the outer surface of the composite body of rod is covered with one layer of thermosetting wearing layer D, and described thermosetting wearing layer D is poly-
One kind in urethane, fluororine-carbon coating, modified epoxy, vinyl ester resinses, unsaturated polyester (UP), phenolic resin is made, thermosetting
Property wearing layer D thickness be 0.5~10mm, the fiber that the described fiber-reinforced resin matrix composite body of rod is used is glass
One or more of fiber, carbon fiber or basalt fibre is made, using MULTILAYER COMPOSITE winding and pultrusion or braiding and pultrusion
Manufacturing process, be successively from inside to outside internal layer longitudinal fiber A, winding layer or braiding layer B, outer layer longitudinal fiber C, all windings
Layer, braiding layer and longitudinal fiber are the one kind in carbon fiber, glass fibre, basalt fibre, aramid fiber, the resin of use
Matrix is one kind of epoxy resin, polyurethane resin or vinyl ester resin, and the continuous length of the body of rod being made is 0~5000m.
Referring to the drawings 2, the preparation facilities of a kind of MULTILAYER COMPOSITE eccentric abrasion prevention coiled rod that the present invention is mentioned, including put silk
Frame 1, pre-heating system 2, wrapping machine or braider 3, injector 5, injection molding 4, equipment for cooling die 6, pultrusion die 7, mould
Heater 8, control section 9, post-curing heating stove 10, draw-gear 11, the composition injection pultrusion equipment of coiler device 14,
One or two adhesive pouring nozzles 4.1 are housed in the bottom of injection molding 4, top is equipped with one or two vacuum nozzles 4.2, outside vacuum nozzle 4.2
Vacuum tube is connect, vacuum tube is connected with vacuum tank；Described injector 5 is noted by the adhesive pouring nozzle 4.1 of bottom to inside injection molding
Enter resin matrix glue 4.3；Between internal layer longitudinal fiber A and outer layer longitudinal fiber C one is woven using braider or wrapping machine 2
The enhanced winding layer of layer or braiding layer B, one is provided between the draw-gear 11 and coiler device 14 of injecting pultrusion equipment
Platform thermosetting resin spraying equipment 12 and solidification equipment 13, using thermosetting resin spraying equipment 12 the one of the shaping oil pumping body of rod
Section or several sections one layer of thermosetting wearing layer of surface attachment, then solidify by solidification equipment 13, form fiber-reinforced composite material
Material eccentric abrasion prevention coiled rod；Described thermosetting resin spraying equipment 12 includes resin pump 12a, static blender 12b, filtering
Plate 12c, resin cavity 12d, filter 12e, nozzle 12f, heater 12g, the output end of resin pump 12a are connected to static blender
The lower end of 12b, static blender 12b is connected by filter 12c with resin cavity 12d, and the outside of static blender 12b is provided with and adds
The lower end of hot device 12g, filter 12c is provided with nozzle 12f, and oil pumping club shaft 12j is sprayed by nozzle 12f, described
The both sides of resin cavity 12d are provided with filter 12e；Described nozzle 12f is made up of resin flow channel 12h and injection orifice plate 12i, described
Resin flow channel 12h use 360 degree helical structures, injection orifice plate 12i using taper star jet orifice structure, referring in particular to accompanying drawing 7
With 8.
Referring to the drawings 5, above-mentioned wrapping machine includes control system 3a, servomotor 3b, reductor 3c, twin shaft exchange system
3d, winding fiber holding tray 3e, tensioning apparatus 3f, fiber places axle 3g, and servomotor 3b connects twin shaft and changes by reductor 3c
To system 3d, the two ends of twin shaft exchange system 3d connect winding fiber holding tray 3e, the outside of winding fiber holding tray 3e respectively
Fiber is connected by tensioning apparatus 3f and places axle 3g.
Referring to the drawings 6, braider includes that control system 3a, servomotor 3b, reductor 3c, tensioning apparatus 3f, fiber are put
Axle 3g, winding split axle drive system 3h, winding axle exchange system 3i, servomotor 3b are put by reductor 3c connection winding split axles
Drive system 3h, winding split axle drive system 3h are connected with winding axle exchange system 3i, and winding axle exchange system 3i outsides pass through
Tensioning apparatus 3f connection fibers place axle 3g.
