CN107574515A - A kind of integrated composite spinning method - Google Patents

A kind of integrated composite spinning method Download PDF

Info

Publication number
CN107574515A
CN107574515A CN201710638376.9A CN201710638376A CN107574515A CN 107574515 A CN107574515 A CN 107574515A CN 201710638376 A CN201710638376 A CN 201710638376A CN 107574515 A CN107574515 A CN 107574515A
Authority
CN
China
Prior art keywords
inlet channel
hollow cavity
integrated composite
gas outlet
composite spinning
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
Application number
CN201710638376.9A
Other languages
Chinese (zh)
Other versions
CN107574515B (en
Inventor
傅婷
张玉泽
王姜
丁倩
江慧
肖岚
陈南梁
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Donghua University
National Dong Hwa University
Original Assignee
Donghua University
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Donghua University filed Critical Donghua University
Priority to CN201710638376.9A priority Critical patent/CN107574515B/en
Publication of CN107574515A publication Critical patent/CN107574515A/en
Application granted granted Critical
Publication of CN107574515B publication Critical patent/CN107574515B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Abstract

The present invention relates to a kind of integrated composite spinning method, the overhung of grid ring is fixed with guiding device in Nesting Zone, the bottom surface of guiding device and the distance on grid ring surface are 1~5mm, hollow cavity is offered in guiding device, the direction of hollow cavity inlet and outlet is identical with sliver traffic direction, hollow cavity connects with space in the groove for gathering groove, hollow cavity connects with two top inlet channels and a side inlet channel, the airflow direction of top inlet channel is perpendicular to grid ring, two top inlet channels are located on the straight line parallel with sliver traffic direction, side inlet channel is the tapered configuration that air inlet is big and gas outlet is small.Compared with traditional integrated composite spinning method, the pressure of negative-pressure air-flow and the quality of the final obtained integrated composite yarn of guarantee when the inventive method can effectively reduce integrated composite spinning, the energy consumption of integrated composite spinning is significantly reduced, has saved production cost, there is fabulous practical value and promotional value.

