CN106591729A - Straight core-spun yarn friction spinning mechanism - Google Patents

Straight core-spun yarn friction spinning mechanism Download PDF

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Publication number
CN106591729A
CN106591729A CN201611162918.1A CN201611162918A CN106591729A CN 106591729 A CN106591729 A CN 106591729A CN 201611162918 A CN201611162918 A CN 201611162918A CN 106591729 A CN106591729 A CN 106591729A
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parts
water
alloy
dust cage
oxide
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翁华明
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Suzhou Rich Industrial Equipment Co Ltd
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Suzhou Rich Industrial Equipment Co Ltd
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B05SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
    • B05DPROCESSES FOR APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
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    • DTEXTILES; PAPER
    • D02YARNS; MECHANICAL FINISHING OF YARNS OR ROPES; WARPING OR BEAMING
    • D02GCRIMPING OR CURLING FIBRES, FILAMENTS, THREADS, OR YARNS; YARNS OR THREADS
    • D02G3/00Yarns or threads, e.g. fancy yarns; Processes or apparatus for the production thereof, not otherwise provided for
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Abstract

The invention discloses a straight core-spun yarn friction spinning mechanism which comprises a carding roller, a dust cage and a twisting machine which are linked up in sequence. The lower end of the carding roller is provided with a carding roller outlet, the upper end of the dust cage is provided with a dust cage inlet, and the plane at the carding roller outlet and the plane at the dust cage inlet are arranged in a mutually inclined manner; and the carding roller is wrapped with a shell. The preparation process of a coating includes the specific steps that (1), by weight, a mixture of 2-7 parts of phenolic resin and 1-5 parts of nanometer silicon dioxide is dispersed in 10-15 parts of water, and then 3-6 parts of short-cut carbon fiber, 1-5 parts of a silane coupling agent, 2-4 parts of ethylene glycol monobutyl ether, 3-7 parts of cetyl trimethyl ammonium bromide, 1-5 parts of graphite, 2-6 parts of kaolin and 3-8 parts of micro silicon powder are added and mixed; (2), the mixture obtained in step 1 is subjected to ball milling and dried, and a dried material is obtained; (3), the dried material obtained in step 2 is sintered in a high-temperature vacuum furnace and ground till the fineness reaches 40-60 microns, and the coating is obtained.

Description

A kind of straight covering yarn mechanism of weaving that rubs
Technical field
The invention belongs to technical field of textile equipment, particularly a kind of straight covering yarn mechanism of weaving that rubs.
Background technology
Current friction spun yarn is a kind of open-end-spinning, as all open-end-spinnings, with rotor spinning phase As feed opening mechanism, feeding ribbon is resolved into into single fiber state, and the cohesion of fiber twisting is taken out by band The screen cloth of device is inhaled come what is realized, screen cloth can be the dust cage of major diameter, or flat continuous reticular zones.
Current friction spinning machine often has that mechanism is complicated, cumbersome, spinning effect is bad and manufacturing cost is high , also there is fiber and vertically feed in shortcoming, the low defect of yarn strength between two dust cages of yarn axle;Design one kind can solve the problem that above-mentioned The straight covering yarn mechanism of friction weaving of shortcoming is the technical problem to be solved.
The content of the invention
The present invention provides a kind of friction weaving straight covering yarn mechanism to solve technical problem present in known technology.
