Journal of Textile Research ›› 2021, Vol. 42 ›› Issue (11): 166-172.doi: 10.13475/j.fzxb.20200502308

• Machinery & Accessories • Previous Articles     Next Articles

Effect of structural parameter of relay nozzles on characteristics of flow field in profiled reed of air jet loom

ZHOU Haobang, SHEN Min(), YU Lianqing, XIAO Shichao   

  1. Hubei Key Laboratory of Digital Textile Equipment, Wuhan Textile University, Wuhan, Hubei 430200, China
  • Received:2020-05-07 Revised:2021-08-10 Online:2021-11-15 Published:2021-11-29
  • Contact: SHEN Min E-mail:min_shen18@163.com

Abstract:

In order to improve the speed and stability of weft insertion system of air-jet looms, the k-ε expression in the Reynolds time average equation was used to simulate the resultant flow field of three different relay nozzles,i.e. a single circular hole, a regular triangular hole and a star-shaped hole,in the profiled reed. Under the air supply pressure of 0.2-0.4 MPa and the different auxiliary spray spacing, the combined flow field was simulated revealing the jet velocity and velocity nephogram along the central axis of the flow field. The results show that when the pressure is the same, the velocity of the central axis of the resultant flow field of the triangle hole relay nozzle is the highest, and it has the largest traction force on the yarn; the velocity of the central axis of the resultant flow field of the star-shaped hole relay nozzle is the smallest, and the weft insertion stability is the best. It was also found that the velocity fluctuation of the central axis of the single circular hole relay nozzle is the largest, and the spacing is more than 70 mm, which is not suitable for weft insertion. Several groups of relay nozzles are used for the width of the whole fabric, and the action timing of each group of nozzles were synchronized. Because the useful jet length is not long, the interval between the nozzles should not be too long in order to realize the relay weft insertion.

Key words: air jet loom, relay nozzle, profiled reed, synthetic flow field, numerical simulation, star-shaped nozzle

CLC Number: 

  • TS103.3

Fig.1

Auxiliary nozzle structure"

Fig.2

Signal circular hole auxiliary nozzle. (a)Front view; (b)Sketch map of section structure"

Fig.3

Triangle hole auxiliary nozzle. (a)Front view; (b)Sketch map of section structure"

Fig.4

Star hole auxiliary nozzle. (a)Front view; (b)Sketch map of section structure"

Fig.5

Geometric model of flow field of three auxiliary nozzles converging into reed. (a)Geometry model of profiled reed; (b)Geometric model of synthetic flow field"

Fig.6

Mesh generation of synthetic flow field of main and auxiliary nozzles into reed"

Tab.1

Pressure inlet conditions under different gas supply pressures"

总压P1/
MPa
静压P2/
MPa
湍动能κ/
(m2·s-2)
湍动能耗散率ε/
(m2·s-3)
0.2 198 366 5.7 9 942.8
0.3 297 554 5.1 8 480.5
0.4 396 703 4.8 7 724.4

Fig.7

Nozzles and profiled reed of flow field test device"

Fig.8

Numerical simulation and experimental verification of synthetic flow field of three auxiliary nozzles"

Fig.9

Effect of pass on air velocity along central axis"

Fig.10

Cloud diagram of velocity distribution of three pass types at 0.4 MPa. (a)Single hole; (b)Regular triangle hole; (c)Star hole"

Fig.11

Effect of auxiliary nozzle spacing on air velocity along central axis. (a)Single circular hole; (b)Triangle hole; (c)Star hole type"

Tab.2

Velocity fluctuation under different auxiliary nozzle spacing"

间距L/mm 平均速度/
(m·s-1)
速度差值/
(m·s-1)
速度
波动率/%
55 89.08 18.25 0.204 9
60 88.59 17.00 0.191 9
65 87.84 20.22 23.02
65 87.26 22.21 25.45
75 82.40 30.95 37.54

Fig.12

Effect of pressure on air velocity along central axis. (a)Single circular hole; (b)Triangle hole; (c) Star hole"

Fig.13

Effect of pass size on air velocity along central axis. (a)Single circular hole; (b)Triangle hole; (c) Star hole"

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