A kind of preparation method of MULTILAYER COMPOSITE eccentric abrasion prevention coiled rod that the present invention is mentioned, comprises the following steps and is made：
A draws multiple fibre from guide frame 1 is put, and by injection molding 4 under the traction of draw-gear 11, is full of in injection molding 4
The resin matrix glue 4.3 of the injection of injector 5, resin matrix is epoxy resin, vinyl ester resin or polyurethane resin；
B weaves one layer of enhanced winding between internal layer longitudinal fiber A and outer layer longitudinal fiber C using braider or wrapping machine 2
Layer or braiding layer B, wherein, one or more layers 0.1~2mm thickness is wound by wrapping machine 3, winding angle is 15~85 ° to be twined
Winding layer；Or using braider 3 between internal layer longitudinal fiber A and outer layer longitudinal fiber C, winding one or more layers thickness is
0.1~2mm, intersecting angle is 15~85 ° of braiding layer；
Through the fibre bundle of glue dipping in injection molding 4 again by the curing molding of pultrusion die 7, the porch of pultrusion die 7 sets b
There is equipment for cooling die 6, for reducing die entrance temperature, it is to avoid mold temperature is conducted to injection molding 4；In pultrusion die 7
Behind surrounding, equipment for cooling die 6, mold heating device 8 is distributed with, in 2~4 sections of heating, solidification temperature is at 95~180 DEG C
Between, heating mode in gradient, between 0.08~1.5 m/min, pultrusion goes out the composite body of rod to pultrusion speed；Pultrusion goes out
The composite body of rod carry out thermal stress treatment and solidify afterwards into post-curing heating stove 9, solidify afterwards terminate, by draw-gear
11；
C sets a set thermosetting resin spraying equipment between the draw-gear 11 and coiler device 14 of injection extruding equipment
Device 12 and solidification equipment 13, using the surface attachment one of one section or several sections of plastic extrusion apparatus 12 on the shaping oil pumping body of rod
Layer thermosetting wearing layer, then by solidification equipment 13；After through fully solidification, using coiler device 11 by it wound on a diameter of
On the disk of 1.5m~3.5m.
Below by embodiment, to the detailed description of the invention, but the invention is not restricted to these embodiments.
Embodiment 1：
The preparation method of MULTILAYER COMPOSITE eccentric abrasion prevention coiled rod, its internal layer longitudinal fiber A is carbon fiber, outer layer longitudinal fiber C
It is high strength glass fiber, ectonexine mid-wrap layer B is high-strength glass fibre, and its preparation method comprises the following steps：
By internal layer multi-beam carbon-fiber silk through putting guide frame row silk hole enter into surface treatment stove, furnace temperature between 80~150 DEG C,
Hauling speed is 1.0~12.5 minutes by the time between 0.08~1.5 m/min, and the carbon fiber after heat treatment is being twined
After winding layer glass fibre cladding, enter simultaneously in injection molding, injection molding full of note with winding layer, outer layer high-strength glass fibre
The resin adhesive liquid of machine injection is penetrated, resin adhesive liquid proportioning is polyalcohol：Isocyanates=100:121；Carbon fiber after impregnation enters drawing
Extruding mold, pultrusion die porch is down to behind room temperature, but water-cooled using recirculated water cooling mode, using mold heating device, will
Three sections of heating of mould, temperature is 110 DEG C, 165 DEG C, 155 DEG C；Composite bar after shaping continues with 0.08~1.5 m/min
Speed advance, by length be 2 meters, temperature be 150 DEG C post-curing heating stove solidify afterwards treatment, fully cooled down by air
Afterwards, the body of rod enters thermosetting resin spraying equipment by hauling machine as heart yearn, and thermosetting resin spraying equipment squeezes coating thickness
It is the layer of polyurethane of 0.5mm, after being heating and curing, oil pumping club shaft outer surface is bonded in, with one section of fiber with wearing layer
Enhancing composite eccentric abrasion prevention coiled rod is wound on disk and completes.