The present invention is adopted the technical scheme that by solving technical problem present in known technology:A kind of friction weaving is straight Covering yarn mechanism, including the combing roller, dust cage and twister that are connected successively, combing roller lower end is provided with combing roller outlet, on dust cage End is provided with dust cage entrance, and combing roller exit plane is mutually inclined setting with dust cage porch plane;Combing roller is enclosed with outer Shell, in shell, the mass percent of each composition is:C:0.02-0.03%, Al:1.16-1.83%,Zn:1.22-1.39%,Mn: 0.37-0.58%, S:≤ 0.030%, P:≤ 0.030%, Cr:0.02-0.04%, Ni:0.84-1.19%, Cu:0.25-0.29%, V: 0.02-0.05%, Mo:0.06-0.09%, Ti:1.33-1.59%, B:0.01-0.02%, Pd:0.02-0.04%,Pt:0.33- 0.49%,W:0.23-0.36%,Nd:0.13-0.16%,Ce:0.11-0.12%,Eu:0.07-0.15%,Lu:0.03-0.07%, Au:0.33-0.42%, Ag:0.86-1.04%, Ga:0.01-0.02%, Y:0.21-0.27%, Sn:1.34-1.58%, Zr:0.02- 0.07%, Re:0.01-0.03%, Bi:0.05-0.09%, magnesium oxide:0.33-0.37%, copper oxide:0.08-0.13%, oxidation Ferrum:0.12-0.18%, manganese dioxide:0.06-0.09%, Copper hydrate:0.05-0.08%, hydrated ferric oxide.:0.03- 0.05%, balance of Fe;
The making of wire netting comprises the steps:
A, add raw materials in smelting furnace by the mass percent of each composition in predetermined internal combustion engine cooling water pump, by smelting furnace Temperature brings up to 1520 degrees Celsius to 1540 degrees Celsius, and raw material is smelted to form alloy solution;
B, alloy solution obtained in the previous step is cooled down, during cooling, water-cooled is combined with air cooling, first adopts water-cooled with 15-18 DEG C/alloy solution water-cooled to 450-460 DEG C of formation alloy, is then air cooled to 340-350 DEG C by the cooldown rate of s, then using water The cold cooldown rate with 18-20 DEG C/s is by alloy water-cooled to room temperature;
C, heating, the alloy after previous step is cooled down carry out secondary smelting in smelting furnace, and the temperature in smelting furnace is brought up to 1580 Degree Celsius to 1610 degrees Celsius, alloy is formed alloy solution by secondary smelting;
D, pour the alloy solution in smelting furnace into electric furnace, nodulizer and inovulant are sequentially added in the bag hole of casting ladle, use thin steel Plate is covered on nodulizer, inovulant, and is consolidated, and steel-sheet thickness is 0.5mm to 1mm;
E, the opposite side that the alloy solution in electric furnace is poured into casting ladle indent, spheroidizing reacion 70s to 85s, after spheroidizing reacion is abundant, The slag agent of one layer of collection is spread, is quickly skimmed;
F, quickly skim after, be sprinkled into swelling perlite powder on alloy solution surface immediately, twice of slag hitting, after the completion of slag hitting, is formed Alloy solution to be cast, was poured in five minutes;
G, the outer surface of shell are coated with corrosion resistant coating;
The preparation technology of coating is specially:
The mixture of phenolic resin 2-7 parts and nano silicon 1-5 parts in parts by weight, is scattered in water 10-15 by step 1 In part, chopped carbon fiber 3-6 parts, silane coupler 1-5 parts, ethylene glycol monobutyl ether 2-4 parts, cetyl trimethyl bromine are added Change ammonium 3-7 parts, graphite 1-5 parts, Kaolin 2-6 parts and SILICA FUME 3-8 parts, mixing;
Step 1 gained mixed material is carried out ball milling by step 2, is dried, is obtained dried object;
Step 3, step 2 gained dried object is sintered in vacuum high temperature furnace, is ground to fineness and is reached 40-60 μm and obtains final product.