Description

A kind of integrated composite spinning method
Technical field
The invention belongs to field of textiles, is related to a kind of Yarn spinning method, more particularly to a kind of integrated composite spinning method.
Background technology
In recent years, due to both having the advantages of traditional ring spinning, and can significantly improves yarn and existed compact spinning process Hairiness number and intensity etc. performance, also increasingly ground in field of textiles, compact spinning process by wide popularization and application Study carefully the concern of personnel.
At present, the method that integrated composite spinning uses is mainly air-flowing type integrated composite spinning, such as patent CN104131371A is disclosed A kind of collecting-spinning device, including drafting system and the apparatus for collecting that is arranged on before drafting system, drafting system at least wrap A front roller and the front leather roller tangent with front roller are included, apparatus for collecting includes twisting resistance roller, resistance twist roller, negative-pressure air-suction abnormity Pipe, air-flow prerotation vane and open-work cushion rubber, twisting resistance roller are arranged on before front roller, and negative-pressure air-suction special pipe is arranged on front roller Between twisting resistance roller, open-work cushion rubber is set on twisting resistance roller and resistance twist roller is pressed on open-work cushion rubber, negative-pressure air-suction abnormity It to be close on the upside of pipe on open-work cushion rubber, air-flow prerotation vane is arranged between front leather roller and resistance twist roller, though above-mentioned collecting-spinning device It is so simple in construction, need not change spinning frame, but carry out needing the higher negative-pressure air-flow of pressure during air-flow boundling, just can guarantee that final The quality of the integrated composite yarn of formation, the energy consumption for carrying out integrated composite spinning are higher.
In order to further reduce energy consumption, the cost of integrated composite spinning is reduced, researcher has carried out substantial amounts of research, but studies Improvement of the personnel for apparatus for collecting is concentrated mainly on the shape for changing and gathering groove, such as patent CN104975385 discloses one Kind improves the device of the integrated composite spinning of air-breathing slot structure form, and air-breathing groove slotted eye axis direction is improved into centre has interruption Subsection setup, it is more reasonable that it can configure the negative pressure flow of whole agglomeration, while improves the air-breathing slot structure tool of setting There is the self-cleaning function to grid ring, although above-mentioned collecting-spinning device saves the gas for carrying out integrated composite spinning to a certain extent Stream consumption, improves the spinning effect of compact spinning, but carries out still needing the higher negative-pressure air-flow of pressure during integrated composite spinning, above-mentioned Improve and do not solve the shortcomings that compact spinning power consumption is high inherently.
Therefore, study a kind of pressure of negative-pressure air-flow when can effectively reduce integrated composite spinning and ensure final obtained gather The integrated composite spinning method tool of the quality of yarn is of great significance.
The content of the invention
The invention aims to overcome above-mentioned deficiency of the prior art, by installing guiding device in Nesting Zone, So as to provide it is a kind of can effectively reduce integrated composite spinning when negative-pressure air-flow pressure and ensure the product of final obtained integrated composite yarn The integrated composite spinning method of matter.
In order to achieve the above object, the technical solution adopted by the present invention is:
A kind of integrated composite spinning method, the overhung of grid ring is fixed with guiding device, the Nesting Zone in Nesting Zone Jaw is exported between twist triangle zone positioned at spinning ring front roller is gathered, and Nesting Zone is mainly by grid ring and air draught flute Pipe form, the air draught flute pipe upper end, which is provided with, gathers groove, and grid ring, which is covered in, gathers groove top, the bottom surface of the guiding device with The distance on grid ring surface is 1~5mm, and distance too conference influences draught effect;
Hollow cavity is offered in the guiding device, the direction of hollow cavity inlet and outlet is identical with sliver traffic direction, Hollow cavity connects with space in the groove for gathering groove;Gather groove with hollow cavity to be connected, negative-pressure air-flow is provided for hollow cavity;
The hollow cavity connects with two top inlet channels and a side inlet channel, the top inlet channel Airflow direction perpendicular to grid ring, in the case where gathering groove and providing the less negative-pressure air-flow of pressure, top inlet channel can To provide air-flow vertically downward for hollow cavity, the sliver in Nesting Zone is set to adsorb in grid ring, two top air inlets are led to Road is located on the straight line parallel with sliver traffic direction, in order to ensures the air-flow entered by top inlet channel Can be relative to sliver vertically downward, the side inlet channel is the tapered configuration that air inlet is big and gas outlet is small, not The speed of side inlet channel exit air-flow can be accelerated on the premise of intensified negative pressure air-flow, realize the optimization of spinning effect, The airflow direction of the side inlet channel gas outlet and the angle of grid ring are 15~60 °, during side inlet channel can make Air-flow in cavity body produces lateral flow, so that the sliver outer layer fiber in hollow cavity occurs laterally diverted and wrapped The surface of institute's yarn is twined, reduces the filoplume of institute's yarn, improves the strength of institute's yarn, ensures final obtained integrated composite yarn Quality.