Embodiment 2：
The preparation method of fibre reinforced composites eccentric abrasion prevention coiled rod, internal layer longitudinal fiber A and outer layer longitudinal fiber C are
High-strength glass fibre, mid-wrap layer B uses high-strength glass fibre, its preparation method to comprise the following steps：
Hauling speed is 0.2 m/min, and change injecting resin is epoxy resin, its epoxy resin E-51：Methyl tetrahydrochysene benzene
Acid anhydride：DMP-30：The parts by weight of zinc stearate are 100：85：2.0：1, the heating of two sections of pultrusion die, temperature is 120 DEG C, 160
℃；Die length 1000mm, the sucker rod after shaping is 160 DEG C by temperature, and length is processed for the solidify afterwards treatment furnace of 3m；It is cold
But afterwards by the use of the fluororine-carbon coating that thermosetting resin spraying equipment continuous spray thickness is 2mm as wearing layer, by fully solidification
Afterwards, the continuous sucker rod made of fiber reinforced composition with wearing layer is wound on disk and completes.
Embodiment 3：
The preparation method of preferred fibre reinforced composites eccentric abrasion prevention coiled rod, internal layer longitudinal fiber A and outer layer longitudinal direction
Fiber C is basalt fibre, and mid-wrap layer B is also basalt fibre, and its preparation method comprises the following steps：
The furnace temperature of heat treatment of fiber is 120 DEG C, and hauling speed is 0.38 m/min, and change injecting resin is vinyl ester resin,
Wherein Atlac 430：MEKP：BPO：The parts by weight of zinc stearate are 100：1.5：1.5：1, three sections of mould is heated, and temperature is
95℃、115℃、145℃；Sucker rod after shaping is 140 DEG C by temperature, and length is processed for the solidify afterwards treatment furnace of 3m；It is cold
But modified epoxy of the thickness for 10mm is continuously extruded as wearing layer by the use of thermosetting resin spraying equipment afterwards, by abundant
After cooling, the continuous sucker rod made of fiber reinforced composition with wearing layer is wound on the disk of a diameter of 3.5m.
Embodiment 4：
The preparation method of preferred fibre reinforced composites eccentric abrasion prevention coiled rod, internal layer longitudinal fiber A and outer layer longitudinal direction
Fiber C is aramid fiber, and mid-wrap layer B is also aramid fiber, and its preparation method comprises the following steps：
The furnace temperature of heat treatment of fiber is 120 DEG C, and hauling speed is 0.38 m/min, and change injecting resin is vinyl ester resin,
Wherein Atlac 430：MEKP：BPO：The parts by weight of zinc stearate are 100：1.5：1.5：1, three sections of mould is heated, and temperature is
95℃、115℃、145℃；Sucker rod after shaping is 140 DEG C by temperature, and length is processed for the solidify afterwards treatment furnace of 3m；It is cold
But vinyl ester resinses of the thickness for 10mm are continuously extruded as wearing layer by the use of thermosetting resin spraying equipment afterwards, by abundant
After cooling, the continuous sucker rod made of fiber reinforced composition with wearing layer is wound on the disk of a diameter of 3.5m.
Winding layer is replaced by braiding layer, and its thickness is 0.1 ~ 2mm；
Described thermosetting wearing layer be polyurethane, fluororine-carbon coating, modified epoxy, vinyl ester resinses, unsaturated polyester (UP),
One kind in phenolic resin.