Further, the straight covering yarn mechanism of aforesaid friction weaving, in shell, the mass percent of each composition is:C: 0.025%, Al:1.52%,Zn:1.25%,Mn:0.43%, S:≤ 0.030%, P:≤ 0.030%, Cr:0.025%, Ni:1.15%, Cu:0.26%, V:0.03%, Mo:0.07%, Ti:1.36%, B:0.015%, Pd:0.025%,Pt:0.36%,W:0.25%,Nd: 0.15%,Ce:0.115%,Eu:0.08%,Lu:0.05%, Au:0.36%, Ag:1.01%, Ga:0.015%, Y:0.25%, Sn: 1.36%, Zr:0.04%, Re:0.01%, Bi:0.06%, magnesium oxide:0.35%, copper oxide:0.095%, ferrum oxide:0.15%, Manganese dioxide:0.07%, Copper hydrate:0.06%, hydrated ferric oxide.:0.04%, balance of Fe;
The preparation technology of coating is specially:
Step 1, in parts by weight, the mixture of 2 parts of 3 parts of phenolic resin and nano silicon is scattered in 12 parts of water, then Add 4 parts of chopped carbon fiber, 3 parts of silane coupler, 2 parts of ethylene glycol monobutyl ether, 4 parts of cetyl trimethylammonium bromide, graphite 3 6 parts of part, 3 parts of Kaolin and SILICA FUME, mixing;
Step 1 gained mixed material is carried out ball milling by step 2, is dried, is obtained dried object;
Step 3, step 2 gained dried object is sintered in vacuum high temperature furnace, is ground to fineness and is reached 43 μm and obtains final product.
Further, the straight covering yarn mechanism of aforesaid friction weaving, in shell, the mass percent of each composition is:C: 0.027%, Al:1.72%,Zn:1.27%,Mn:0.43%, S:≤ 0.030%, P:≤ 0.030%, Cr:0.027%, Ni:0.95%, Cu:0.27%, V:0.03%, Mo:0.08%, Ti:1.43%, B:0.015%, Pd:0.027%,Pt:0.43%,W:0.27%,Nd: 0.15%,Ce:0.11%,Eu:0.13%,Lu:0.05%, Au:0.39%, Ag:0.95%, Ga:0.015%, Y:0.27%, Sn: 1.43%, Zr:0.05%, Re:0.02%, Bi:0.08%, magnesium oxide:0.36%, copper oxide:0.095%, ferrum oxide:0.16%, Manganese dioxide:0.072%, Copper hydrate:0.072%, hydrated ferric oxide.:0.043%, balance of Fe;
The preparation technology of coating is specially:
Step 1, in parts by weight, the mixture of 3 parts of 5 parts of phenolic resin and nano silicon is scattered in 11 parts of water, then Add 5 parts of chopped carbon fiber, 4 parts of silane coupler, 3 parts of ethylene glycol monobutyl ether, 6 parts of cetyl trimethylammonium bromide, graphite 3 5 parts of part, 5 parts of Kaolin and SILICA FUME, mixing;
Step 1 gained mixed material is carried out ball milling by step 2, is dried, is obtained dried object;
Step 3, step 2 gained dried object is sintered in vacuum high temperature furnace, is ground to fineness and is reached 58 μm and obtains final product.
Specific embodiment
For the content of the invention, feature and effect of the present invention can be further appreciated that, hereby enumerate following examples and describe in detail such as Under.
