EP2431507A1 - Weft insertion apparatus in jet loom - Google Patents
Weft insertion apparatus in jet loom Download PDFInfo
- Publication number
- EP2431507A1 EP2431507A1 EP11178050A EP11178050A EP2431507A1 EP 2431507 A1 EP2431507 A1 EP 2431507A1 EP 11178050 A EP11178050 A EP 11178050A EP 11178050 A EP11178050 A EP 11178050A EP 2431507 A1 EP2431507 A1 EP 2431507A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- weft insertion
- ratio
- jet
- weft
- nozzle
- 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
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- 238000003780 insertion Methods 0.000 title claims abstract description 62
- 230000037431 insertion Effects 0.000 title claims abstract description 62
- 238000002347 injection Methods 0.000 claims abstract description 106
- 239000007924 injection Substances 0.000 claims abstract description 106
- 238000012545 processing Methods 0.000 claims abstract description 16
- 230000003247 decreasing effect Effects 0.000 claims abstract description 8
- 235000014676 Phragmites communis Nutrition 0.000 description 21
- 238000013459 approach Methods 0.000 description 5
- 230000007423 decrease Effects 0.000 description 4
- 230000000694 effects Effects 0.000 description 3
- 230000002411 adverse Effects 0.000 description 2
- 238000002474 experimental method Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 238000009760 electrical discharge machining Methods 0.000 description 1
- 238000009941 weaving Methods 0.000 description 1
Images
Classifications
-
- D—TEXTILES; PAPER
- D03—WEAVING
- D03D—WOVEN FABRICS; METHODS OF WEAVING; LOOMS
- D03D47/00—Looms in which bulk supply of weft does not pass through shed, e.g. shuttleless looms, gripper shuttle looms, dummy shuttle looms
- D03D47/28—Looms in which bulk supply of weft does not pass through shed, e.g. shuttleless looms, gripper shuttle looms, dummy shuttle looms wherein the weft itself is projected into the shed
- D03D47/30—Looms in which bulk supply of weft does not pass through shed, e.g. shuttleless looms, gripper shuttle looms, dummy shuttle looms wherein the weft itself is projected into the shed by gas jet
- D03D47/3006—Construction of the nozzles
- D03D47/302—Auxiliary nozzles
Definitions
- the present invention relates to a weft insertion apparatus in a jet loom, wherein the weft insertion apparatus includes an auxiliary nozzle for weft insertion having an injection hole from which an air jet is ejected to deliver a weft in a weft guiding passage.
- An injection hole 111 of an auxiliary nozzle 11 for weft insertion of the type as illustrated Figs. 9(a), (b) and (c) is directed to a weft guiding passage 14 that is formed by an array of weft guiding holes 131 formed in the dents 13 of a modified reed 12.
- Injection timing at the auxiliary nozzle 11 is matched with the flying timing of a weft Y that flies in the weft guiding passage 14.
- the weft Y in the weft guiding passage 14 is delivered to the end of weft insertion by air jet action from the injection hole 111.
- the numeral T is warps.
- a nozzle hole (an injection hole) is tapered so that the cross-sectional area of the hole is decreased toward the direction of air injection.
- the processing deflection angle ⁇ is an angle between the direction of weft insertion Lo and the axial line of the injection hole 111 when viewed in the extending direction of the modified reed 12
- the jet deflection angle ⁇ is an angle between the direction of weft insertion Lo and a line of the direction of air injection C when viewed in the extending direction of the modified reed 12.
- the line of the direction of air injection C is the line indicating the direction where the pressure of injection is maximum in an air jet.
- the line of the direction of air injection C does not match the axial line 112 of the injection hole 111.
- the direction of air injection C or the jet deflection angle ⁇ changes depending on the internal pressure of the nozzle.
- a measuring device for measuring a direction of air jet as disclosed in Japanese Laid-Open Patent Publication No. 9-176937 is used.
- Fig. 10 is a graph showing results of the experiment.
- An axis abscissa in Fig. 10 denotes internal pressure of the nozzle and an axis ordinate denotes the variation ⁇ in the jet deflection angle ⁇ .
- the axial line 112 of the injection hole 111 in the form of a truncated cone is the axial line of a cone having an apex angle ⁇ , wherein the cone is formed by extending the generatrices (side lines) of the truncated cone.
- the jet deflection angle ⁇ at the time when the internal pressure of the nozzle is Pmax is expressed as 0° at the axis ordinate.
- the curve ⁇ represents the variation in the jet deflection angle ⁇ with respect to the change in internal pressure of the nozzle, i.e., how the jet deflection angle ⁇ is changed on the basis of Pmax as the internal pressure of the nozzle decreases from Pmax.
- the jet deflection angle 6 is changed in a negative direction (i.e., a direction for the air jet to move away from the reed).
- the minimum pressure Pmin for weft insertion refers to minimum pressure required for an air jet from the auxiliary nozzle 11 to reach the weft guiding passage 14 in a manner that the line of the direction of air injection C in the air jet can be defined. At pressures less than the minimum pressure Pmin, an air jet from the auxiliary nozzle 11 diffuses before reaching the weft guiding passage 14, failing to provide the weft Y with effective towing force.
- An object of the invention is to provide an auxiliary nozzle for weft insertion that ensures the direction of air injection stays in a weft guiding passage with high reliability even when the pressure in an air tank supplying air to the auxiliary nozzle is set lower to reduce an amount of air jet.
- a weft insertion apparatus in a jet loom includes an auxiliary nozzle (21) for weft insertion having an injection hole (23) from which an air jet is ejected to deliver a weft (Y) in a weft guiding passage (14).
- the injection hole (23) is tapered so that the cross-sectional area of the hole (23) is decreased toward the direction of air injection of the auxiliary nozzle (21).
- the ratio A is 2.5 or greater.
- the ratio A is 3 or greater.
- the ratio A is 4.5 or greater.
- the injection hole is in the form of a truncated cone.
- maximum pressure for weft insertion refers to a maximum value for internal pressure of the nozzle.
- Minimum pressure for weft insertion refers to the minimum pressure required for an air jet from the auxiliary nozzle to reach the weft guiding passage in a manner that the direction of air injection in the air jet can be defined.
- a tapered angle ⁇ is defined as an angle between the generatrix of the injection hole and the axial line of the injection hole.
- FIG. 1 An overall structure of a weft insertion apparatus including an auxiliary nozzle for weft insertion is the same as that of Fig. 9 .