Claims (2)
1. a kind of preparation facilities of MULTILAYER COMPOSITE eccentric abrasion prevention coiled rod, it is characterized in that including putting guide frame（1）, pre-heating system
（2）, wrapping machine or braider（3）, injector（5）, injection molding（4）, equipment for cooling die（6）, pultrusion die（7）, mould
Heater（8）, control section（9）, post-curing heating stove（10）, draw-gear（11）, coiler device（14）Composition injection is drawn
Extrusion forming equipment, in injection molding（4）Bottom be equipped with one or two adhesive pouring nozzles（4.1）, top is equipped with one or two vacuum nozzles
（4.2）, vacuum nozzle（4.2）External vacuum tube, vacuum tube is connected with vacuum tank；Described injector（5）By the injecting glue of bottom
Mouth（4.1）To injection molding inside resin by injection Matrix adhesive（4.3）；It is characterized in that：In internal layer longitudinal fiber（A）It is vertical with outer layer
To fiber（C）Between use wrapping machine or braider（3）Braiding one layer of enhanced winding layer or braiding layer（B）, injection pultrusion into
The draw-gear of type equipment（11）And coiler device（14）Between be provided with a thermosetting resin spraying equipment（12）And solidification
Device（13）, using thermosetting resin spraying equipment（12）In one section or several sections of the shaping oil pumping body of rod one layer of heat of surface attachment
Solidity wearing layer, then by solidification equipment（13）Solidification, forms fibre reinforced composites eccentric abrasion prevention coiled rod；It is described
Thermosetting resin spraying equipment（12）Including resin pump（12a）, static blender（12b）, filter（12c）, resin cavity
（12d）, filter（12e）, nozzle（12f）, heater（12g）, resin pump（12a）Output end be connected to static blender
（12b）, static blender（12b）Lower end pass through filter（12c）With resin cavity（12d）Connection, static blender（12b）'s
Outside is provided with heater（12g）, filter（12c）Lower end be provided with nozzle（12f）, described resin cavity（12d）Both sides set
There is filter（12e）；
Described nozzle（12f）By resin flow channel（12h）With injection orifice plate（12i）Composition, described resin flow channel（12h）Using
360 degree of helical structures, spray orifice plate（12i）Using taper star jet orifice structure；
Described wrapping machine includes control system（3a）, servomotor（3b）, reductor（3c）, twin shaft exchange system（3d）, twine
Around fiber holding tray（3e）, tensioning apparatus（3f）, fiber placement axle（3g）, servomotor（3b）By reductor（3c）Connection is double
Axle exchange system（3d）, twin shaft exchange system（3d）Two ends connect respectively winding fiber holding tray（3e）, winding fiber placement
Disk（3e）Outside pass through tensioning apparatus（3f）Connection fiber places axle（3g）.
2. the preparation facilities of MULTILAYER COMPOSITE eccentric abrasion prevention coiled rod according to claim 1, it is characterized in that：Described volume
Loom includes control system（3a）, servomotor（3b）, reductor（3c）, tensioning apparatus（3f）, fiber place axle（3g）, winding
Split axle drive system（3h）, winding axle exchange system（3i）, servomotor（3b）By reductor（3c）Connection winding split axle drives
Dynamic system（3h）, wind split axle drive system（3h）With winding axle exchange system（3i）Connection, winds axle exchange system（3i）Outward
Side passes through tensioning apparatus（3f）Connection fiber places axle（3g）.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710010065.8A CN106891549B (en) | 2014-06-16 | 2014-06-16 | A kind of preparation facilities of MULTILAYER COMPOSITE eccentric abrasion prevention coiled rod |
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710010065.8A CN106891549B (en) | 2014-06-16 | 2014-06-16 | A kind of preparation facilities of MULTILAYER COMPOSITE eccentric abrasion prevention coiled rod |
| CN201410264787.2A CN104060944B (en) | 2014-06-16 | 2014-06-16 | Multilayer compound eccentric-wear-preventing continuous sucker rod and manufacturing device and method thereof |
Related Parent Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410264787.2A Division CN104060944B (en) | 2014-06-16 | 2014-06-16 | Multilayer compound eccentric-wear-preventing continuous sucker rod and manufacturing device and method thereof |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN106891549A true CN106891549A (en) | 2017-06-27 |
