CN101476180A - Self-twisting hollow ingot special for jet air vortex spinning - Google Patents

Self-twisting hollow ingot special for jet air vortex spinning Download PDF

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Publication number
CN101476180A
CN101476180A CNA2009100458080A CN200910045808A CN101476180A CN 101476180 A CN101476180 A CN 101476180A CN A2009100458080 A CNA2009100458080 A CN A2009100458080A CN 200910045808 A CN200910045808 A CN 200910045808A CN 101476180 A CN101476180 A CN 101476180A
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China
Prior art keywords
hollow ingot
self
fiber entry
passage
diameter
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CNA2009100458080A
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Chinese (zh)
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CN101476180B (en
Inventor
薛文良
程隆棣
俞建勇
邹专勇
朱如华
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Donghua University
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Donghua University
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    • DTEXTILES; PAPER
    • D01NATURAL OR MAN-MADE THREADS OR FIBRES; SPINNING
    • D01HSPINNING OR TWISTING
    • D01H1/00Spinning or twisting machines in which the product is wound-up continuously
    • D01H1/11Spinning by false-twisting
    • D01H1/115Spinning by false-twisting using pneumatic means

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Textile Engineering (AREA)
  • Spinning Or Twisting Of Yarns (AREA)

Abstract

The invention relates to a self-twist hollow ingot special for jet blast vortex spinning which includes a fibre inlet (1) and a hollow ingot channel (2), a surface groove (3) is opened on the fibre inlet (1) and the hollow ingot channel (2), the fibre inlet (1) diameter D1 is larger than the hollow ingot channel (2) diameter D2, the fibre inlet (1) chamfer angle theta is 30-60 degree, an inner surface of the surface groove (3) is streamline. The self-twist hollow ingot provided by the invention can reduce loss amount of fibre, increase utilization rate of raw material, accordingly reduce cost for producing yarn; at the same time, enhance cohesive force among fibre in yarn greatly, accordingly, strong force of final yarn is increased.