- Fig. 1(a) is a front view of a part of an auxiliary nozzle 21 for weft insertion and a part of a modified reed 12.
- Fig. 1(b) is a cross-sectional view of Fig. 1(a) taken along the line 1b-1b.
- Fig. 2(a) is a side view of a distal end of the auxiliary nozzle 21. The distal end of the auxiliary nozzle 21 is rounded or arcuate when viewed in the direction of weft insertion Lo.
- Fig. 2(b) is a cross-sectional view of Fig. 2(a) taken along the line 2b-2b.
- Fig. 2(c) is a cross-sectional view of Fig. 2(b) taken along the line 2 c -2 c .
- each of the auxiliary nozzles 21 may be positioned for every specified number of the dents 13.
- the auxiliary nozzle 21 for weft insertion is in the form of a pipe and a distal tip of the auxiliary nozzle 21 is closed.
- the distal portion of the auxiliary nozzle 21 becomes smaller so that the width of the auxiliary nozzle 21 in the direction of weft insertion Lo becomes smaller toward upward.
- a flat portion 22 in the form of a plate is formed in the distal portion of the auxiliary nozzle 21.
- An outer surface 221 of the flat portion 22 faces slightly upward to face the direction of weft insertion Lo.
- the outer surface 221 is parallel to the direction in which each warp T extends.
- the flat portion 22 includes an injection hole 23 that communicates with an air supply passage 211 in the auxiliary nozzle 21.
- the injection hole 23 is configured in tapered form where the cross-sectional area of the hole is decreased toward the direction of air injection. That is, the injection hole 23 is a truncated cone-shaped hole.
- a cone is formed by extending the generatrices (side lines) of the truncated cone of the injection hole 23, and the axial line 231 of the cone (or the injection hole 23) is inclined with respect to the reference line L1 perpendicular to the axial line 212 of the auxiliary nozzle 21 in the pipe form.
- an angle between the reference line L1 and the axial line 231 is defined as a processing elevation angle ⁇ when viewed in the front and rear direction of a weaving machine and in the direction perpendicular to the extending direction of the modified reed 12 (see Fig. 9(a) ).
- the axial line 231 faces slightly upward.
- the injection direction of air actually injected from the injection hole 23 does not match the axial line 231.
- the jet elevation angle ⁇ does not match the processing elevation angle ⁇ .
- a processing deflection angle ⁇ is defined as an angle between the direction of weft insertion Lo (the direction that goes from left to right in the drawing, as in the direction of weft insertion Lo of Fig. 9 ) and the axial line 231. Similar to the relationship between the processing elevation angle ⁇ and the jet elevation angle ⁇ , the jet deflection angle ⁇ does not match the processing deflection angle ⁇ .
- a tapered angle of a cone formed by extending the generatrices (side lines) of the truncated cone of the injection hole 23 is defined as an angle ⁇ between the generatrix of the cone and the axial line 231.
- the ratio A which is a value of ⁇ / ⁇
- the curve E0 in the graph of Fig. 4 represents the variation ⁇ in a jet elevation angle ⁇ with respect to the change in the internal pressure of the nozzle when the ratio A is 3.6.
- the jet elevation angle ⁇ an angle between the line of the direction of air injection C and the reference line L1 viewed in the direction of weft insertion Lo as illustrated in Fig. 2(b) .
- a measuring device for measuring the direction of an air jet as disclosed in Japanese Laid-Open Patent Publication No. 9-176937 is used.
- the curve E1 is the variation ⁇ in the jet elevation angle ⁇ with respect to the change in the internal pressure of the nozzle when the ratio A is 1.3.
- An axis abscissa denotes internal pressure of the nozzle and an axis ordinate denotes the variation ⁇ in the jet elevation angle ⁇ .
- the jet elevation angle at the time when the internal pressure of the nozzle is Pmax is expressed as 0° at the axis ordinate.
- the positive change ⁇ > 0 in the jet elevation angle ⁇ is the situation where a jet elevation angle is directed more upward than the line of the direction of air injection C when the internal pressure of the nozzle is the maximum pressure Pmax.
- the positive change ⁇ > 0 in the jet elevation angle ⁇ is smaller in the ratio A of 3.6 than in the ratio A of 1.3. That is, the magnitude of the upward change in the line of the direction of air injection C from the situation where the internal pressure of the nozzle is the maximum pressure Pmax is smaller in the ratio A of 3.6 than in the ratio A of 1.3.
- the ratio A of 3.6 is preferred to the ratio A of 1.3 to prevent the line of the direction of air injection C from deviating upward from the weft guiding passage 14.
- the curve Do in the graph of Fig. 5 is the variation ⁇ in the jet deflection angle ⁇ of air jet with respect to the change in internal pressure of the nozzle when the ratio A is 3.6.
- the jet deflection angle ⁇ is an angle between the line of the direction of air injection C and the direction of weft insertion Lo as illustrated in Fig. 2(c) when viewed in the extending direction of the modified reed 12 (see Fig. 9(a) ).
- the curve D1 is the variation ⁇ in the jet deflection angle ⁇ with respect to the change in internal pressure of the nozzle when the ratio A is 1.3.
- An axis abscissa denotes internal pressure of the nozzle and an axis ordinate denotes the variation ⁇ in the jet deflection angle ⁇ .
- the jet deflection angle ⁇ at the time when the internal pressure of the nozzle is Pmax is expressed as 0° at the axis ordinate.
- the positive change of the jet deflection angle ⁇ , i.e., ⁇ > 0, means that the line of the direction of air injection C approaches the modified reed 12 than in the case when the internal pressure of the nozzle is the maximum pressure Pmax.
- the negative change of the jet deflection angle ⁇ , i.e., ⁇ ⁇ 0, means that the line of the direction of air injection C moves away from the modified reed 12 than in the case when the internal pressure of the nozzle is the maximum pressure Pmax.
- the negative change ⁇ ⁇ 0 of the jet deflection angle ⁇ is greater, the line of the direction of air injection C moves away from the weft guiding passage 14 of the modified reed 12 greatly.
- the variation ⁇ in the jet deflection angle ⁇ is always positive when the ratio A is 3.6, and the value of the variation ⁇ becomes greater as the internal pressure of the nozzle becomes smaller.
- the ratio A is 1.3
- the variation ⁇ in the jet deflection angle ⁇ is positive on the high-pressure side but negative on the low-pressure side. Since the line of the direction of air injection C is directed upward, if the line of the direction of air injection C moves away from the modified reed 12, the variation ⁇ in the jet deflection angle ⁇ is more likely to deviate upward from the weft guiding passage 14.