As preferable technical scheme:
A kind of integrated composite spinning method as described above, in order to ensure two top inlet channels and a side inlet channel The air-flow of connection will not be produced and interfered, and the orientation of top inlet channel and side inlet channel needs to meet certain condition, Specially:Top inlet channel gas outlet center is equal with the height of side inlet channel gas outlet center, or top air inlet Passage gas outlet center is higher 2~5mm than side inlet channel gas outlet center;Side inlet channel gas outlet center is with crossing two The distance between top inlet channel gas outlet center and plane perpendicular to two tops inlet channel gas outlet are 3~8mm; Cross side inlet channel gas outlet center and perpendicular to two top inlet channel gas outlet center lines plane by the center Line is divided into two sections, wherein one section of length is the 0.3~0.5 of the line of centres length.
A kind of integrated composite spinning method as described above, a length of 20~25mm for gathering groove, a width of 1~3mm;The collection The fluting direction of poly- groove is in 10~30 ° of angles perpendicular to sliver traffic direction, or with sliver traffic direction, is collected in the prior art The fluting direction of poly- groove can only tilt, it is impossible to perpendicular to sliver traffic direction, because only that the inclined groove that gathers can just make sliver The rolling or surface fiber for producing transverse direction in a forward direction are shifted, and the present invention adds the water conservancy diversion with side inlet channel After device, gather the fluting direction of groove also can make sliver produce horizontal rolling in a forward direction perpendicular to sliver traffic direction Or surface fiber shifts;The pressure for gathering negative-pressure air-flow in groove is -500~-1000Pa.Traditional integrated composite spinning is born The pressure of pressure gas stream be generally -2000Pa and its more than, the present invention greatly reduces the pressure of integrated composite spinning negative-pressure air-flow, reduces The energy consumption of integrated composite spinning, has saved resource and cost.
A kind of integrated composite spinning method as described above, during spinning, sliver number be 10~80 English branch, and spindle rotating speed is 4000 ~18000rpm, the twist are 400~1200 sth. made by twisting/m, and regular roving feeding is 3~5g/10m.
A kind of integrated composite spinning method as described above, the groove that gathers are fully located in the orthographic projection of hollow cavity, or 1~5mm of orthographic projection of hollow cavity is stretched out at the both ends for gathering groove.
A kind of integrated composite spinning method as described above, the hollow cavity are rectangular-shape or semi-cylindrical, rectangular-shape The height of hollow cavity is 4~8mm, and the height of semi-cylindrical hollow cavity is 10~25mm.
A kind of integrated composite spinning method as described above, length of the hollow cavity along sliver traffic direction is 10~25mm.
A kind of integrated composite spinning method as described above, the air inlet of the top inlet channel is long groove shape or poroid, long A length of 2~5mm of groove, a width of 2~3mm, a diameter of 1~3mm in hole;A length of the 5 of the air inlet of the side inlet channel~ 15mm, a width of 2~3mm, a length of 2~5mm of the gas outlet of side inlet channel, a width of 2~3mm.
A kind of integrated composite spinning method as described above, the side inlet channel is straight line tapered configuration.
A kind of integrated composite spinning method as described above, the guiding device are concave architecture, and top is a horizontal plane, water The vertical plane of plane and both sides is connected by inclined-plane, and the air inlet of top inlet channel is opened up in the horizontal plane, and side air inlet is led to The air inlet in road is opened on an inclined-plane.
Beneficial effect:
(1) a kind of integrated composite spinning method of the invention, compared with traditional integrated composite spinning method, it is necessary to negative-pressure air-flow pressure Power is smaller while can ensure the quality of final obtained integrated composite yarn, greatly reduces the energy consumption of integrated composite spinning, has saved life Cost is produced, there is fabulous practical value and promotional value;
(2) a kind of integrated composite spinning method of the invention, it is simple in construction, it is easily installed realization.
Brief description of the drawings
Fig. 1 is the structural representation of the collecting-spinning device of the present invention;
Fig. 2 is the diagrammatic cross-section of the guiding device of the present invention;
Fig. 3 is the structural representation of the guiding device of the present invention;
Fig. 4 is position view of the guiding device in Nesting Zone of the present invention;
Wherein, 1- front rollers, 2- guiding devices, 3- slivers, 4- air draught flute pipes, 5- tops inlet channel, the air inlet of 6- sides Passage, 7- hollow cavities, 8- grid rings, 9- gather groove.
Embodiment