| CN106891549B CN106891549B (en) | 2019-01-08 |
Family
ID=51548853
Family Applications (3)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710010065.8A Active CN106891549B (en) | 2014-06-16 | 2014-06-16 | A kind of preparation facilities of MULTILAYER COMPOSITE eccentric abrasion prevention coiled rod |
| CN201710010288.4A Pending CN106671453A (en) | 2014-06-16 | 2014-06-16 | Manufacturing method of multi-layer composite eccentric wear preventing continuous sucker rod |
| CN201410264787.2A Active CN104060944B (en) | 2014-06-16 | 2014-06-16 | Multilayer compound eccentric-wear-preventing continuous sucker rod and manufacturing device and method thereof |
Family Applications After (2)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710010288.4A Pending CN106671453A (en) | 2014-06-16 | 2014-06-16 | Manufacturing method of multi-layer composite eccentric wear preventing continuous sucker rod |
| CN201410264787.2A Active CN104060944B (en) | 2014-06-16 | 2014-06-16 | Multilayer compound eccentric-wear-preventing continuous sucker rod and manufacturing device and method thereof |
Country Status (1)
| Country | Link |
|---|---|
| CN (3) | CN106891549B (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110126308A (en) * | 2019-05-24 | 2019-08-16 | 增城华昌塑料五金模具有限公司 | A method of drawing twines synchronous manufacture fiber composite arrow shaft |
| CN110303694A (en) * | 2019-05-31 | 2019-10-08 | 北京卫星制造厂有限公司 | A kind of rapid molding device and method of continuous fiber reinforced composite materials pipe fitting |
| CN116160721A (en) * | 2023-02-03 | 2023-05-26 | 武汉理工大学 | Rocket nozzle preparation system |
Families Citing this family (21)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105003209B (en) * | 2015-07-21 | 2018-03-02 | 山东大学 | A kind of sucker rod and preparation facilities and preparation method with composite screw wearing layer |
| CN105172169B (en) * | 2015-09-23 | 2017-11-07 | 胜利油田新大管业科技发展有限责任公司 | High-temperature resistance carbon fiber strengthens composite continuous sucker rod and preparation facilities and method |
| CN105178878B (en) * | 2015-09-28 | 2019-09-03 | 江苏众成复合材料有限责任公司 | A kind of continuous sucker rod made of fiber reinforced composition and its preparation facilities and method |
| CN105235241A (en) * | 2015-10-26 | 2016-01-13 | 南京诺尔泰复合材料设备制造有限公司 | Thermosetting composite and thermoplastic material sucker rod preparation method and device |
| CN105298403B (en) * | 2015-11-24 | 2017-06-27 | 山东大学 | A kind of continuous carbon fibre sucker rod with wear-resistant protecting layer and preparation method thereof |
| CN105625951B (en) * | 2016-02-29 | 2017-11-21 | 胜利油田新大管业科技发展有限责任公司 | A kind of preparation method of fibre reinforced composites eccentric abrasion prevention coiled rod |
| CN106837203B (en) * | 2016-09-30 | 2018-02-09 | 席小平 | A kind of preparation method of multilayer rub resistance carbon-fiber continuous rod |
| CN106593361B (en) * | 2017-01-18 | 2017-11-03 | 华运隆腾机械制造有限公司 | A kind of oil well pump intelligent drive device and winding type pumping unit system |
| CN109723388A (en) * | 2017-10-27 | 2019-05-07 | 中国石油化工股份有限公司 | A kind of fibre reinforced wrapped tube and preparation method thereof |
| CN108104733B (en) * | 2018-02-01 | 2024-02-23 | 山东中恒景新碳纤维科技发展有限公司 | Carbon fiber composite sucker rod with autonomous repair function |
| CN108678684B (en) * | 2018-06-29 | 2024-01-12 | 山东大学 | Impact-resistant composite sucker rod |
| CN109488219B (en) * | 2018-11-28 | 2024-02-02 | 胜利新大新材料股份有限公司 | Corrosion-resistant high-temperature-resistant composite material continuous sucker rod with multilayer structure and preparation process thereof |
| CN109849219A (en) * | 2019-01-24 | 2019-06-07 | 基准宇航(北京)有限公司 | A kind of device and method preparing continuous carbon fibre enhancing PEEK thermoplastic prepreg |
| CN109798075B (en) * | 2019-02-10 | 2020-09-01 | 北京工商大学 | Fatigue-resistant steel oil pumping polished rod with multi-layer structure and processing technology thereof |
| CN109838469A (en) * | 2019-03-11 | 2019-06-04 | 江苏恒神股份有限公司 | A kind of connection type of Carbon Fiber Composite Propeller Shaft |
| CN110239154B (en) * | 2019-04-12 | 2023-12-15 | 江苏华盟新型材料科技有限公司 | High-strength fiber pultrusion pipeline |