Description

Self-twisting hollow ingot special for jet air vortex spinning
Technical field
The invention belongs to the air-jet eddy-current spinning field, particularly relate to a kind of air-jet eddy-current spinning self-twisting hollow ingot.
Background technology
Air-jet eddy-current spinning becomes present development one of novel spinning technology faster with its high yield excellent properties at a high speed, but still there is certain problem in yarn qualities so far, show that mainly the yarn details is many, powerful low, thereby limited the expansion of its product development Application Areas.Its main cause is: one, from processing method, owing to adopt swirling eddy twisting mode, though efficient has improved greatly with respect to machinery twisting, the decline of fiber control is caused the loss of fiber again easily, thereby make the final yarns details increase and powerful decline; Two, from yarn texture, because the air-jet eddy-current spinning final yarns is that middle parallel fibers adds outer covered fiber, compare with the helical structure of fiber in the ring spinning line, the fibre cohesion of air-jet eddy-current spinning yarn is low, thereby makes yarn strength descend to some extent.Therefore how to optimize yarn texture, improve many, the powerful low problems of details, become and broken through the important topic that air-jet eddy-current spinning further develops bottleneck; Simultaneously, though air-jet eddy-current spinning utilizes air-flow twisted fibers resultant yarn to overcome the big shortcoming of inertia force that twisting parts high speed rotary produces, not only can improve twisting efficiency greatly, and can significantly improve spinning speed and cut down the consumption of energy, but air-flow is strong to the control of fiber not as machinery to the control of fiber, under action of high-speed airflow, the part fiber will break away from the control of air-flow, discharge with air-flow, form the fibre that falls, cause utilization ratio of raw materials to reduce greatly, thereby increase the yarn production cost.
Summary of the invention
Technical problem to be solved by this invention provides a kind of self-twisting hollow ingot special for jet air vortex spinning, to solve the defective that yarn texture is relatively poor in the prior art, details is many, brute force is low.
A kind of self-twisting hollow ingot special for jet air vortex spinning comprises fiber entry (1) and hollow ingot passage (2), has surface grooves (3) on described fiber entry (1) and the hollow ingot passage (2), the diameter D of fiber entry (1) 1Diameter D greater than hollow ingot passage (2) 2, fiber entry (1) chamfering θ is 30 °~60 °, the inner surface of described surface grooves (3) is streamlined.
Described surface grooves (3) is linear or camber line shape.
Described surface grooves (3) has 4~8, is the center annular array distribution with the center of circle of fiber entry (1) and hollow ingot passage (2).
The diameter D of described fiber entry (1) 1Be 3~5mm, the diameter D of hollow ingot passage (2) 2Be 1.2~1.6mm, the width D of surface grooves (3) 3Be 0.1~0.8mm, fiber entry (1) is to the height H of hollow ingot passage (2) 1Be 8~10mm, hollow ingot passage (2) height H 2Be 4~6mm, surface grooves (3) height H 3Be 0.1~1mm.
Beneficial effect
The diameter of fiber entry of the present invention helps entering of fiber greater than the diameter of hollow ingot passage, and the frictional force effect of inlet surface groove, help to resist the withdrawing power of air-flow, reduce the loss amount of fiber, can improve utilization ratio of raw materials, thereby reduce the yarn production cost; Simultaneously when continuous fibre stream enters hollow ingot because the frictional force effect of surface grooves, fiber self will produce certain rotation under swirling eddy drives, and will keep this rotation status to enter the yarn body, by the twist of yarn itself its state is fixed at last, on the one hand because fiber itself reverses the effect of internal stress, cohesive force in the yarn between the fiber will strengthen greatly, thereby improve the brute force of final yarns; The streamlined structure of surface grooves inner surface can prevent that fiber is wounded.
Description of drawings
Fig. 1 is the profile of self-twisting hollow ingot special for jet air vortex spinning of the present invention;
Fig. 2 is the horizontal projection of self-twisting hollow ingot special for jet air vortex spinning of the present invention;
Fig. 3 is the horizontal projection of self-twisting hollow ingot special for jet air vortex spinning of the present invention;
Fig. 4 is the profile of self-twisting hollow ingot special for jet air vortex spinning surface grooves of the present invention.
Wherein, 1-fiber entry, 2-hollow ingot passage, 3-surface grooves, D 1-fiber entry diameter, D 2-hollow ingot channel diameter, D 3-surface grooves width, H 1-fiber entry is to height, the H of hollow ingot passage 2-hollow ingot channel height, H 3-surface grooves height, θ-fiber entry chamfering
The specific embodiment
Below in conjunction with specific embodiment, further set forth the present invention.Should be understood that these embodiment only to be used to the present invention is described and be not used in and limit the scope of the invention.Should be understood that in addition those skilled in the art can make various changes or modifications the present invention after the content of having read the present invention's instruction, these equivalent form of values fall within the application's appended claims institute restricted portion equally.
Embodiment 1
As shown in Figure 1, 2, a kind of self-twisting hollow ingot special for jet air vortex spinning, comprise fiber entry 1 and hollow ingot passage 2, the otherwise rectilinear, surface groove 3 that to have 4 centers of circle with fiber entry 1 and hollow ingot passage 2 on described fiber entry 1 and the hollow ingot passage 2 be the center annular array distribution, the diameter D of described fiber entry 1 1Be 3mm, the diameter D of hollow ingot passage 2 2Be 1.2mm, the width D of surface grooves 3 3Be 0.1mm, fiber entry is to the height H of hollow ingot passage 1Be 8mm, hollow ingot channel height H 2Be 4mm, the surface grooves height H 3Be 0.1mm, fiber entry 1 chamfering θ is 30 °, and the inner surface of described surface grooves 3 is streamlined.
Embodiment 2
Shown in Fig. 1,3, a kind of self-twisting hollow ingot special for jet air vortex spinning, comprise fiber entry 1 and hollow ingot passage 2, the camber line shape surface grooves 3 that to have 8 centers of circle with fiber entry 1 and hollow ingot passage 2 on described fiber entry 1 and the hollow ingot passage 2 be the center annular array distribution, the diameter D of described fiber entry 1 1Be 4mm, the diameter D of hollow ingot passage 2 2Be 1.4mm, the width D of surface grooves 3 3Be 0.4mm, fiber entry is to the height H of hollow ingot passage 1Be 9mm, hollow ingot channel height H 2Be 5mm, the surface grooves height H 3Be 0.4mm, fiber entry 1 chamfering θ is 45 °, and the inner surface of described surface grooves 3 is streamlined.
Embodiment 3
Shown in Fig. 1,3, a kind of self-twisting hollow ingot special for jet air vortex spinning, comprise fiber entry 1 and hollow ingot passage 2, the camber line shape surface grooves 3 that to have 6 centers of circle with fiber entry 1 and hollow ingot passage 2 on described fiber entry 1 and the hollow ingot passage 2 be the center annular array distribution, the diameter D of described fiber entry 1 1Be 5mm, the diameter D of hollow ingot passage 2 2Be 1.6mm, the width D of surface grooves 3 3Be 0.8mm, fiber entry is to the height H of hollow ingot passage 1Be 10mm, hollow ingot channel height H 2Be 6mm, the surface grooves height H 3Be 1mm, fiber entry 1 chamfering θ is 60 °, and the inner surface of described surface grooves 3 is streamlined.