Embodiment 1
A kind of straight covering yarn mechanism of friction weaving is present embodiments provided, including the combing roller, dust cage and twister that are connected successively, Combing roller lower end is provided with combing roller outlet, and dust cage upper end is provided with dust cage entrance, combing roller exit plane and dust cage porch Plane is mutually inclined setting;Combing roller is enclosed with shell, and in shell, the mass percent of each composition is:C:0.025%, Al: 1.52%,Zn:1.25%,Mn:0.43%, S:≤ 0.030%, P:≤ 0.030%, Cr:0.025%, Ni:1.15%, Cu:0.26%, V: 0.03%, Mo:0.07%, Ti:1.36%, B:0.015%, Pd:0.025%,Pt:0.36%,W:0.25%,Nd:0.15%,Ce: 0.115%,Eu:0.08%,Lu:0.05%, Au:0.36%, Ag:1.01%, Ga:0.015%, Y:0.25%, Sn:1.36%, Zr: 0.04%, Re:0.01%, Bi:0.06%, magnesium oxide:0.35%, copper oxide:0.095%, ferrum oxide:0.15%, manganese dioxide: 0.07%, Copper hydrate:0.06%, hydrated ferric oxide.:0.04%, balance of Fe;
The making of wire netting comprises the steps:
A, add raw materials in smelting furnace by the mass percent of each composition in predetermined internal combustion engine cooling water pump, by smelting furnace Temperature brings up to 1520 degrees Celsius to 1540 degrees Celsius, and raw material is smelted to form alloy solution;
B, alloy solution obtained in the previous step is cooled down, during cooling, water-cooled is combined with air cooling, first adopts water-cooled with 15-18 DEG C/alloy solution water-cooled to 450-460 DEG C of formation alloy, is then air cooled to 340-350 DEG C by the cooldown rate of s, then using water The cold cooldown rate with 18-20 DEG C/s is by alloy water-cooled to room temperature;
C, heating, the alloy after previous step is cooled down carry out secondary smelting in smelting furnace, and the temperature in smelting furnace is brought up to 1580 Degree Celsius to 1610 degrees Celsius, alloy is formed alloy solution by secondary smelting;
D, pour the alloy solution in smelting furnace into electric furnace, nodulizer and inovulant are sequentially added in the bag hole of casting ladle, use thin steel Plate is covered on nodulizer, inovulant, and is consolidated, and steel-sheet thickness is 0.5mm to 1mm;
E, the opposite side that the alloy solution in electric furnace is poured into casting ladle indent, spheroidizing reacion 70s to 85s, after spheroidizing reacion is abundant, The slag agent of one layer of collection is spread, is quickly skimmed;
F, quickly skim after, be sprinkled into swelling perlite powder on alloy solution surface immediately, twice of slag hitting, after the completion of slag hitting, is formed Alloy solution to be cast, was poured in five minutes;
G, the outer surface of shell are coated with corrosion resistant coating;
The preparation technology of coating is specially:
Step 1, in parts by weight, the mixture of 2 parts of 3 parts of phenolic resin and nano silicon is scattered in 12 parts of water, then Add 4 parts of chopped carbon fiber, 3 parts of silane coupler, 2 parts of ethylene glycol monobutyl ether, 4 parts of cetyl trimethylammonium bromide, graphite 3 6 parts of part, 3 parts of Kaolin and SILICA FUME, mixing;
Step 1 gained mixed material is carried out ball milling by step 2, is dried, is obtained dried object;
Step 3, step 2 gained dried object is sintered in vacuum high temperature furnace, is ground to fineness and is reached 43 μm and obtains final product.
Embodiment 2
A kind of straight covering yarn mechanism of friction weaving is present embodiments provided, including the combing roller, dust cage and twister that are connected successively, Combing roller lower end is provided with combing roller outlet, and dust cage upper end is provided with dust cage entrance, combing roller exit plane and dust cage porch Plane is mutually inclined setting;Combing roller is enclosed with shell, and in shell, the mass percent of each composition is:C:0.027%, Al: 1.72%,Zn:1.27%,Mn:0.43%, S:≤ 0.030%, P:≤ 0.030%, Cr:0.027%, Ni:0.95%, Cu:0.27%, V: 0.03%, Mo:0.08%, Ti:1.43%, B:0.015%, Pd:0.027%,Pt:0.43%,W:0.27%,Nd:0.15%,Ce: 0.11%,Eu:0.13%,Lu:0.05%, Au:0.39%, Ag:0.95%, Ga:0.015%, Y:0.27%, Sn:1.43%, Zr: 0.05%, Re:0.02%, Bi:0.08%, magnesium oxide:0.36%, copper oxide:0.095%, ferrum oxide:0.16%, manganese dioxide: 0.072%, Copper hydrate:0.072%, hydrated ferric oxide.:0.043%, balance of Fe;