| CN111716759A (en) * | 2020-06-10 | 2020-09-29 | 福建省泉诚塑胶科技有限公司 | Fiber-woven pultrusion pipeline and manufacturing method |
| CN111923450A (en) * | 2020-09-14 | 2020-11-13 | 江苏九鼎新材料股份有限公司 | Pultrusion method of thin-wall component |
| CN112721345A (en) * | 2021-01-20 | 2021-04-30 | 哈尔滨玻璃钢研究院有限公司 | Composite material holding pole structure for communication antenna and preparation method thereof |
| CN113085225B (en) * | 2021-03-31 | 2022-07-26 | 合肥工业大学 | Method for continuously preparing integral composite sleeper by using controllable polyurethane composite material |
| CN117283901B (en) * | 2023-09-28 | 2024-02-20 | 山东三泰非金属材料有限公司 | Gum dipping system for composite material pultrusion process |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2001301072A (en) * | 2000-04-20 | 2001-10-30 | Mitsubishi Heavy Ind Ltd | Ring made of fiber reinforced composite material and method of manufacturing the same |
| CN2545355Y (en) * | 2002-03-14 | 2003-04-16 | 张传国 | Built-in centering device |
| US20040067364A1 (en) * | 2002-10-08 | 2004-04-08 | National Aerospace Laboratory Of Japan | Carbon nanofiber-dispersed resin fiber-reinforced composite material |
| CN101913254A (en) * | 2010-07-21 | 2010-12-15 | 高宝安 | Vertical pultrusion process and device of multilayer fiber composite laminated section bar |
| CN103075112A (en) * | 2012-11-30 | 2013-05-01 | 胜利油田新大管业科技发展有限责任公司 | Fibre reinforced composite anti-eccentric coiled rod as well as preparation device and preparation method thereof |
| CN202965219U (en) * | 2012-11-30 | 2013-06-05 | 胜利油田新大管业科技发展有限责任公司 | Plastic extruding machine for manufacturing fiber reinforced composite eccentric wear prevention continuous sucker rod |
Family Cites Families (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1319712A (en) * | 2000-04-12 | 2001-10-31 | 刘堪金 | Composite mateiral tension rod |
| CN101396874B (en) * | 2007-09-28 | 2010-06-30 | 北京化工大学 | Preparation method and device of eccentric wear prevention pumping rod |
| CN201962486U (en) * | 2010-11-23 | 2011-09-07 | 江苏腾达非织造材料有限公司 | One-time molding melting and spraying compound production equipment |
| CN102285106B (en) * | 2011-09-06 | 2013-12-18 | 李建学 | Computer controlled composite material bent tube winding machine |
-
2014
- 2014-06-16 CN CN201710010065.8A patent/CN106891549B/en active Active
- 2014-06-16 CN CN201710010288.4A patent/CN106671453A/en active Pending
- 2014-06-16 CN CN201410264787.2A patent/CN104060944B/en active Active
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2001301072A (en) * | 2000-04-20 | 2001-10-30 | Mitsubishi Heavy Ind Ltd | Ring made of fiber reinforced composite material and method of manufacturing the same |
| CN2545355Y (en) * | 2002-03-14 | 2003-04-16 | 张传国 | Built-in centering device |
| US20040067364A1 (en) * | 2002-10-08 | 2004-04-08 | National Aerospace Laboratory Of Japan | Carbon nanofiber-dispersed resin fiber-reinforced composite material |
| CN101913254A (en) * | 2010-07-21 | 2010-12-15 | 高宝安 | Vertical pultrusion process and device of multilayer fiber composite laminated section bar |
| CN103075112A (en) * | 2012-11-30 | 2013-05-01 | 胜利油田新大管业科技发展有限责任公司 | Fibre reinforced composite anti-eccentric coiled rod as well as preparation device and preparation method thereof |
| CN202965219U (en) * | 2012-11-30 | 2013-06-05 | 胜利油田新大管业科技发展有限责任公司 | Plastic extruding machine for manufacturing fiber reinforced composite eccentric wear prevention continuous sucker rod |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110126308A (en) * | 2019-05-24 | 2019-08-16 | 增城华昌塑料五金模具有限公司 | A method of drawing twines synchronous manufacture fiber composite arrow shaft |
| CN110126308B (en) * | 2019-05-24 | 2021-12-14 | 增城华昌塑料五金模具有限公司 | Method for synchronously manufacturing fiber composite arrow shaft by drawing and winding |
| CN110303694A (en) * | 2019-05-31 | 2019-10-08 | 北京卫星制造厂有限公司 | A kind of rapid molding device and method of continuous fiber reinforced composite materials pipe fitting |
| CN116160721A (en) * | 2023-02-03 | 2023-05-26 | 武汉理工大学 | Rocket nozzle preparation system |
| CN116160721B (en) * | 2023-02-03 | 2024-05-14 | 武汉理工大学 | Rocket nozzle preparation system |
Also Published As
| Publication number | Publication date |
|---|---|