The invention will be further elucidated with reference to specific embodiments.It should be understood that these embodiments are merely to illustrate this hair Bright rather than limitation the scope of the present invention.In addition, it is to be understood that after the content of the invention lectured has been read, art technology Personnel can make various changes or modifications to the present invention, and these equivalent form of values equally fall within the application appended claims and limited Fixed scope.
Embodiment 1
A kind of integrated composite spinning method, as depicted in figs. 1 and 2, the overhung of grid ring 8 is fixed with water conservancy diversion in Nesting Zone Device 2, Nesting Zone export jaw between twist triangle zone positioned at spinning ring front roller 1 is gathered, Nesting Zone mainly by Grid ring 8 and air draught flute pipe 4 form, and the upper end of air draught flute pipe 4, which is provided with, gathers groove 9, and grid ring 8, which is covered in, gathers the top of groove 9, water conservancy diversion The bottom surface of device 2 and the distance on the surface of grid ring 8 are 3mm;
Guiding device 2 is concave architecture, and top is a horizontal plane, and the vertical plane of horizontal plane and both sides is connected by inclined-plane Connect, the air inlet of top inlet channel 5 is opened up in the horizontal plane, and the air inlet of side inlet channel 6 is opened on an inclined-plane;
Hollow cavity 7 is offered in guiding device 2, the direction that hollow cavity 7 is imported and exported is identical with the traffic direction of sliver 3, Space connects in groove of the hollow cavity 7 with gathering groove 9;
As shown in figure 3, hollow cavity 7 is rectangular-shape, the height of rectangular-shape hollow cavity 7 is 6mm, hollow cavity 7 Length along the traffic direction of sliver 3 is 18mm;
Hollow cavity 7 connects with two top inlet channels 5 and a side inlet channel 6, the gas of top inlet channel 5 Stream direction is located on the straight line parallel with the traffic direction of sliver 3 perpendicular to grid ring 8, two top inlet channels 5, side Inlet channel 6 is the straight line tapered configuration that air inlet is big and gas outlet is small, and tapered configuration can not increase negative-pressure air-flow On the premise of can accelerate the speed of the exit air-flow of side inlet channel 6, realize the optimization of spinning effect, side inlet channel The airflow direction of 6 gas outlets and the angle of grid ring 8 are 25 °;
The air inlet of top inlet channel 5 is long groove shape, a length of 3mm of elongated slot, a width of 2mm;Side inlet channel 6 enters A length of 10mm of gas port, a width of 3mm, a length of 3mm of the gas outlet of side inlet channel 6, a width of 2mm;
The gas outlet center of top inlet channel 5 is equal with the height of the gas outlet center of side inlet channel 6, and side air inlet is led to The gas outlet center of road 6 is with crossing two gas outlet centers of top inlet channel 5 and perpendicular to two gas outlets of top inlet channel 5 The distance between plane is 6mm;Cross the gas outlet center of side inlet channel 6 and perpendicular to two gas outlets of top inlet channel 5 The line of centres is divided into two sections by the plane of the line of centres, wherein one section of length is the 0.5 of the line of centres length;
As shown in figure 4, the orthographic projection 2mm of hollow cavity 7 is stretched out at the both ends for gathering groove 9, gather a length of 22mm of groove 9, it is wide For 2mm;The fluting direction and the traffic direction of sliver 3 for gathering groove 9 are in 15 ° of angles, gather the pressure of negative-pressure air-flow in groove 9 for- 600Pa。
During spinning, sliver number is 30 English branch, and spindle rotating speed is 11000rpm, and the twist is 700 sth. made by twisting/m, and regular roving feeding is 4g/10m, the Unevenness CV % values of final obtained yarn are 12.44, and -40% details number is 35/km ,+35% slubbing number For 275/km, fracture strength 23.75cN/tex, elongation at break 7.89%.
Embodiment 2
A kind of integrated composite spinning method, the overhung of grid ring is fixed with guiding device in Nesting Zone, and Nesting Zone is located at Gather spinning ring front roller and export jaw between twist triangle zone, Nesting Zone is mainly by grid ring and air draught flute pipe group Into air draught flute pipe upper end, which is provided with, gathers groove, and grid ring, which is covered in, gathers groove top, bottom surface and the grid ring surface of guiding device Distance is 1mm;
Guiding device is concave architecture, and top is a horizontal plane, and the vertical plane of horizontal plane and both sides is connected by inclined-plane, The air inlet of top inlet channel is opened up in the horizontal plane, and the air inlet of side inlet channel is opened on an inclined-plane;
Hollow cavity is offered in guiding device, the direction of hollow cavity inlet and outlet is identical with sliver traffic direction, hollow Cavity connects with space in the groove for gathering groove;
Hollow cavity is semi-cylindrical, and the height of semi-cylindrical hollow cavity is 25mm, and hollow cavity is along sliver operation side To length be 25mm;
Hollow cavity connects with two top inlet channels and a side inlet channel, the air-flow side of top inlet channel It is located to perpendicular to grid ring, two top inlet channels on the straight line parallel with sliver traffic direction, side air inlet is led to Road is the straight line tapered configuration that air inlet is big and gas outlet is small, and tapered configuration can be on the premise of negative-pressure air-flow not be increased The speed of side inlet channel exit air-flow can be accelerated, realize the optimization of spinning effect, side inlet channel gas outlet Airflow direction and the angle of grid ring are 60 °;