- the graph of Fig. 5 indicates that deviation of the line of the direction of air injection C from the weft guiding passage 14 is less likely to occur in the ratio A of 3.6 than in the ratio A of 1.3 when the internal pressure of the nozzle is on the low-pressure side.
- a curve Z in the graph of Fig. 6 represents the variation range ⁇ max between the maximum pressure Pmax and the minimum pressure Pmin of the jet elevation angle ⁇ with respect to the change in the ratio A.
- the variation range ⁇ max is the variation in the jet elevation angle ⁇ when the internal pressure of the nozzle is decreased from the maximum pressure Pmax for weft insertion to the minimum pressure Pmin for weft insertion.
- the minimum pressure Pmin is set as low pressure as possible to such an extend that the line of the direction of air injection C can be measured with the measuring device for measuring a direction of air jet as disclosed in Japanese Laid-Open Patent Publication No. 9-176937 .
- An axis abscissa denotes the ratio A and an axis ordinate denotes the variation range ⁇ max of the jet elevation angle ⁇ .
- a curve H in the graph of Fig. 7 represents the variation range ⁇ max of the jet deflection angle ⁇ with respect to the change in the ratio A.
- the variation range ⁇ max is the variation in the jet deflection angle ⁇ when the internal pressure of the nozzle is decreased from the maximum pressure Pmax for weft insertion to the minimum pressure Pmin for weft insertion.
- An axis abscissa denotes the ratio A and an axis ordinate denotes the variation range ⁇ max of the jet deflection angle ⁇ .
- the positive variation range of jet deflection angle ⁇ i.e., ⁇ max > 0, means that the line of the direction of air injection C approaches the modified reed 12 compared to the case when the internal pressure of the nozzle is the maximum pressure Pmax.
- the negative variation range of the jet deflection angle ⁇ i.e., ⁇ max ⁇ 0, means that the line of the direction of air injection C moves away from the modified reed 12 compared to the case when the internal pressure of the nozzle is the maximum pressure Pmax.
- the variation range ⁇ max of the jet deflection angle ⁇ is negative when the ratio A is 2 or less.
- the smaller the ratio A is the greater the negative variation range of the jet deflection angle ⁇ ( ⁇ max ⁇ 0) becomes.
- the line of the direction of air injection C moves away from the modified reed 12 further. Since the line of the direction of air injection C faces upward, if the line of the direction of air injection C moves away from the modified reed 12, the line of the direction of air injection C is more likely to deviate upward from the weft guiding passage 14.
- the variation range ⁇ max of the jet deflection angle ⁇ is positive when the ratio A is A0 or greater.
- the positive variation range of the jet deflection angle ⁇ ( ⁇ max > 0) becomes greater as the ratio A is greater.
- the positive variation range of the jet deflection angle ⁇ ( ⁇ max > 0) indicates the situation where the line of the direction of air injection C is closer to the modified reed 12 compared to the case where the internal pressure of the nozzle is the maximum pressure Pmax.
- the processing elevation angle ⁇ faces upward, as the line of the direction of air injection C approaches the modified reed 12, the line of the direction of air injection C turns lower.
- the change in the jet elevation angle ⁇ in an upper direction is offset to facilitate positioning of the line of the direction of air injection C in the weft guiding passage 14.
- the value of A0 is greater than 2 but smaller than 2.5. In this embodiment, A0 is 2.2.
- the variation range ⁇ max of the jet deflection angle ⁇ is always positive when the ratio A > A0.
- the variation range ⁇ max of the jet deflection angle ⁇ will not turn negative, thereby facilitating positioning of the line of the direction of air injection C in the weft guiding passage 14 even when the internal pressure of the nozzle becomes the minimum pressure Pmin.
- the positive variation range ( ⁇ max > 0) is greater, the line of the direction of air injection C is lowered and positioning of the line of the direction of air injection C in the weft guiding passage 14 is facilitated.
- the ratio A is 3
- the line of the direction of air injection C is easily positioned in the weft guiding passage 14 compared to the case where the ratio A is 2.5.
- the ratio A exceeds 3.6, an increment of the positive variation range ( ⁇ max > 0) becomes smaller.
- the ratio A is 4. 5
- the positive variation range ⁇ max > 0 is almost steady.
- the processing deflection angle ⁇ is constant, the smaller the ratio A is, the smaller the taper angle ⁇ is.
- the injection hole 23 is easier to process as the taper angle ⁇ is smaller.
- the ratio A of 4.5 or less is desirable.
- Fig. 8(b) is a graph illustrating the changes in the intersection points Cn in the cases where the ratios A are 1.3, 2, 2.5, 3, and 3.6 when the internal pressure of the nozzle as illustrated in the waveform Np in Fig. 3 is changed from the maximum pressure Pmax for weft insertion to the minimum pressure Pmin for weft insertion.
- An axis abscissa x denotes the direction of weft insertion Lo while an axis ordinate y denotes the upper direction.
- the plane of x-y coordinates represents the imaginary plane 142.
- Intersection points C0 and C1 are the change in intersection points when the ratio A is 1.3.
- Intersection points C0 and C2 are the change in intersection points when the ratio A is 2.
- Intersection points C0 and C3 are the change in intersection points when the ratio A is 2.5.
- Intersection points C0 and C4 are the change in intersection points when the ratio A is 3.
- Intersection points C0 and C5 are the change in intersection points when the ratio A is 3.6.
- intersection point C0 is the intersection point when the internal pressure of the nozzle is the maximum pressure Pmax.
- intersection points C1, C2, C3, C4 and C5 are the intersection points when the internal pressure of the nozzle is the minimum pressure Pmin.
- intersection point C2 is near the upper edge 143 of the back wall surface 141.
- intersection points C0 and C3 are within the back wall surface 141.
- intersection points C0 and C4 are within the back wall surface 141.
- intersection points C0 and C5 are within the back wall surface 141.
- intersection point Cn In the situation where the intersection point Cn deviates upward from the back wall surface 141, an adverse effect on the flying position of the weft Y becomes prominent, and decrease in the flying speed of the weft and failure of weft insertion are likely to occur.
- the intersection point C2 is near the upper edge 143 of the back wall surface 141 when the ratio A is 2 while the intersection point C3 is within the back wall surface 141 when the ratio A is 2.5. That is, when the ratio A is 2.5, deviation of the intersection point Cn upward from the back wall surface 141 is inhibited with high reliability.
- the intersection points C0 and C4 are both positioned within the back wall surface 141.
- the ratio A is 3.0, deviation of the intersection point Cn upward from the back wall surface 141 is inhibited with higher reliability.
- the intersection point C4 is positioned inside the upper edge 143 of the back wall surface 141.
- the intersection point C5 is positioned further inside (or lower than) the intersection point C4. That is, when the ratio A is 3.6, deviation of the intersection point Cn upward from the back wall surface 141 is inhibited with even higher reliability.
- the present invention may be embodied in the following embodiment.
- the injection hole may be a hole in the form of a truncated elliptic cone.
- a weft insertion apparatus in a jet loom wherein the weft insertion apparatus includes an auxiliary nozzle (21) for weft insertion having an injection hole (23) from which air jet is ejected to deliver a weft (Y) in a weft guiding passage (14), is provided.
- the injection hole (23) is tapered so that the cross-sectional area of the hole (23) is decreased toward the direction of air injection of the auxiliary nozzle (21).
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Abstract
Description
- The present invention relates to a weft insertion apparatus in a jet loom, wherein the weft insertion apparatus includes an auxiliary nozzle for weft insertion having an injection hole from which an air jet is ejected to deliver a weft in a weft guiding passage.
- An
injection hole 111 of anauxiliary nozzle 11 for weft insertion of the type as illustratedFigs. 9(a), (b) and (c) is directed to aweft guiding passage 14 that is formed by an array ofweft guiding holes 131 formed in thedents 13 of a modifiedreed 12. Injection timing at theauxiliary nozzle 11 is matched with the flying timing of a weft Y that flies in theweft guiding passage 14. The weft Y in theweft guiding passage 14 is delivered to the end of weft insertion by air jet action from theinjection hole 111. The numeral T is warps. - Internal pressure of air in the nozzle that is to be ejected from the injection hole 111 (i.e., air pressure inside the auxiliary nozzle 11) changes as indicated by the waveform Np in the graph of
Fig. 3 . - In an auxiliary nozzle for weft insertion disclosed in Japanese Laid-Open Patent Publication No.
3-97939 injection hole 111 ofFig. 9(c) , a nozzle hole (an injection hole) is tapered so that the cross-sectional area of the hole is decreased toward the direction of air injection. - The inventors of this application conducted an experiment to see the variations in jet deflection angle δ when the internal pressure of the nozzle is changed, on the condition that the relationship between an apex angle θ and a processing deflection angle ψ in the
tapered injection hole 111 disclosed in Japanese Laid-Open Patent Publication No.3-97939 Fig. 9(c) , the processing deflection angle ψ is an angle between the direction of weft insertion Lo and the axial line of theinjection hole 111 when viewed in the extending direction of themodified reed 12, and the jet deflection angle δ is an angle between the direction of weft insertion Lo and a line of the direction of air injection C when viewed in the extending direction of themodified reed 12. The line of the direction of air injection C is the line indicating the direction where the pressure of injection is maximum in an air jet. The line of the direction of air injection C does not match theaxial line 112 of theinjection hole 111. As described below, the direction of air injection C or the jet deflection angle δ changes depending on the internal pressure of the nozzle. - To measure the line of the direction of air injection C, for example, a measuring device for measuring a direction of air jet as disclosed in Japanese Laid-Open Patent Publication No.
9-176937 -
Fig. 10 is a graph showing results of the experiment. An axis abscissa inFig. 10 denotes internal pressure of the nozzle and an axis ordinate denotes the variation Δδ in the jet deflection angle δ. Theaxial line 112 of theinjection hole 111 in the form of a truncated cone is the axial line of a cone having an apex angle θ, wherein the cone is formed by extending the generatrices (side lines) of the truncated cone. In the graph ofFig. 10 , the jet deflection angle δ at the time when the internal pressure of the nozzle is Pmax is expressed as 0° at the axis ordinate. The curve Δδ represents the variation in the jet deflection angle δ with respect to the change in internal pressure of the nozzle, i.e., how the jet deflection angle δ is changed on the basis of Pmax as the internal pressure of the nozzle decreases from Pmax. As apparent from the curve Δδ, when the internal pressure of the nozzle is the minimum pressure Pmin for weft insertion, thejet deflection angle 6 is changed in a negative direction (i.e., a direction for the air jet to move away from the reed). - The minimum pressure Pmin for weft insertion refers to minimum pressure required for an air jet from the
auxiliary nozzle 11 to reach theweft guiding passage 14 in a manner that the line of the direction of air injection C in the air jet can be defined. At pressures less than the minimum pressure Pmin, an air jet from theauxiliary nozzle 11 diffuses before reaching theweft guiding passage 14, failing to provide the weft Y with effective towing force. - According to the graph of
Fig. 10 , when the internal pressure of the nozzle decreases from the maximum pressure Pmax to the minimum pressure Pmin, the jet deflection angle δ changes in a negative direction. Thus, the line of the direction of air injection C is more likely to deviate upward from theweft guiding passage 14. As the maximum pressure Pmax of the internal pressure of the nozzle (or the pressure of an air tank that supplies air to the auxiliary nozzle 11) is set lower to reduce air consumption, the towing force of theauxiliary nozzle 11 is reduced. Thus, an adverse effect of the variation Δδ in the jet deflection angle δ on the flying position of the weft Y becomes prominent when the air injection from theauxiliary nozzle 11 is completed after the distal tip of the weft Y passes through theauxiliary nozzle 11. - An object of the invention is to provide an auxiliary nozzle for weft insertion that ensures the direction of air injection stays in a weft guiding passage with high reliability even when the pressure in an air tank supplying air to the auxiliary nozzle is set lower to reduce an amount of air jet.
- According to one aspect of the invention, a weft insertion apparatus in a jet loom is provided. The weft insertion apparatus includes an auxiliary nozzle (21) for weft insertion having an injection hole (23) from which an air jet is ejected to deliver a weft (Y) in a weft guiding passage (14). The injection hole (23) is tapered so that the cross-sectional area of the hole (23) is decreased toward the direction of air injection of the auxiliary nozzle (21). The ratio A of a tapered angle γ of the injection hole (23) to a processing deflection angle β of the injection hole (23), y/β = A, has the relationship expressed by an inequality (1):
- In one embodiment, the ratio A is 2.5 or greater.
- In another embodiment, the ratio A is 3 or greater.
- In yet another embodiment, the ratio A is 4.5 or greater.
- In still another embodiment, the injection hole is in the form of a truncated cone.
- As used herein, maximum pressure for weft insertion refers to a maximum value for internal pressure of the nozzle.
- Minimum pressure for weft insertion refers to the minimum pressure required for an air jet from the auxiliary nozzle to reach the weft guiding passage in a manner that the direction of air injection in the air jet can be defined.
- A tapered angle γ is defined as an angle between the generatrix of the injection hole and the axial line of the injection hole.
-
-
Fig. 1(a) is a front view illustrating a part of an auxiliary nozzle for weft insertion and a part of a modified reed according to one embodiment of the invention; -
Fig. 1(b) is a cross-sectional view ofFig. 1(a) taken along the line 1 b-1 b; -
Fig. 2(a) is a partial side view of the auxiliary nozzle; -
Fig. 2(b) is a cross-sectional view ofFig. 2(a) taken along theline 2b-2b; -
Fig. 2(c) is a cross-sectional view ofFig. 2(b) taken along theline 2c-2c; -
Fig. 3 is a graph showing the change in the internal pressure of the nozzle; -
Fig. 4 is a graph representing the relationship between the internal pressure of the nozzle and the variation in jet elevation angle; -
Fig. 5 is a graph representing the relationship between the internal pressure of the nozzle and the variation in jet deflection angle; -
Fig. 6 is a graph representing the relationship between a ratio A and a variation range of jet elevation angle; -
Fig. 7 is a graph representing the relationship between the ratio A and a variation range of the jet deflection angle; -
Fig. 8(a) is a partial cross-sectional view illustrating a part of an auxiliary nozzle for weft insertion and a part of a modified reed; -
Fig. 8(b) is a graph of intersection points on an imaginary plane; -
Fig. 9(a) is a side view of a weft insertion apparatus; -
Fig. 9(b) is a partial side view ofFig. 9(a) ; -
Fig. 9(c) is a cross-sectional view ofFig. 9(b) taken along theline 9c-9c; and -
Fig. 10 is a graph showing the variation in jet deflection angle when the ratio A is 1.3. - An embodiment of the invention will be described with reference to
Figs. 1 to 8 . An overall structure of a weft insertion apparatus including an auxiliary nozzle for weft insertion is the same as that ofFig. 9 . -
Fig. 1(a) is a front view of a part of anauxiliary nozzle 21 for weft insertion and a part of a modifiedreed 12.Fig. 1(b) is a cross-sectional view ofFig. 1(a) taken along the line 1b-1b.Fig. 2(a) is a side view of a distal end of theauxiliary nozzle 21. The distal end of theauxiliary nozzle 21 is rounded or arcuate when viewed in the direction of weft insertion Lo.Fig. 2(b) is a cross-sectional view ofFig. 2(a) taken along theline 2b-2b.Fig. 2(c) is a cross-sectional view ofFig. 2(b) taken along theline 2 c -2 c . - In the drawings, a single
auxiliary nozzle 21 is provided. However, as appreciated by those skilled in the art, in the weft apparatus, each of theauxiliary nozzles 21 may be positioned for every specified number of thedents 13. - As illustrated in
Fig. 2(b) , theauxiliary nozzle 21 for weft insertion is in the form of a pipe and a distal tip of theauxiliary nozzle 21 is closed. The distal portion of theauxiliary nozzle 21 becomes smaller so that the width of theauxiliary nozzle 21 in the direction of weft insertion Lo becomes smaller toward upward. Aflat portion 22 in the form of a plate is formed in the distal portion of theauxiliary nozzle 21. Anouter surface 221 of theflat portion 22 faces slightly upward to face the direction of weft insertion Lo. Theouter surface 221 is parallel to the direction in which each warp T extends. - As illustrated in
Figs. 2(b) and (c) , theflat portion 22 includes aninjection hole 23 that communicates with anair supply passage 211 in theauxiliary nozzle 21. Theinjection hole 23 is configured in tapered form where the cross-sectional area of the hole is decreased toward the direction of air injection. That is, theinjection hole 23 is a truncated cone-shaped hole. A cone is formed by extending the generatrices (side lines) of the truncated cone of theinjection hole 23, and theaxial line 231 of the cone (or the injection hole 23) is inclined with respect to the reference line L1 perpendicular to theaxial line 212 of theauxiliary nozzle 21 in the pipe form. - As illustrated in
Fig. 2(b) , an angle between the reference line L1 and theaxial line 231 is defined as a processing elevation angle α when viewed in the front and rear direction of a weaving machine and in the direction perpendicular to the extending direction of the modified reed 12 (seeFig. 9(a) ). Theaxial line 231 faces slightly upward. The injection direction of air actually injected from theinjection hole 23 does not match theaxial line 231. Thus, the jet elevation angle ε does not match the processing elevation angle α. - As illustrated in
Fig. 2(c) , a processing deflection angle β is defined as an angle between the direction of weft insertion Lo (the direction that goes from left to right in the drawing, as in the direction of weft insertion Lo ofFig. 9 ) and theaxial line 231. Similar to the relationship between the processing elevation angle α and the jet elevation angle ε, the jet deflection angle δ does not match the processing deflection angle β. - A tapered angle of a cone formed by extending the generatrices (side lines) of the truncated cone of the
injection hole 23 is defined as an angle γ between the generatrix of the cone and theaxial line 231. - In this embodiment, the ratio A, which is a value of γ/β, is set to 3.6. The curve E0 in the graph of
Fig. 4 represents the variation Δε in a jet elevation angle ε with respect to the change in the internal pressure of the nozzle when the ratio A is 3.6. The jet elevation angle ε an angle between the line of the direction of air injection C and the reference line L1 viewed in the direction of weft insertion Lo as illustrated inFig. 2(b) . To measure the line of direction of air injection C, for example, a measuring device for measuring the direction of an air jet as disclosed in Japanese Laid-Open Patent Publication No.9-176937 - The curve E1 is the variation Δε in the jet elevation angle ε with respect to the change in the internal pressure of the nozzle when the ratio A is 1.3. An axis abscissa denotes internal pressure of the nozzle and an axis ordinate denotes the variation Δε in the jet elevation angle ε. In this graph, the jet elevation angle at the time when the internal pressure of the nozzle is Pmax is expressed as 0° at the axis ordinate. The positive change Δε > 0 in the jet elevation angle ε is the situation where a jet elevation angle is directed more upward than the line of the direction of air injection C when the internal pressure of the nozzle is the maximum pressure Pmax.
- As apparent from the comparison between the curve E0 and the curve E1, the positive change Δε > 0 in the jet elevation angle ε is smaller in the ratio A of 3.6 than in the ratio A of 1.3. That is, the magnitude of the upward change in the line of the direction of air injection C from the situation where the internal pressure of the nozzle is the maximum pressure Pmax is smaller in the ratio A of 3.6 than in the ratio A of 1.3. This means that the ratio A of 3.6 is preferred to the ratio A of 1.3 to prevent the line of the direction of air injection C from deviating upward from the
weft guiding passage 14. - The curve Do in the graph of
Fig. 5 is the variation Δδ in the jet deflection angle δ of air jet with respect to the change in internal pressure of the nozzle when the ratio A is 3.6. The jet deflection angle δ is an angle between the line of the direction of air injection C and the direction of weft insertion Lo as illustrated inFig. 2(c) when viewed in the extending direction of the modified reed 12 (seeFig. 9(a) ). The curve D1 is the variation Δδ in the jet deflection angle δ with respect to the change in internal pressure of the nozzle when the ratio A is 1.3. An axis abscissa denotes internal pressure of the nozzle and an axis ordinate denotes the variation Δδ in the jet deflection angle δ. - In this graph, the jet deflection angle δ at the time when the internal pressure of the nozzle is Pmax is expressed as 0° at the axis ordinate. The positive change of the jet deflection angle δ, i.e., Δδ > 0, means that the line of the direction of air injection C approaches the modified
reed 12 than in the case when the internal pressure of the nozzle is the maximum pressure Pmax. The negative change of the jet deflection angle δ, i.e., Δδ < 0, means that the line of the direction of air injection C moves away from the modifiedreed 12 than in the case when the internal pressure of the nozzle is the maximum pressure Pmax. As the negative change Δδ < 0 of the jet deflection angle δ is greater, the line of the direction of air injection C moves away from theweft guiding passage 14 of the modifiedreed 12 greatly. - As apparent from the comparison between the curve D0 and the curve D1, the variation Δδ in the jet deflection angle δ is always positive when the ratio A is 3.6, and the value of the variation Δδ becomes greater as the internal pressure of the nozzle becomes smaller. When the ratio A is 1.3, the variation Δδ in the jet deflection angle δ is positive on the high-pressure side but negative on the low-pressure side. Since the line of the direction of air injection C is directed upward, if the line of the direction of air injection C moves away from the modified
reed 12, the variation Δδ in the jet deflection angle δ is more likely to deviate upward from theweft guiding passage 14. - The graph of
Fig. 5 indicates that deviation of the line of the direction of air injection C from theweft guiding passage 14 is less likely to occur in the ratio A of 3.6 than in the ratio A of 1.3 when the internal pressure of the nozzle is on the low-pressure side. - A curve Z in the graph of
Fig. 6 represents the variation range Δεmax between the maximum pressure Pmax and the minimum pressure Pmin of the jet elevation angle ε with respect to the change in the ratio A. The variation range Δεmax is the variation in the jet elevation angle ε when the internal pressure of the nozzle is decreased from the maximum pressure Pmax for weft insertion to the minimum pressure Pmin for weft insertion. It is preferred that the minimum pressure Pmin is set as low pressure as possible to such an extend that the line of the direction of air injection C can be measured with the measuring device for measuring a direction of air jet as disclosed in Japanese Laid-Open Patent Publication No.9-176937 weft guiding passage 14. - A curve H in the graph of
Fig. 7 represents the variation range Δδmax of the jet deflection angle δ with respect to the change in the ratio A. The variation range Δδmax is the variation in the jet deflection angle δ when the internal pressure of the nozzle is decreased from the maximum pressure Pmax for weft insertion to the minimum pressure Pmin for weft insertion. An axis abscissa denotes the ratio A and an axis ordinate denotes the variation range Δεmax of the jet deflection angle δ. The positive variation range of jet deflection angle δ, i.e., Δδmax > 0, means that the line of the direction of air injection C approaches the modifiedreed 12 compared to the case when the internal pressure of the nozzle is the maximum pressure Pmax. The negative variation range of the jet deflection angle δ, i.e., Δδmax < 0, means that the line of the direction of air injection C moves away from the modifiedreed 12 compared to the case when the internal pressure of the nozzle is the maximum pressure Pmax. - As apparent from the curve H, the variation range Δδmax of the jet deflection angle δ is negative when the ratio A is 2 or less. On the condition where the ratio A is 2 or less, the smaller the ratio A is, the greater the negative variation range of the jet deflection angle δ (Δδmax < 0) becomes. As the negative variation range of the jet deflection angle δ (Δδmax < 0) becomes greater, the line of the direction of air injection C moves away from the modified
reed 12 further. Since the line of the direction of air injection C faces upward, if the line of the direction of air injection C moves away from the modifiedreed 12, the line of the direction of air injection C is more likely to deviate upward from theweft guiding passage 14. - Provided that the ratio when the variation range Δδmax of the jet deflection angle δ becomes 0 when the internal pressure of the nozzle is changed from the maximum pressure Pmax to the minimum pressure Pmin is defined as A0, the variation range Δδmax of the jet deflection angle δ is positive when the ratio A is A0 or greater. On the condition that the ratio A is the value of A0 or greater, the positive variation range of the jet deflection angle Δδ (δmax > 0) becomes greater as the ratio A is greater. The positive variation range of the jet deflection angle δΔ (δmax > 0) indicates the situation where the line of the direction of air injection C is closer to the modified
reed 12 compared to the case where the internal pressure of the nozzle is the maximum pressure Pmax. Since the processing elevation angle α faces upward, as the line of the direction of air injection C approaches the modifiedreed 12, the line of the direction of air injection C turns lower. Thus, as the line of the direction of air injection C approaches the modifiedreed 12, the change in the jet elevation angle ε in an upper direction is offset to facilitate positioning of the line of the direction of air injection C in theweft guiding passage 14. - The value of A0 is greater than 2 but smaller than 2.5. In this embodiment, A0 is 2.2. As apparent from
Fig. 7 , the variation range Δδmax of the jet deflection angle δ is always positive when the ratio A > A0. Thus, by determining the processing deflection angle β and the tapered angle γ so that the ratio A is equal to or greater than the ratio A0, the variation range Δδmax of the jet deflection angle δ will not turn negative, thereby facilitating positioning of the line of the direction of air injection C in theweft guiding passage 14 even when the internal pressure of the nozzle becomes the minimum pressure Pmin. - As the positive variation range (Δδmax > 0) is greater, the line of the direction of air injection C is lowered and positioning of the line of the direction of air injection C in the
weft guiding passage 14 is facilitated. Thus, when the ratio A is 3, the line of the direction of air injection C is easily positioned in theweft guiding passage 14 compared to the case where the ratio A is 2.5. - If the ratio A exceeds 3.6, an increment of the positive variation range (Δδmax > 0) becomes smaller. When the ratio A is 4. 5, the positive variation range Δδmax > 0 is almost steady. When the processing deflection angle β is constant, the smaller the ratio A is, the smaller the taper angle γ is. The
injection hole 23 is easier to process as the taper angle γ is smaller. Thus, the ratio A of 4.5 or less is desirable. - As illustrated in
Fig. 8(a) , the intersection between animaginary plane 142 flush with theback wall surface 141 of theweft guiding passage 14 and the line of the direction of air injection C of air ejected from theinjection hole 111 is defined as Cn. -
Fig. 8(b) is a graph illustrating the changes in the intersection points Cn in the cases where the ratios A are 1.3, 2, 2.5, 3, and 3.6 when the internal pressure of the nozzle as illustrated in the waveform Np inFig. 3 is changed from the maximum pressure Pmax for weft insertion to the minimum pressure Pmin for weft insertion. An axis abscissa x denotes the direction of weft insertion Lo while an axis ordinate y denotes the upper direction. The plane of x-y coordinates represents theimaginary plane 142. - When the internal pressure of the nozzle is the maximum pressure Pmax, the positions of the intersection points Cn in the cases where the ratios A are 1.3, 2, 2.5, 3 and 3.6 become almost the same. Thus, this intersection is denoted as Co collectively.
- Intersection points C0 and C1 are the change in intersection points when the ratio A is 1.3. Intersection points C0 and C2 are the change in intersection points when the ratio A is 2. Intersection points C0 and C3 are the change in intersection points when the ratio A is 2.5. Intersection points C0 and C4 are the change in intersection points when the ratio A is 3. Intersection points C0 and C5 are the change in intersection points when the ratio A is 3.6.
- The intersection point C0 is the intersection point when the internal pressure of the nozzle is the maximum pressure Pmax. The intersection points C1, C2, C3, C4 and C5 are the intersection points when the internal pressure of the nozzle is the minimum pressure Pmin.
- When the ratio A is 1.3, the intersection point C1 deviates upward from the
back wall surface 141. - When the ratio A is 2, the intersection point C2 is near the
upper edge 143 of theback wall surface 141. - When the ratio A is 2.5, the intersection points C0 and C3 are within the
back wall surface 141. - When the ratio A is 3, the intersection points C0 and C4 are within the
back wall surface 141. - When the ratio A is 3.6, the intersection points C0 and C5 are within the
back wall surface 141. - In the situation where the intersection point Cn deviates upward from the
back wall surface 141, an adverse effect on the flying position of the weft Y becomes prominent, and decrease in the flying speed of the weft and failure of weft insertion are likely to occur. The intersection point C2 is near theupper edge 143 of theback wall surface 141 when the ratio A is 2 while the intersection point C3 is within theback wall surface 141 when the ratio A is 2.5. That is, when the ratio A is 2.5, deviation of the intersection point Cn upward from theback wall surface 141 is inhibited with high reliability. - When the ratio A is 3, the intersection points C0 and C4 are both positioned within the
back wall surface 141. Thus, when the ratio A is 3.0, deviation of the intersection point Cn upward from theback wall surface 141 is inhibited with higher reliability. - When the ratio A is 3, the intersection point C4 is positioned inside the
upper edge 143 of theback wall surface 141. When the ratio A is 3.6, the intersection point C5 is positioned further inside (or lower than) the intersection point C4. That is, when the ratio A is 3.6, deviation of the intersection point Cn upward from theback wall surface 141 is inhibited with even higher reliability. - The above embodiment has the following advantages.
- (1) As illustrated in
Fig. 7 , A0 is the value of γ/β when the variation range Δδmax of thejet deflection angle 6 becomes 0 when the internal pressure of the nozzle is changed from the maximum pressure Pmax to the minimum pressure Pmin at the time of air injection at theauxiliary nozzle 21. The value of A0 is greater than 2 but smaller than 2.5. When the ratio A is greater than the value of A0, the variation range Δδmax of the jet deflection angle δ is positive. On the condition that the variation range Δδmax is positive, the line of the direction of air injection C approaches toward the modifiedreed 12 even when the internal pressure of the nozzle changes from the maximum pressure Pmax to the minimum pressure Pmin at the end of air injection, and an effect due to increase in the variation Δε of the jet elevation angle ε as illustrated inFig. 4 is offset. Thus, the possibility of the line of the direction of air injection C to deviate upward from theweft guiding passage 14 is reduced.
Thus, theauxiliary nozzle 21 for weft insertion that satisfies an inequality expression of the ratio A:injection hole 23 to deviate from theweft guiding passage 14 due to a decrease in the internal pressure of the nozzle. - (2) The variation range Δδmax of the jet deflection angle δ when the ratio A is 2.5 is greater than that in the case where the ratio A is A0. The internal pressure of the nozzle at the time of completion of air injection at the
auxiliary nozzle 21 is lower than the minimum pressure Pmin for weft insertion which is the pressure at which the line of the direction of air injection C is measurable. When the ratio is A0, it is possible that the variation range Δδmax of the jet deflection angle δ becomes negative when the internal pressure of the nozzle becomes lower than the minimum pressure Pmin. The configuration where A is 2.5 or greater facilitates positioning the line of the direction of air injection C in theweft guiding passage 14 with high reliability. - (3) The variation range Δδmax of the jet deflection angle δ when the ratio A is 3 is greater than that in the case where the ratio A is 2.5. Accordingly, the configuration where the A is 3 or greater facilitates positioning the line of the direction of air injection C in the
weft guiding passage 14 with higher reliability. - (4) Even when the ratio A is greater than 4.5, the positive variation range Δδmax remains almost steady. Generally, the
injection hole 23 is formed by electro spark machining. When the processing deflection angle β is constant, the smaller the ratio A is, the smaller the taper angle γ is. Theinjection hole 23 is easier to process as the taper angle γ is smaller. Thus, the configuration where A is 4.5 or greater is advantageous to facilitate the processing of theinjection hole 23. - The present invention may be embodied in the following embodiment.
- The injection hole may be a hole in the form of a truncated elliptic cone.
- A weft insertion apparatus in a jet loom, wherein the weft insertion apparatus includes an auxiliary nozzle (21) for weft insertion having an injection hole (23) from which air jet is ejected to deliver a weft (Y) in a weft guiding passage (14), is provided. The injection hole (23) is tapered so that the cross-sectional area of the hole (23) is decreased toward the direction of air injection of the auxiliary nozzle (21). The ratio A of a tapered angle γ of the injection hole (23) to a processing deflection angle β of the injection hole (23), γ/β = A, has the relationship expressed by an inequality (1):
Claims (5)
- A weft insertion apparatus in a jet loom, wherein the weft insertion apparatus includes an auxiliary nozzle (21) for weft insertion having an injection hole (23) from which an air jet is ejected to deliver a weft (Y) in a weft guiding passage (14),
wherein the injection hole (23) is tapered so that the cross-sectional area of the hole (23) is decreased toward the direction of air injection of the auxiliary nozzle (21), and
wherein the ratio A of a tapered angle γ of the injection hole (23) to a processing deflection angle β of the injection hole (23), γ/β = A, has the relationship expressed by an inequality (1):
wherein A0 is the value of γ/β when the variation range (Δδmax) of the jet deflection angle (δ) becomes 0 when the injection pressure of the auxiliary nozzle (21) is changed from the maximum pressure (Pmax) for weft insertion to the minimum pressure (Pmin) for weft insertion. - The weft insertion apparatus according to claim 1 wherein the ratio A is 2.5 or greater.
- The weft insertion apparatus according to claim 1 wherein the ratio A is 3 or greater.
- The weft insertion apparatus according to any one of claims 1 to 3 wherein the ratio A is 4.5 or greater.
- The weft insertion apparatus according to any one of claims 1 to 4 wherein the injection hole is in the form of a truncated cone.
Applications Claiming Priority (1)
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JP2010208424A JP5553443B2 (en) | 2010-09-16 | 2010-09-16 | Weft insertion device in jet loom |
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EP2431507A1 true EP2431507A1 (en) | 2012-03-21 |
EP2431507B1 EP2431507B1 (en) | 2012-10-03 |
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EP20110178050 Active EP2431507B1 (en) | 2010-09-16 | 2011-08-19 | Weft insertion apparatus in jet loom |
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EP (1) | EP2431507B1 (en) |
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CN103696100A (en) * | 2013-12-05 | 2014-04-02 | 建滔(清远)玻璃纤维有限公司 | Pressure reducing throttle mechanism for air jet loom |
CN104711748A (en) * | 2013-12-13 | 2015-06-17 | 江南大学 | Technological parameter adjustment method of energy-saving auxiliary jet nozzle of air jet loom |
JP7364356B2 (en) * | 2019-05-13 | 2023-10-18 | 津田駒工業株式会社 | Sub-nozzle for air-jet looms |
Citations (5)
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BE835773A (en) * | 1975-11-20 | 1976-03-16 | HOLLOW NEEDLE-SHAPED NOZZLE WITH A NOZZLE INSERTED NEAR THE TIP IN THE SIDEWALL OF THE TIP | |
DE3639867C1 (en) * | 1986-11-21 | 1987-10-29 | Picanol Nv | Jet-weaving machine |
DE3720492C1 (en) * | 1987-06-20 | 1988-08-04 | Dornier Gmbh Lindauer | Air nozzle for weft-thread insertion in pneumatic weaving machines |
JPH0397939A (en) | 1989-09-08 | 1991-04-23 | Toyota Central Res & Dev Lab Inc | Sub-nozzle of air-jet loom |
JPH09176937A (en) | 1995-12-27 | 1997-07-08 | Toyota Central Res & Dev Lab Inc | Jet direction measurement and instrument therefor in air jet loom |
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CS235259B1 (en) * | 1981-04-30 | 1985-05-15 | Vladimir Kuda | Picking channel of jet loom |
CN86208860U (en) * | 1986-11-08 | 1987-12-05 | 咸阳纺织机械厂 | Auxiliary spray nozzle of a jet loom for drawing weft yarn |
DE3823362A1 (en) * | 1988-07-09 | 1990-01-11 | Picanol Nv | Jet-weaving machine |
CN1030509C (en) * | 1992-08-04 | 1995-12-13 | 株式会社丰田自动织机制作所 | Auxiliary nozzle used in jet loom |
TW219380B (en) * | 1992-11-06 | 1994-01-21 | Nippon Tungsten | Auxiliary nozzle used in air ejection weaving machine |
DE29720595U1 (en) * | 1997-11-20 | 1998-02-05 | Dornier Gmbh Lindauer | Auxiliary blowing nozzle, in particular for an air jet loom |
CN101424000A (en) * | 2007-12-17 | 2009-05-06 | 西安工程大学 | Integral pipeline segment and topdressing auxiliary nozzle |
CN101775692A (en) * | 2010-02-08 | 2010-07-14 | 金坛市天盛机械制造有限公司 | Pipeline plate subassembly for assisting nozzle |
-
2010
- 2010-09-16 JP JP2010208424A patent/JP5553443B2/en active Active
-
2011
- 2011-08-19 EP EP20110178050 patent/EP2431507B1/en active Active
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Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
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BE835773A (en) * | 1975-11-20 | 1976-03-16 | HOLLOW NEEDLE-SHAPED NOZZLE WITH A NOZZLE INSERTED NEAR THE TIP IN THE SIDEWALL OF THE TIP | |
DE3639867C1 (en) * | 1986-11-21 | 1987-10-29 | Picanol Nv | Jet-weaving machine |
DE3720492C1 (en) * | 1987-06-20 | 1988-08-04 | Dornier Gmbh Lindauer | Air nozzle for weft-thread insertion in pneumatic weaving machines |
JPH0397939A (en) | 1989-09-08 | 1991-04-23 | Toyota Central Res & Dev Lab Inc | Sub-nozzle of air-jet loom |
JPH09176937A (en) | 1995-12-27 | 1997-07-08 | Toyota Central Res & Dev Lab Inc | Jet direction measurement and instrument therefor in air jet loom |
Also Published As
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JP5553443B2 (en) | 2014-07-16 |
CN102409469B (en) | 2014-03-19 |
CN102409469A (en) | 2012-04-11 |
EP2431507B1 (en) | 2012-10-03 |
JP2012062604A (en) | 2012-03-29 |
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