The making of wire netting comprises the steps:
A, add raw materials in smelting furnace by the mass percent of each composition in predetermined internal combustion engine cooling water pump, by smelting furnace Temperature brings up to 1520 degrees Celsius to 1540 degrees Celsius, and raw material is smelted to form alloy solution;
B, alloy solution obtained in the previous step is cooled down, during cooling, water-cooled is combined with air cooling, first adopts water-cooled with 15-18 DEG C/alloy solution water-cooled to 450-460 DEG C of formation alloy, is then air cooled to 340-350 DEG C by the cooldown rate of s, then using water The cold cooldown rate with 18-20 DEG C/s is by alloy water-cooled to room temperature;
C, heating, the alloy after previous step is cooled down carry out secondary smelting in smelting furnace, and the temperature in smelting furnace is brought up to 1580 Degree Celsius to 1610 degrees Celsius, alloy is formed alloy solution by secondary smelting;
D, pour the alloy solution in smelting furnace into electric furnace, nodulizer and inovulant are sequentially added in the bag hole of casting ladle, use thin steel Plate is covered on nodulizer, inovulant, and is consolidated, and steel-sheet thickness is 0.5mm to 1mm;
E, the opposite side that the alloy solution in electric furnace is poured into casting ladle indent, spheroidizing reacion 70s to 85s, after spheroidizing reacion is abundant, The slag agent of one layer of collection is spread, is quickly skimmed;
F, quickly skim after, be sprinkled into swelling perlite powder on alloy solution surface immediately, twice of slag hitting, after the completion of slag hitting, is formed Alloy solution to be cast, was poured in five minutes;
G, the outer surface of shell are coated with corrosion resistant coating;
The preparation technology of coating is specially:
Step 1, in parts by weight, the mixture of 3 parts of 5 parts of phenolic resin and nano silicon is scattered in 11 parts of water, then Add 5 parts of chopped carbon fiber, 4 parts of silane coupler, 3 parts of ethylene glycol monobutyl ether, 6 parts of cetyl trimethylammonium bromide, graphite 3 5 parts of part, 5 parts of Kaolin and SILICA FUME, mixing;
Step 1 gained mixed material is carried out ball milling by step 2, is dried, is obtained dried object;
Step 3, step 2 gained dried object is sintered in vacuum high temperature furnace, is ground to fineness and is reached 58 μm and obtains final product.
The above is only to presently preferred embodiments of the present invention, not make any pro forma restriction to the present invention, it is every According to the technical spirit of the present invention to any simple modification made for any of the above embodiments, equivalent variations and modification, this is belonged to In the range of bright technical scheme.

Claims (3)

1. the straight covering yarn mechanism of a kind of friction weaving, it is characterised in that:Including the combing roller, dust cage and twister that are connected successively, The combing roller lower end is provided with combing roller outlet, and the dust cage upper end is provided with dust cage entrance, combing roller exit plane Setting is mutually inclined with dust cage porch plane;The combing roller is enclosed with shell, the quality of each composition in the shell Percentage ratio is:C:0.02-0.03%, Al:1.16-1.83%,Zn:1.22-1.39%,Mn:0.37-0.58%, S:≤ 0.030%, P: ≤ 0.030%, Cr:0.02-0.04%, Ni:0.84-1.19%, Cu:0.25-0.29%, V:0.02-0.05%, Mo:0.06- 0.09%, Ti:1.33-1.59%, B:0.01-0.02%, Pd:0.02-0.04%,Pt:0.33-0.49%,W:0.23-0.36%,Nd: 0.13-0.16%,Ce:0.11-0.12%,Eu:0.07-0.15%,Lu:0.03-0.07%, Au:0.33-0.42%, Ag:0.86- 1.04%, Ga:0.01-0.02%, Y:0.21-0.27%, Sn:1.34-1.58%, Zr:0.02-0.07%, Re:0.01-0.03%, Bi:0.05-0.09%, magnesium oxide:0.33-0.37%, copper oxide:0.08-0.13%, ferrum oxide:0.12-0.18%, titanium dioxide Manganese:0.06-0.09%, Copper hydrate:0.05-0.08%, hydrated ferric oxide.:0.03-0.05%, balance of Fe;