The air inlet of top inlet channel is poroid, a diameter of 3mm in hole;The air inlet of side inlet channel it is a length of 15mm, a width of 3mm, a length of 5mm of the gas outlet of side inlet channel, a width of 3mm;
Top inlet channel gas outlet center is higher 5mm than side inlet channel gas outlet center, the outlet of side inlet channel 6 Mouthful center and cross two top inlet channel gas outlet centers and between the plane of two tops inlet channel gas outlet Distance be 8mm;Cross side inlet channel gas outlet center and perpendicular to two top inlet channel gas outlet center lines The line of centres is divided into two sections by plane, wherein one section of length is the 0.5 of the line of centres length;
Gather groove to be fully located in the orthographic projection of hollow cavity, gather a length of 25mm of groove, a width of 3mm;Gather opening for groove Perpendicular to sliver traffic direction, the pressure for gathering negative-pressure air-flow in groove is -1000Pa in groove direction.
During spinning, sliver number is 80 English branch, and spindle rotating speed is 18000rpm, and the twist is 1200 sth. made by twisting/m, and regular roving feeding is 3g/10m, the Unevenness CV % values of final obtained yarn are 16.35, and -40% details number is 350/km, and+35% slubbing is individual Number is 670/km, fracture strength 22.63cN/tex, elongation at break 7.21%.
Embodiment 3
A kind of integrated composite spinning method, the overhung of grid ring is fixed with guiding device in Nesting Zone, and Nesting Zone is located at Gather spinning ring front roller and export jaw between twist triangle zone, Nesting Zone is mainly by grid ring and air draught flute pipe group Into air draught flute pipe upper end, which is provided with, gathers groove, and grid ring, which is covered in, gathers groove top, bottom surface and the grid ring surface of guiding device Distance is 5mm;
Guiding device is concave architecture, and top is a horizontal plane, and the vertical plane of horizontal plane and both sides is connected by inclined-plane, The air inlet of top inlet channel is opened up in the horizontal plane, and the air inlet of side inlet channel is opened on an inclined-plane;
Hollow cavity is offered in guiding device, the direction of hollow cavity inlet and outlet is identical with sliver traffic direction, hollow Cavity connects with space in the groove for gathering groove;
Hollow cavity is semi-cylindrical, and the height of semi-cylindrical hollow cavity is 10mm, and hollow cavity is along sliver operation side To length be 10mm;
Hollow cavity connects with two top inlet channels and a side inlet channel, the air-flow side of top inlet channel It is located to perpendicular to grid ring, two top inlet channels on the straight line parallel with sliver traffic direction, side air inlet is led to Road is the straight line tapered configuration that air inlet is big and gas outlet is small, and tapered configuration can be on the premise of negative-pressure air-flow not be increased The speed of side inlet channel exit air-flow can be accelerated, realize the optimization of spinning effect, side inlet channel gas outlet Airflow direction and the angle of grid ring are 15 °;
The air inlet of top inlet channel is poroid, a diameter of 1mm in hole;The air inlet of side inlet channel it is a length of 5mm, a width of 2mm, a length of 2mm of the gas outlet of side inlet channel, a width of 2mm;
Top inlet channel gas outlet center is higher 2mm than side inlet channel gas outlet center, the outlet of side inlet channel 6 Mouthful center and cross two top inlet channel gas outlet centers and between the plane of two tops inlet channel gas outlet Distance be 3mm;Cross side inlet channel gas outlet center and perpendicular to two top inlet channel gas outlet center lines The line of centres is divided into two sections by plane, wherein one section of length is the 0.3 of the line of centres length;
The orthographic projection 5mm of hollow cavity is stretched out at the both ends for gathering groove, gathers a length of 20mm, a width of 1mm of groove;Gather groove Fluting direction and sliver traffic direction are in 10 ° of angles, and the pressure for gathering negative-pressure air-flow in groove is -500Pa.
During spinning, sliver number is 10 English branch, and spindle rotating speed is 4000rpm, and the twist is 400 sth. made by twisting/m, regular roving feeding 5g/ 10m, the Unevenness CV % values of final obtained yarn are 9.89, and -40% details number is 0/km, and+35% slubbing number is 2 Individual/km, fracture strength 24.11cN/tex, elongation at break 8.57%.
Embodiment 4
A kind of integrated composite spinning method, the overhung of grid ring is fixed with guiding device in Nesting Zone, and Nesting Zone is located at Gather spinning ring front roller and export jaw between twist triangle zone, Nesting Zone is mainly by grid ring and air draught flute pipe group Into air draught flute pipe upper end, which is provided with, gathers groove, and grid ring, which is covered in, gathers groove top, bottom surface and the grid ring surface of guiding device Distance is 4mm;
Guiding device is concave architecture, and top is a horizontal plane, and the vertical plane of horizontal plane and both sides is connected by inclined-plane, The air inlet of top inlet channel is opened up in the horizontal plane, and the air inlet of side inlet channel is opened on an inclined-plane;