| CN104060944A (en) | 2014-09-24 |
| CN106671453A (en) | 2017-05-17 |
| CN106891549B (en) | 2019-01-08 |
| CN104060944B (en) | 2017-02-15 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN104060944B (en) | Multilayer compound eccentric-wear-preventing continuous sucker rod and manufacturing device and method thereof | |
| CN105172169B (en) | High-temperature resistance carbon fiber strengthens composite continuous sucker rod and preparation facilities and method | |
| CN105625951B (en) | A kind of preparation method of fibre reinforced composites eccentric abrasion prevention coiled rod | |
| CN205000906U (en) | Fibre reinforced composite continuous sucker rod's preparation facilities | |
| CN105178878B (en) | A kind of continuous sucker rod made of fiber reinforced composition and its preparation facilities and method | |
| CN103075112B (en) | Fibre reinforced composite anti-eccentric coiled rod as well as preparation device and preparation method thereof | |
| CN105003209B (en) | A kind of sucker rod and preparation facilities and preparation method with composite screw wearing layer | |
| CN101396874B (en) | Preparation method and device of eccentric wear prevention pumping rod | |
| CN106194046B (en) | Multi-layer abrasion-resistant carbon fiber continuous sucker rod and making device and making method | |
| CN108625794A (en) | A kind of carbon-fiber continuous rod and its preparation facilities and method | |
| CN205477401U (en) | Resistant carbon fiber reinforcement combined material continuous sucker rod that grinds partially and preparation facilities thereof | |
| CN205291631U (en) | High temperature resistant carbon fiber reinforcement combined material continuous sucker rod and preparation facilities | |
| CN107443773A (en) | Coiled rod, the device and method for preparing coiled rod | |
| CN103206612A (en) | Light-metal-lined composite cylinder fully-wrapped with basalt fiber, and production process thereof | |
| CN104343396A (en) | Preparation method of fiber reinforced composite material continuous sucker rod | |
| CN103225369A (en) | Fiber composite bar with surface having helicitic texture, and making method thereof | |
| CN111720631A (en) | High-ring-stiffness stretch-wound FRP pipe and preparation method thereof | |
| CN102233679A (en) | Production line and production method of composite material profile with units connected in series | |
| CN202965218U (en) | Preparation device for fiber reinforced composite material anti-eccentric wearing continuous sucker rod | |
| CN106761444A (en) | A kind of constant temperature heat tracing carbon-fiber continuous rod and preparation facilities and preparation method | |
| CN203008798U (en) | Fiber reinforced composite material anti-eccentric continuous sucker rod | |
| CN105235241A (en) | Thermosetting composite and thermoplastic material sucker rod preparation method and device | |
| CN103707561B (en) | A kind of laminboard layer composite lamp stand and quick molding method thereof | |
| CN104325653B (en) | The method for continuous production of a kind of GRP pipe and prepared GRP pipe | |
| CN207469874U (en) | A kind of carbon fiber pultruded panels enhance composite material pole tower used for transmission line |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CP02 | Change in the address of a patent holder |
Address after: 257091 No. 86 Beiyi Road, Dongying Technological and Economic Development Zone, Dongying City, Shandong Province Patentee after: Shengli Oilfield Xinda Pipe Industry Technology Development Co., Ltd. Address before: 257091 No. 86 Beiyi Road, Dongying Economic Development Zone, Shandong Province Patentee before: Shengli Oilfield Xinda Pipe Industry Technology Development Co., Ltd. |
|
| CP02 | Change in the address of a patent holder | ||
| CP01 | Change in the name or title of a patent holder |
Address after: No.86, Beiyi Road, Dongying technological and Economic Development Zone, Dongying City, Shandong Province Patentee after: Shengli new big new materials Co., Ltd Address before: No.86, Beiyi Road, Dongying technological and Economic Development Zone, Dongying City, Shandong Province Patentee before: SHENGLI OILFIELD XINDA PIPES TECHNOLOGY DEVELOPMENT Co.,Ltd. |
|
| CP01 | Change in the name or title of a patent holder |