Claims (4)

1. a self-twisting hollow ingot special for jet air vortex spinning is characterized in that: comprise fiber entry (1) and hollow ingot passage (2), have surface grooves (3) on described fiber entry (1) and the hollow ingot passage (2), the diameter D of fiber entry (1) 1Diameter D greater than hollow ingot passage (2) 2, fiber entry (1) chamfering θ is 30 °~60 °, the inner surface of described surface grooves (3) is streamlined.
2. self-twisting hollow ingot special for jet air vortex spinning as claimed in claim 1 is characterized in that: described surface grooves (3) is linear or camber line shape.
3. self-twisting hollow ingot special for jet air vortex spinning as claimed in claim 2 is characterized in that: described surface grooves (3) has 4~8, is the center annular array distribution with the center of circle of fiber entry (1) and hollow ingot passage (2).
4. as the described self-twisting hollow ingot special for jet air vortex spinning of any claim in the claim 1~3, it is characterized in that: the diameter D of described fiber entry (1) 1Be 3~5mm, the diameter D of hollow ingot passage (2) 2Be 1.2~1.6mm, the width D of surface grooves (3) 3Be 0.1~0.8mm, fiber entry (1) is to the height H of hollow ingot passage (2) 1Be 8~10mm, hollow ingot passage (2) height H 2Be 4~6mm, surface grooves (3) height H 3Be 0.1~1mm.
CN2009100458080A 2009-01-23 2009-01-23 Self-twisting hollow ingot special for jet air vortex spinning Expired - Fee Related CN101476180B (en)

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Application Number Priority Date Filing Date Title
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CN101476180B CN101476180B (en) 2010-12-08

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Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102787405A (en) * 2012-07-27 2012-11-21 绍兴文理学院 Hollow spindle with spiral guide grooves
CN102926054A (en) * 2012-11-09 2013-02-13 东华大学 Air injection vortex spinning device with pumping component
CN103031626A (en) * 2011-10-07 2013-04-10 里特机械公司 Thread creation element for spinning position of air jet spinning machine with twist stop element
CN103215704A (en) * 2013-04-09 2013-07-24 东华大学 Ring spinning device with pre-twisting device and method
CN103305979A (en) * 2013-06-24 2013-09-18 东华大学 Air-injection vortex-spinning groove-shaped low-fiber hollow spindle
CN109154110A (en) * 2016-05-26 2019-01-04 里特机械公司 Yarn for fly frame forms element and is equipped with the fly frame that yarn forms element
CN111394838A (en) * 2020-05-06 2020-07-10 江南大学 Hollow spindle for spinning of vortex spinning equipment

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103031626A (en) * 2011-10-07 2013-04-10 里特机械公司 Thread creation element for spinning position of air jet spinning machine with twist stop element
CN103031626B (en) * 2011-10-07 2016-01-20 里特机械公司 For having the yarn forming element of the yarning part of the sir jet spinning machines only turning round element
CN102787405A (en) * 2012-07-27 2012-11-21 绍兴文理学院 Hollow spindle with spiral guide grooves
CN102787405B (en) * 2012-07-27 2014-11-26 绍兴文理学院 Hollow spindle with spiral guide grooves
CN102926054A (en) * 2012-11-09 2013-02-13 东华大学 Air injection vortex spinning device with pumping component
CN102926054B (en) * 2012-11-09 2015-04-22 东华大学 Air injection vortex spinning device with pumping component
CN103215704A (en) * 2013-04-09 2013-07-24 东华大学 Ring spinning device with pre-twisting device and method
CN103215704B (en) * 2013-04-09 2016-02-17 东华大学 A kind of ring spinning apparatus and method carrying pre-twister
CN103305979A (en) * 2013-06-24 2013-09-18 东华大学 Air-injection vortex-spinning groove-shaped low-fiber hollow spindle
CN109154110A (en) * 2016-05-26 2019-01-04 里特机械公司 Yarn for fly frame forms element and is equipped with the fly frame that yarn forms element
CN109154110B (en) * 2016-05-26 2021-06-18 里特机械公司 Yarn forming element for a roving frame and roving frame equipped with a yarn forming element
CN111394838A (en) * 2020-05-06 2020-07-10 江南大学 Hollow spindle for spinning of vortex spinning equipment

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Assignee: Jiangyin Huafang Advanced Technology Development Co., Ltd.

Assignor: Donghua University

Contract record no.: 2011320000365

Denomination of invention: Self-twisting hollow ingot special for jet air vortex spinning

Granted publication date: 20101208

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Open date: 20090708

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CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20101208

Termination date: 20140123