Hollow cavity is offered in guiding device, the direction of hollow cavity inlet and outlet is identical with sliver traffic direction, hollow Cavity connects with space in the groove for gathering groove;
Hollow cavity is rectangular-shape, and the height of rectangular-shape hollow cavity is 8mm, and hollow cavity is along sliver traffic direction Length be 18mm;
Hollow cavity connects with two top inlet channels and a side inlet channel, the air-flow side of top inlet channel It is located to perpendicular to grid ring, two top inlet channels on the straight line parallel with sliver traffic direction, side air inlet is led to Road is the straight line tapered configuration that air inlet is big and gas outlet is small, and tapered configuration can be on the premise of negative-pressure air-flow not be increased The speed of side inlet channel exit air-flow can be accelerated, realize the optimization of spinning effect, side inlet channel gas outlet Airflow direction and the angle of grid ring are 15 °;
The air inlet of top inlet channel is long groove shape, a length of 2mm of elongated slot, a width of 2mm;The air inlet of side inlet channel The a length of 5mm, a width of 3mm, a length of 2mm of the gas outlet of side inlet channel, a width of 2mm of mouth;
Top inlet channel gas outlet center is higher 2mm than side inlet channel gas outlet center, the outlet of side inlet channel 6 Mouthful center and cross two top inlet channel gas outlet centers and between the plane of two tops inlet channel gas outlet Distance be 3mm;Cross side inlet channel gas outlet center and perpendicular to two top inlet channel gas outlet center lines The line of centres is divided into two sections by plane, wherein one section of length is the 0.3 of the line of centres length;
The orthographic projection 1mm of hollow cavity is stretched out at the both ends for gathering groove, gathers a length of 20mm, a width of 1mm of groove;Gather groove Fluting direction and sliver traffic direction are in 30 ° of angles, and the pressure for gathering negative-pressure air-flow in groove is -700Pa.
During spinning, sliver number is 20 English branch, and spindle rotating speed is 5000rpm, and the twist is 500 sth. made by twisting/m, and regular roving feeding is 4.5g/10m, the mechanical property Unevenness CV % values of final obtained yarn are 10.78, and -40% details number is 0/km ,+ 35% slubbing number is 5/km, fracture strength 23.85cN/tex, elongation at break 8.11%.
Embodiment 5
A kind of integrated composite spinning method, the overhung of grid ring is fixed with guiding device in Nesting Zone, and Nesting Zone is located at Gather spinning ring front roller and export jaw between twist triangle zone, Nesting Zone is mainly by grid ring and air draught flute pipe group Into air draught flute pipe upper end, which is provided with, gathers groove, and grid ring, which is covered in, gathers groove top, bottom surface and the grid ring surface of guiding device Distance is 1mm;
Guiding device is concave architecture, and top is a horizontal plane, and the vertical plane of horizontal plane and both sides is connected by inclined-plane, The air inlet of top inlet channel is opened up in the horizontal plane, and the air inlet of side inlet channel is opened on an inclined-plane;
Hollow cavity is offered in guiding device, the direction of hollow cavity inlet and outlet is identical with sliver traffic direction, hollow Cavity connects with space in the groove for gathering groove;
Hollow cavity is rectangular-shape, and the height of rectangular-shape hollow cavity is 4mm, and hollow cavity is along sliver traffic direction Length be 22mm;
Hollow cavity connects with two top inlet channels and a side inlet channel, the air-flow side of top inlet channel It is located to perpendicular to grid ring, two top inlet channels on the straight line parallel with sliver traffic direction, side air inlet is led to Road is the straight line tapered configuration that air inlet is big and gas outlet is small, and tapered configuration can be on the premise of negative-pressure air-flow not be increased The speed of side inlet channel exit air-flow can be accelerated, realize the optimization of spinning effect, side inlet channel gas outlet Airflow direction and the angle of grid ring are 15 °;
The air inlet of top inlet channel is long groove shape, a length of 5mm of elongated slot, a width of 3mm;The air inlet of side inlet channel The a length of 5mm, a width of 3mm, a length of 2mm of the gas outlet of side inlet channel, a width of 2mm of mouth;
Top inlet channel gas outlet center is higher 2mm than side inlet channel gas outlet center, the outlet of side inlet channel 6 Mouthful center and cross two top inlet channel gas outlet centers and between the plane of two tops inlet channel gas outlet Distance be 3mm;Cross side inlet channel gas outlet center and perpendicular to two top inlet channel gas outlet center lines The line of centres is divided into two sections by plane, wherein one section of length is the 0.4 of the line of centres length;
Gather groove to be fully located in the orthographic projection of hollow cavity, gather a length of 20mm of groove, a width of 1mm;Gather opening for groove Groove direction and sliver traffic direction are in 20 ° of angles, and the pressure for gathering negative-pressure air-flow in groove is -800Pa.
During spinning, sliver number is 30 English branch, and spindle rotating speed is 6000rpm, and the twist is 600 sth. made by twisting/m, and regular roving feeding is 3.5g/10m, the Unevenness CV % values of final obtained yarn are 11.65, and -40% details number is 30/km, and+35% slubbing is individual Number is 260/km, fracture strength 22.86cN/tex, elongation at break 7.56%.