The making of the wire netting comprises the steps:
A, add raw materials in smelting furnace by the mass percent of each composition in predetermined internal combustion engine cooling water pump, by smelting furnace Temperature brings up to 1520 degrees Celsius to 1540 degrees Celsius, and raw material is smelted to form alloy solution;
B, alloy solution obtained in the previous step is cooled down, during cooling, water-cooled is combined with air cooling, first adopts water-cooled with 15-18 DEG C/alloy solution water-cooled to 450-460 DEG C of formation alloy, is then air cooled to 340-350 DEG C by the cooldown rate of s, then using water The cold cooldown rate with 18-20 DEG C/s is by alloy water-cooled to room temperature;
C, heating, the alloy after previous step is cooled down carry out secondary smelting in smelting furnace, and the temperature in smelting furnace is brought up to 1580 Degree Celsius to 1610 degrees Celsius, alloy is formed alloy solution by secondary smelting;
D, pour the alloy solution in smelting furnace into electric furnace, nodulizer and inovulant are sequentially added in the bag hole of casting ladle, use thin steel Plate is covered on nodulizer, inovulant, and is consolidated, and steel-sheet thickness is 0.5mm to 1mm;
E, the opposite side that the alloy solution in electric furnace is poured into casting ladle indent, spheroidizing reacion 70s to 85s, after spheroidizing reacion is abundant, The slag agent of one layer of collection is spread, is quickly skimmed;
F, quickly skim after, be sprinkled into swelling perlite powder on alloy solution surface immediately, twice of slag hitting, after the completion of slag hitting, is formed Alloy solution to be cast, was poured in five minutes;
G, the outer surface of the shell are coated with corrosion resistant coating;
The preparation technology of the coating is specially:
The mixture of phenolic resin 2-7 parts and nano silicon 1-5 parts in parts by weight, is scattered in water 10-15 by step 1 In part, chopped carbon fiber 3-6 parts, silane coupler 1-5 parts, ethylene glycol monobutyl ether 2-4 parts, cetyl trimethyl bromine are added Change ammonium 3-7 parts, graphite 1-5 parts, Kaolin 2-6 parts and SILICA FUME 3-8 parts, mixing;
Step 1 gained mixed material is carried out ball milling by step 2, is dried, is obtained dried object;
Step 3, step 2 gained dried object is sintered in vacuum high temperature furnace, is ground to fineness and is reached 40-60 μm and obtains final product.
2. the straight covering yarn mechanism of friction weaving according to claim 1, it is characterised in that:C:0.025%, Al:1.52%, Zn:1.25%,Mn:0.43%, S:≤ 0.030%, P:≤ 0.030%, Cr:0.025%, Ni:1.15%, Cu:0.26%, V:0.03%, Mo:0.07%, Ti:1.36%, B:0.015%, Pd:0.025%,Pt:0.36%,W:0.25%,Nd:0.15%,Ce:0.115%,Eu: 0.08%,Lu:0.05%, Au:0.36%, Ag:1.01%, Ga:0.015%, Y:0.25%, Sn:1.36%, Zr:0.04%, Re: 0.01%, Bi:0.06%, magnesium oxide:0.35%, copper oxide:0.095%, ferrum oxide:0.15%, manganese dioxide:0.07%, hydrogen Copper oxide:0.06%, hydrated ferric oxide.:0.04%, balance of Fe;
The preparation technology of the coating is specially:
Step 1, in parts by weight, the mixture of 2 parts of 3 parts of phenolic resin and nano silicon is scattered in 12 parts of water, then Add 4 parts of chopped carbon fiber, 3 parts of silane coupler, 2 parts of ethylene glycol monobutyl ether, 4 parts of cetyl trimethylammonium bromide, graphite 3 6 parts of part, 3 parts of Kaolin and SILICA FUME, mixing;
Step 1 gained mixed material is carried out ball milling by step 2, is dried, is obtained dried object;
Step 3, step 2 gained dried object is sintered in vacuum high temperature furnace, is ground to fineness and is reached 43 μm and obtains final product.
3. the straight covering yarn mechanism of friction weaving according to claim 1, it is characterised in that:C:0.027%, Al:1.72%, Zn:1.27%,Mn:0.43%, S:≤ 0.030%, P:≤ 0.030%, Cr:0.027%, Ni:0.95%, Cu:0.27%, V:0.03%, Mo:0.08%, Ti:1.43%, B:0.015%, Pd:0.027%,Pt:0.43%,W:0.27%,Nd:0.15%,Ce:0.11%,Eu: 0.13%,Lu:0.05%, Au:0.39%, Ag:0.95%, Ga:0.015%, Y:0.27%, Sn:1.43%, Zr:0.05%, Re: 0.02%, Bi:0.08%, magnesium oxide:0.36%, copper oxide:0.095%, ferrum oxide:0.16%, manganese dioxide:0.072%, hydrogen Copper oxide:0.072%, hydrated ferric oxide.:0.043%, balance of Fe;
The preparation technology of the coating is specially:
Step 1, in parts by weight, the mixture of 3 parts of 5 parts of phenolic resin and nano silicon is scattered in 11 parts of water, then Add 5 parts of chopped carbon fiber, 4 parts of silane coupler, 3 parts of ethylene glycol monobutyl ether, 6 parts of cetyl trimethylammonium bromide, graphite 3 5 parts of part, 5 parts of Kaolin and SILICA FUME, mixing;
Step 1 gained mixed material is carried out ball milling by step 2, is dried, is obtained dried object;
Step 3, step 2 gained dried object is sintered in vacuum high temperature furnace, is ground to fineness and is reached 58 μm and obtains final product.
CN201611162918.1A 2016-12-15 2016-12-15 Straight core-spun yarn friction spinning mechanism Pending CN106591729A (en)

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107541830A (en) * 2017-08-15 2018-01-05 张家港思淇科技有限公司 A kind of yarn and yarn-forming mechanism and protective textiles and weaving method and equipment

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105369157A (en) * 2015-12-04 2016-03-02 苏州市神龙门窗有限公司 Processing process of anti-sticking and abrasion-resistant stainless steel door frame
CN105369158A (en) * 2015-12-04 2016-03-02 苏州市神龙门窗有限公司 Processing process of high-temperature-resistant stainless steel window frame
CN205803678U (en) * 2016-07-05 2016-12-14 大丰市欧工摩擦纺织机械制造厂 The straight covering yarn mechanism of a kind of tilting feeding friction weaving
CN106224012A (en) * 2016-08-31 2016-12-14 南京赛达机械制造有限公司 A kind of titanium alloy efficient gas turbine blade
CN106224667A (en) * 2016-07-29 2016-12-14 盐城丰工机械有限公司 The quick firm flange of a kind of connection

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105369157A (en) * 2015-12-04 2016-03-02 苏州市神龙门窗有限公司 Processing process of anti-sticking and abrasion-resistant stainless steel door frame
CN105369158A (en) * 2015-12-04 2016-03-02 苏州市神龙门窗有限公司 Processing process of high-temperature-resistant stainless steel window frame
CN205803678U (en) * 2016-07-05 2016-12-14 大丰市欧工摩擦纺织机械制造厂 The straight covering yarn mechanism of a kind of tilting feeding friction weaving
CN106224667A (en) * 2016-07-29 2016-12-14 盐城丰工机械有限公司 The quick firm flange of a kind of connection
CN106224012A (en) * 2016-08-31 2016-12-14 南京赛达机械制造有限公司 A kind of titanium alloy efficient gas turbine blade

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107541830A (en) * 2017-08-15 2018-01-05 张家港思淇科技有限公司 A kind of yarn and yarn-forming mechanism and protective textiles and weaving method and equipment

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