Claims (10)

1. a kind of integrated composite spinning method, it is characterized in that:The overhung of grid ring is fixed with guiding device in Nesting Zone, described The bottom surface of guiding device and the distance on grid ring surface are 1~5mm;
Hollow cavity is offered in the guiding device, the direction of hollow cavity inlet and outlet is identical with sliver traffic direction, hollow Cavity connects with space in the groove for gathering groove;
The hollow cavity connects with two top inlet channels and a side inlet channel, the gas of the top inlet channel Stream direction is located on the straight line parallel with sliver traffic direction perpendicular to grid ring, two top inlet channels, the side Square inlet channel is air inlet is big and gas outlet is small tapered configuration, the airflow direction of the side inlet channel gas outlet with The angle of grid ring is 15~60 °.
A kind of 2. integrated composite spinning method according to claim 1, it is characterised in that top inlet channel gas outlet center with The height of side inlet channel gas outlet center is equal, or top inlet channel gas outlet center is than side inlet channel outlet The mouth high 2~5mm in center;Side inlet channel gas outlet center is with crossing two top inlet channel gas outlet centers and perpendicular to two The distance between plane of individual top inlet channel gas outlet is 3~8mm;Cross side inlet channel gas outlet center and perpendicular to The line of centres is divided into two sections by the plane of two top inlet channel gas outlet center lines, wherein one section of length is in this The 0.3~0.5 of heart wire length.
A kind of 3. integrated composite spinning method according to claim 1, it is characterised in that it is described gather groove a length of 20~ 25mm, a width of 1~3mm;The fluting direction for gathering groove is in 10 perpendicular to sliver traffic direction, or with sliver traffic direction ~30 ° of angles, the pressure for gathering negative-pressure air-flow in groove are -500~-1000Pa.
4. a kind of integrated composite spinning method according to claim 3, it is characterised in that during spinning, sliver number is 10~80 English branch, spindle rotating speed are 4000~18000rpm, and the twist is 400~1200 sth. made by twisting/m, and regular roving feeding is 3~5g/10m.
5. a kind of integrated composite spinning method according to claim 1, it is characterised in that the groove that gathers is fully located at middle cavity In the orthographic projection of body, or gather 1~5mm of orthographic projection of the both ends stretching hollow cavity of groove.
A kind of 6. integrated composite spinning method according to claim 1, it is characterised in that the hollow cavity be rectangular-shape or Semi-cylindrical, the height of rectangular-shape hollow cavity is 4~8mm, and the height of semi-cylindrical hollow cavity is 10~25mm.
7. a kind of integrated composite spinning method according to claim 6, it is characterised in that hollow cavity is along sliver traffic direction Length is 10~25mm.
A kind of 8. integrated composite spinning method according to claim 1, it is characterised in that the air inlet of the top inlet channel For long groove shape or poroid, a length of 2~5mm of elongated slot, a width of 2~3mm, a diameter of 1~3mm in hole;The side inlet channel Air inlet a length of 5~15mm, a width of 2~3mm, a length of 2~5mm of the gas outlet of side inlet channel, a width of 2~3mm.
A kind of 9. integrated composite spinning method according to claim 8, it is characterised in that the side inlet channel be straight line gradually Contracting shape structure.
10. a kind of integrated composite spinning method according to claim 1, it is characterised in that the guiding device is undercut shape knot Structure, top are a horizontal plane, and the vertical plane of horizontal plane and both sides is connected by inclined-plane, and the air inlet of top inlet channel is opened in On horizontal plane, the air inlet of side inlet channel is opened on an inclined-plane.
CN201710638376.9A 2017-07-31 2017-07-31 Compact spinning method Active CN107574515B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201710638376.9A CN107574515B (en) 2017-07-31 2017-07-31 Compact spinning method

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201710638376.9A CN107574515B (en) 2017-07-31 2017-07-31 Compact spinning method

Publications (2)

Publication Number Publication Date
CN107574515A true CN107574515A (en) 2018-01-12
CN107574515B CN107574515B (en) 2020-04-17

Family

ID=61034536

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201710638376.9A Active CN107574515B (en) 2017-07-31 2017-07-31 Compact spinning method

Country Status (1)

Country Link
CN (1) CN107574515B (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109295567A (en) * 2018-11-21 2019-02-01 东华大学 A kind of device and method improving Compact-spun Yarn performance

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4953349A (en) * 1988-09-29 1990-09-04 Ernst Fehrer Apparatus for making a yarn
DE4426249C2 (en) * 1994-07-25 2003-08-07 Rieter Ag Maschf Spinning process and spinning machine with covered suction roll on the drafting system
CN2613493Y (en) * 2003-01-27 2004-04-28 上海二纺机股份有限公司 Compact spinning device for ring spinning frame
CN1572925A (en) * 2003-05-21 2005-02-02 里特机械公司 Spinning machine with compressing apparatus
CN101280479A (en) * 2008-05-16 2008-10-08 宁波德昌精密纺织机械有限公司 Yarn-collecting device for compact spinning
CN201952548U (en) * 2011-01-10 2011-08-31 常州市同和纺织机械制造有限公司 Integrated composite spinning device for ring spinning frame
CN102505215A (en) * 2011-11-11 2012-06-20 江南大学 Method for reducing suction energy consumption of lattice apron type compact yarn spinning

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4953349A (en) * 1988-09-29 1990-09-04 Ernst Fehrer Apparatus for making a yarn
DE4426249C2 (en) * 1994-07-25 2003-08-07 Rieter Ag Maschf Spinning process and spinning machine with covered suction roll on the drafting system
CN2613493Y (en) * 2003-01-27 2004-04-28 上海二纺机股份有限公司 Compact spinning device for ring spinning frame
CN1572925A (en) * 2003-05-21 2005-02-02 里特机械公司 Spinning machine with compressing apparatus
CN101280479A (en) * 2008-05-16 2008-10-08 宁波德昌精密纺织机械有限公司 Yarn-collecting device for compact spinning
CN201952548U (en) * 2011-01-10 2011-08-31 常州市同和纺织机械制造有限公司 Integrated composite spinning device for ring spinning frame
CN102505215A (en) * 2011-11-11 2012-06-20 江南大学 Method for reducing suction energy consumption of lattice apron type compact yarn spinning

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109295567A (en) * 2018-11-21 2019-02-01 东华大学 A kind of device and method improving Compact-spun Yarn performance

Also Published As

Publication number Publication date
CN107574515B (en) 2020-04-17

Similar Documents

Publication Publication Date Title
CN103603095B (en) The configuration structure in jet-impingement hole in a kind of air injection air vortex spinning apparatus
CN203977000U (en) A kind of ring spindle yarn negative-pressure air-flow suction-type Siro-spun yarn device
CN1388278A (en) Complex twisting device for air-jet eddy-current spinning
CN107574515A (en) A kind of integrated composite spinning method
CN101476186B (en) Compact spinning method
CN102618974A (en) Device for twisting single yarn into compound yarn in spinning process
CN202786571U (en) Whole-course airflow gathering control drafting device
CN205556890U (en) A palpus strip gathering device for hollow roller is last
CN107326484A (en) A kind of flow-guiding type integrated composite spinning method
CN103060963A (en) One-step spinning machine capable of conducting entwisting clockwise and one-step spinning method
CN205556886U (en) Air current guider with arc inlet channel
CN202786570U (en) Double-area double-channel airflow gathering control drafting device
CN203429302U (en) Airflow guide device used for hollow roller type compact siro spinning
CN216838339U (en) Spinning device with energy-saving gathering function
CN102828289B (en) Low-fiber falling air vortex spinning device
CN106435866A (en) Rotor spinning unit capable of eliminating vortex
CN203007531U (en) Front roller humidifying device
CN2633906Y (en) Aggregation spinning device
CN205741319U (en) Ring blowing device and air intake assembly thereof
CN207699742U (en) A kind of New Vortex spinning jet nozzle structure
CN201162087Y (en) Integrated composite spinning gathering apparatus
CN205556898U (en) Many horn mouths of fixed connection formula device
CN204570128U (en) A kind of ring spinning line process units
CN204491113U (en) Pneumatic lifting head device
CN107904710A (en) A kind of New Vortex spinning jet nozzle structure

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant