JP2724587B2 - Osa feather for air jet loom and method of manufacturing the same - Google Patents
Osa feather for air jet loom and method of manufacturing the sameInfo
- Publication number
- JP2724587B2 JP2724587B2 JP63089447A JP8944788A JP2724587B2 JP 2724587 B2 JP2724587 B2 JP 2724587B2 JP 63089447 A JP63089447 A JP 63089447A JP 8944788 A JP8944788 A JP 8944788A JP 2724587 B2 JP2724587 B2 JP 2724587B2
- Authority
- JP
- Japan
- Prior art keywords
- recess
- air
- axis
- feather
- osa
- 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.)
- Expired - Lifetime
Links
- 210000003746 feather Anatomy 0.000 title claims description 20
- 238000004519 manufacturing process Methods 0.000 title claims description 10
- 239000004744 fabric Substances 0.000 claims description 8
- 238000000034 method Methods 0.000 claims description 7
- 238000005520 cutting process Methods 0.000 claims description 4
- 238000012545 processing Methods 0.000 claims description 3
- 238000004080 punching Methods 0.000 description 6
- 230000002093 peripheral effect Effects 0.000 description 5
- 238000009792 diffusion process Methods 0.000 description 3
- 238000007796 conventional method Methods 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 238000003780 insertion Methods 0.000 description 1
- 230000037431 insertion Effects 0.000 description 1
- 230000009191 jumping Effects 0.000 description 1
- 238000005498 polishing Methods 0.000 description 1
- 238000007493 shaping process Methods 0.000 description 1
- 238000005728 strengthening Methods 0.000 description 1
- 230000007704 transition Effects 0.000 description 1
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
- D03D47/27—Drive or guide mechanisms for weft inserting
- D03D47/277—Guide mechanisms
- D03D47/278—Guide mechanisms for pneumatic looms
Landscapes
- Engineering & Computer Science (AREA)
- Textile Engineering (AREA)
- Looms (AREA)
Description
【発明の詳細な説明】 《産業上の利用分野》 この発明は、エアジェットルーム用のオサ羽とその製
造方法に関するものである。DETAILED DESCRIPTION OF THE INVENTION << Industrial Application Field >> The present invention relates to a feather wing for an air jet loom and a method of manufacturing the same.
《従来の技術》 エアジェットルームのオサ羽1には、織前側に凹所3
が設けられており、メインノズルの空気噴流によって送
り出された緯糸4は、並置されたオサ羽の上記凹所によ
って形成される溝状の空気ガイド5を通って飛走する。
この空気ガイドは、空気噴流の拡散を防止して緯糸を安
定に飛走させるために設けられているものであるから、
空気ガイドの壁面を形成する凹所の周縁6a、7a、8aの端
面は、空気噴流を絞る方向に傾斜した傾斜面とするのが
良いと考えられ、従来のこの種のオサ羽では、第10、11
図に示すように、凹所3の周囲の上顎縁6の端面6a、底
縁7の端面7a及び下顎縁8の端面8aの全てを空気噴流を
絞る方向に傾斜させた傾斜面としている。<Conventional technology> The wing 1 of the air jet loom has a recess 3 on the cloth fell side.
The weft yarn 4 sent out by the air jet of the main nozzle flies through a groove-shaped air guide 5 formed by the above-mentioned recesses of the juxtaposed feather wings.
Since this air guide is provided to prevent the diffusion of the air jet and stably fly the weft,
It is considered that the end surfaces of the peripheral edges 6a, 7a, 8a of the recesses forming the wall surface of the air guide are preferably inclined surfaces inclined in the direction in which the air jet is narrowed. , 11
As shown in the figure, the end face 6a of the upper jaw edge 6, the end face 7a of the bottom edge 7, and the end face 8a of the lower jaw edge 8 around the recess 3 are all inclined surfaces inclined in the direction of reducing the air jet.
しかしこのような空気ガイド5を設けても空気噴流の
流速低下による緯糸搬送力の低下は避けることができな
いから、これを補助するために織前側から僅かに斜め上
方に向けて空気ガイド内へと空気を噴射するサブノズル
14(第8、9図)が設けられるのが普通である。However, even if such an air guide 5 is provided, a decrease in the weft conveying force due to a decrease in the flow rate of the air jet cannot be avoided. Therefore, in order to assist this, the weft is moved slightly obliquely upward from the cloth fell into the air guide. Sub nozzle that injects air
Usually 14 (FIGS. 8 and 9) are provided.
また従来のオサ羽は、プレス打ち抜きにより所定形状
に切断したあとオサに組上げて空気ガイドの壁面を整形
するという製造方法か採られており、空気ガイドを形成
するオサ羽の凹所3の周縁の端面6a、7a、8aを所定の傾
斜面にするには、プレス打ち抜き後に面打ちにより凹所
周縁の端面を整形するか、あるいはプレス打ち抜き時の
切断条件で傾斜をだす方法が採用されている。In addition, the conventional wings are manufactured by cutting into a predetermined shape by press punching and then assembling the wings to shape the wall surface of the air guide, and the periphery of the recess 3 of the wings forming the air guide is adopted. In order to form the end surfaces 6a, 7a, 8a into predetermined inclined surfaces, a method of shaping the end surface of the peripheral edge of the recess by punching after press punching, or forming a slope under cutting conditions at the time of press punching is adopted.
《発明が解決しようとする課題》 ところが従来のオサでは、メインノズルやサブノズル
の噴流を強くして緯糸搬送力を増大させると、緯糸の飛
走に乱れが生じ、飛走中の緯糸が空気ガイド外へと飛散
し易くなる問題があった。この発明は、この問題を解決
することを課題として為されたもので、緯糸をより安定
に飛走させることができるエアジェットルーム用のオサ
羽を得ることを課題としている。《Problems to be solved by the invention》 However, in the conventional Osa, when the weft conveying force is increased by strengthening the jet of the main nozzle and the sub-nozzle, the flight of the weft is disturbed, and the weft during the flight is air guide There was a problem that it was easy to fly outside. The present invention has been made to solve this problem, and an object of the present invention is to provide a wing for an air jet loom that can stably fly a weft.
《課題を解決するための手段》 そこでこの発明では、オサ羽1に設けた凹所3の上顎
縁6の端面6aを空気流を絞る方向の面とし、底縁7の端
面7aを空気流を拡散する方向の面とすることにより上記
問題を解決している。<< Means for Solving the Problems >> Accordingly, in the present invention, the end face 6a of the upper jaw edge 6 of the recess 3 provided in the oscillating wing 1 is a surface in the direction of restricting the air flow, and the end face 7a of the bottom edge 7 is used for the air flow. The above problem is solved by making the surface in the direction of diffusion.
そしてこの発明のオサ羽の製造方法は、上記オサ羽の
凹所の端面6a、7aを研削加工により整形するものとし、
該研削加工は、プレス打ち抜き等により所定形状に切断
した薄板を研削砥石車11の軸線に垂直な第1の軸12回り
に傾斜させ、必要により更に該軸線に平行な第2の軸13
回りとに同時に傾斜させて凹所3の端面7a、8aを研削す
るというものである。And the manufacturing method of the Osa feather of the present invention shall shape the end surfaces 6a and 7a of the recess of the Osa feather by grinding.
In the grinding process, a thin plate cut into a predetermined shape by press punching or the like is inclined around a first axis 12 perpendicular to the axis of the grinding wheel 11, and a second axis 13 parallel to the axis is further provided if necessary.
This is to grind the end faces 7a and 8a of the recess 3 while simultaneously inclining the periphery.
《作用》 従来のオサ羽で形成された空気ガイドは、各オサ羽の
凹所周縁の端面6a、7a、8aが全て空気噴流を絞る方向に
傾斜していたため、この傾斜に沿って空気ガイドの中心
線方向に偏向した3方向からの空気流が互いにぶつかり
合って乱れが生じ、しかも底縁7の傾斜面7aによって偏
向した空気流は空気ガイド5の開口側に向かうので、飛
走中の緯糸4を空気ガイド5から飛び出させるように作
用していた。特にサブノズルからの噴流は、第8図に示
すように、空気ガイドの上顎縁6の傾斜面に沿って下方
に偏向しながら底縁7に向かって回り込んで行き、次い
で底縁7の傾斜面7aによって織前側に偏向した空気流が
緯糸4を飛び出させる方向に強く作用していた。<Operation> In the air guide formed by the conventional wings, the end surfaces 6a, 7a, 8a of the peripheral edges of the recesses of the wings are all inclined in the direction of narrowing the air jet. The air flows from three directions deflected toward the center line collide with each other to cause turbulence, and the air flow deflected by the inclined surface 7a of the bottom edge 7 goes to the opening side of the air guide 5, so that the weft during flight 4 acted so as to protrude from the air guide 5. In particular, the jet from the sub-nozzle goes round toward the bottom edge 7 while deflecting downward along the inclined surface of the upper jaw edge 6 of the air guide as shown in FIG. The air flow deflected to the cloth fell side by 7a strongly acted in the direction in which the weft yarn 4 was ejected.
これに対してこの発明のオサ羽で形成された空気ガイ
ドは、各オサ羽の底縁7の端面7aが空気をオサ羽の間の
スリット9からオサの背面側へと逃がすように作用する
ので、空気ガイド5を通過する空気流中に織前側に向け
て偏向した強い空気流を生成させることがなく、空気ガ
イド5内での空気流の衝突を緩和させて空気の乱れを軽
減し、緯糸4を空気ガイド5から飛び出させることなく
安定に飛走させることができる。On the other hand, in the air guide formed by the wings of the present invention, the end face 7a of the bottom edge 7 of each wing serves to release air from the slit 9 between the wings to the back side of the wing. A strong air flow deflected toward the cloth fell is not generated in the air flow passing through the air guide 5, the collision of the air flow in the air guide 5 is reduced, and the turbulence of the air is reduced. 4 can stably fly without jumping out of the air guide 5.
また従来のオサ羽の製造方法では、凹所周縁の端面6
a、7a、8aを正確にばらつきなく整形することは困難で
あったが、上記製造方法によれば、オサ羽の凹所の周縁
の端面を設計した通りの正確な面に加工することがで
き、凹所端面の形状の誤差やばらつきに起因する空気の
乱れの発生を防止することができ、凹所の上顎から底へ
と移行する部分において端面を絞り方向の面から拡散方
向の面へと滑らかに移行させるという理想的な形状を得
ることができ、空気ガイド内の空気の乱れをより生じさ
せることのないオサ羽を得ることができる。更に請求項
3記載の製造方法によれば、多数のオサ羽の上顎縁の端
面と底縁の端面とを同時に一工程で加工することができ
る。In addition, in the conventional method of manufacturing a feather wing, the end face 6
Although it was difficult to accurately shape a, 7a, and 8a without variation, according to the above-described manufacturing method, it is possible to process the end surface of the peripheral edge of the recess of the Osa feather into an accurate surface as designed. It is possible to prevent the occurrence of air turbulence due to errors and variations in the shape of the end face of the recess, and to change the end face from the face in the drawing direction to the face in the diffusion direction at the part transitioning from the upper jaw to the bottom of the recess. It is possible to obtain an ideal shape of smooth transition, and it is possible to obtain a wing that does not cause more turbulence in the air in the air guide. Further, according to the manufacturing method of the third aspect, it is possible to simultaneously process the end faces of the upper jaw edge and the end face of the bottom edge of a large number of feather wings in one step.
《実施例》 第1図ないし第4図はこの発明のオサ羽を備えたオサ
の一実施例を示す図で、第1図はオサ羽の側面図、第2
図はオサの一部正面図、第3図は第1図のA部拡大断面
図、第4図はB部拡大断面図である。<< Embodiment >> FIGS. 1 to 4 are views showing an embodiment of a batting provided with a batting wing of the present invention. FIG. 1 is a side view of the batting, and FIG.
The figure is a partial front view of the Osa, FIG. 3 is an enlarged sectional view of a portion A in FIG. 1, and FIG. 4 is an enlarged sectional view of a B portion.
オサ羽1は、その織前側2に凹所3を有しており、並
置されたオサ羽1・・・の凹所3・・・で緯糸4を導く
空気ガイド5が形成される。凹所3は略コ字形で、上顎
縁6の端面6a、底縁7の端面7a及び下顎縁8の端面8a
は、第3、4図に示すように、空気流Xの通過方向に対
して傾斜した面となっている。その面の傾斜方向は、上
顎縁6の端面6aと下顎面8の端面8aとは空気流Xの下流
側が空気ガイドの中心線側へと高くなる方向(正テー
パ)であり、底縁7の端面7aは空気流Xの下流側が空気
ガイド5の中心線から離れて低くなる方向(逆テーパ)
である。これらの端面6a、7a、8aの傾斜角α、β、γ
は、例えば3度ないし5度であるが、この角度は、オサ
羽の間のスリット9の間隔によっても変化し、スリット
9の間隙が大きい場合には底縁の端面7aを逆テーパにし
なくても該部分において空気流を拡散させる方向に導く
ことは可能である。一方、上顎縁の端面6aは、サブノズ
ル14からの空気流X(第9図参照)を空気ガイド5に沿
う方向に導くために、スリット9の間隙が大きくなれば
なる程正テーパの傾斜の度合を大きくする必要があり、
常に正テーパとなる。また下顎縁の端面8aは、飛走する
緯糸4の重力による下方偏倚を防止するために、一般的
には正テーパとするのが好ましい。The ossa feather 1 has a recess 3 on the cloth fell side 2 thereof, and an air guide 5 for guiding the weft 4 is formed by the recesses 3... Of the ossa feathers 1. The recess 3 is substantially U-shaped, and has an end face 6a of the upper jaw edge 6, an end face 7a of the bottom edge 7, and an end face 8a of the lower jaw edge 8.
Is a surface that is inclined with respect to the direction in which the airflow X passes, as shown in FIGS. The inclination direction of the surface is such that the end surface 6a of the upper jaw edge 6 and the end surface 8a of the lower jaw surface 8 are in a direction (positive taper) in which the downstream side of the airflow X becomes higher toward the center line side of the air guide. The end face 7a has a direction in which the downstream side of the airflow X becomes lower away from the center line of the air guide 5 (reverse taper).
It is. The inclination angles α, β, γ of these end faces 6a, 7a, 8a
Is, for example, 3 degrees to 5 degrees, but this angle also changes depending on the interval between the slits 9 between the wings. When the gap between the slits 9 is large, the end surface 7a of the bottom edge does not need to have an inverse taper. It is also possible to direct the air flow in the direction in which it diffuses. On the other hand, in order to guide the air flow X (see FIG. 9) from the sub-nozzle 14 in a direction along the air guide 5, the end face 6a of the upper jaw edge has a degree of inclination of a positive taper as the gap of the slit 9 becomes larger. Need to be larger,
It always has a positive taper. Generally, the end face 8a of the lower jaw edge is preferably tapered in order to prevent the flying weft 4 from being deflected downward due to gravity.
第5図ないし第7図はこの発明のオサ羽の製造方法の
一実施例を示す図で、プレス打ち抜き加工により所定形
状に切断したオサ羽1・・・の多数枚を積重した状態で
固定し、砥石車11で凹所3の端縁6a、7aを研削している
状態を示している。オサ羽1・・・は、砥石車11の軸線
Yに直交する第1の軸12回りに上顎縁の端面の傾斜角α
に相当する角度だけ砥石車側から見て左回りに傾斜さ
せ、同時に砥石車の軸線Yと平行な第2の軸13回りに底
縁の端面の傾斜角βに相当する角度だけオサ羽の下方か
ら見て左回りに傾斜させて固定されている。この固定
は、治具等を用いてオサ羽をクランプすることにより行
ってやれば良い。5 to 7 are views showing one embodiment of the method of manufacturing the wings of the present invention, in which a large number of wings 1... Cut into a predetermined shape by press punching are stacked and fixed. Then, a state in which the edges 6a and 7a of the recess 3 are ground by the grinding wheel 11 is shown. The oscillating wings 1... Are inclined at an angle α of the end face of the upper jaw edge around a first axis 12 orthogonal to the axis Y of the grinding wheel 11.
Tilted counterclockwise when viewed from the grinding wheel side by an angle corresponding to the above, and at the same time, about a second axis 13 parallel to the axis Y of the grinding wheel, below the Osa feather by an angle corresponding to the tilt angle β of the end face of the bottom edge. It is fixed by inclining counterclockwise when viewed from above. This fixing may be performed by clamping the wings using a jig or the like.
多数のオサ羽1・・・をこのような状態で積層状態で
固定して砥石車11で凹所3の上顎縁の端面6aと底縁の端
面7aとを研削し、更に第6図に想像線で示すようにオサ
羽1・・・を第2の軸13回りの傾斜方向はそのままにし
て第1の軸12回りに反対方向に傾斜させて砥石車11で凹
所の底縁の端面7aと下顎縁の端面8aとを研削し、その後
バレル研磨加工により稜線に丸みを持たせると共に面を
滑らかに加工してやれば、第3、4図に示した端面形状
を備えた凹所3をオサ羽1に形成することができる。A large number of wings 1... Are fixed in a stacked state in this state, and the end surface 6a of the upper jaw edge and the end surface 7a of the bottom edge of the recess 3 are ground by a grinding wheel 11, and further imagined in FIG. .. Are tilted in the opposite direction around the first axis 12 while keeping the inclination direction around the second axis 13 as indicated by the line, and the end face 7a of the bottom edge of the recess is And the end face 8a of the lower jaw edge are ground, and then the ridge is rounded by barrel polishing and the face is smoothly processed, so that the recess 3 having the end face shape shown in FIGS. 1 can be formed.
《発明の効果》 この発明のオサ羽により組上げたオサは、空気ガイド
の上顎面が空気噴流を絞る方向に空気を導き、底面が空
気噴流を一部オサの背面側へ拡散させて織前側に向かう
空気流の発生を抑えるように作用するので、空気ガイド
内の空気の乱れが抑制されて緯糸が滑らかに飛走し、ま
た織前側の開口から緯糸が空気ガイドの外へと飛散する
ことも無くなる。<< Effect of the Invention >> In the Osa assembled by the Osa feathers of the present invention, the upper jaw surface of the air guide guides air in the direction of narrowing the air jet, and the bottom surface partially diffuses the air jet to the back side of the Osa and moves toward the cloth front. It acts to suppress the generation of the heading air flow, so that the turbulence of the air in the air guide is suppressed and the weft flies smoothly, and the weft also scatters outside the air guide from the opening on the weave front. Disappears.
またこの発明の製造方法によれば、空気ガイドを形成
するオサ羽の凹所周縁の端面が正確な形状及び傾斜角で
整形され、加工誤差やばらつきの発生が回避されるの
で、空気ガイドを通過する空気流の方向を正確にコント
ロールすることができ、設計段階で意図した通りの空気
流を空気ガイド内に生成させることが可能になり、より
安定した緯入れができるオサを提供することができる。Further, according to the manufacturing method of the present invention, the end surface of the peripheral edge of the recess of the wing that forms the air guide is shaped with an accurate shape and an inclined angle, and the occurrence of processing errors and variations is avoided. It is possible to accurately control the direction of the air flow that occurs, it is possible to generate the intended air flow in the air guide at the design stage, and it is possible to provide an Osa that can perform more stable weft insertion .
第1図ないし第4図はこの発明のオサ羽を備えたオサの
一実施例を示す図で、第1図はオサ羽の側面図、第2図
はオサの一部正面図、第3図は第1図のA部拡大断面
図、第4図はB部拡大断面図である。第5図ないし第7
図はこの発明方法によりオサ羽の凹所を研削加工してい
る状態を示した図で、第5図は側面図、第6図は正面
図、第7図は第6図の下方より見た図である。第8図及
び第9図はサブノズルからの空気噴流と空気ガイドとの
関係を示した説明図である。第10図及び第11図は従来の
オサ羽の凹所の端面形状を示した図で、第10図は第3図
に、第11図は第4図にそれぞれ相当する図である。 図中、 1:オサ羽、3:凹所 5:空気ガイド、6:上顎縁 6a:上顎縁の端面、7:底縁 7a:底縁の端面、11:研削砥石車 12:第1の軸、13:第2の軸1 to 4 are views showing an embodiment of an Osa equipped with an Osa feather according to the present invention. FIG. 1 is a side view of the Osa feather, FIG. 2 is a partial front view of the Osa feather, FIG. FIG. 4 is an enlarged sectional view of a portion A in FIG. 1, and FIG. 4 is an enlarged sectional view of a portion B in FIG. Figures 5 to 7
FIG. 5 is a view showing a state in which the recess of the wing is ground by the method of the present invention. FIG. 5 is a side view, FIG. 6 is a front view, and FIG. FIG. 8 and 9 are explanatory diagrams showing the relationship between the air jet from the sub nozzle and the air guide. 10 and 11 are views showing the end face shapes of the recesses of the conventional Osa feather. FIG. 10 is a view corresponding to FIG. 3, and FIG. 11 is a view corresponding to FIG. In the figure, 1: Osa feather, 3: recess 5: air guide, 6: maxillary edge 6a: end face of maxillary edge, 7: bottom edge 7a: end face of bottom edge, 11: grinding wheel 12: first shaft , 13: second axis
Claims (3)
(5)を形成する凹所(3)をオサ羽(1)の織前側に
設けたエアジェットルーム用オサ羽において、前記凹所
(3)は、上顎縁(6)の端面(6a)が空気流を絞る方
向の面とされ、底縁(7)の端面(7a)が空気流を拡散
する方向の面とされていることを特徴とする、エアジェ
ットルーム用オサ羽。An air jet loom wing, wherein a recess (3) forming an air guide (5) for guiding a weft-inserted air flow is provided on the cloth fell side of the wing (1). 3) indicates that the end surface (6a) of the upper jaw edge (6) is a surface in the direction to restrict the air flow, and the end surface (7a) of the bottom edge (7) is a surface in the direction to diffuse the air flow. Characterized as Osa feather for air jet loom.
切断し、当該凹所周縁の端面(6a)、(7a)、(8a)を
研削加工により加工する工程を含み、該研削加工は、研
削しようとする薄板を研削砥石車(11)の軸線に垂直な
軸(12)回りに傾斜させて研削することを特徴とする、
請求項第1項記載のオサ羽の製造方法。2. A step of cutting a thin plate into a shape having a recess (3) on the front side of a weave, and processing end surfaces (6a), (7a) and (8a) of the periphery of the recess by grinding. Grinding is characterized in that the thin plate to be ground is ground by tilting it around an axis (12) perpendicular to the axis of the grinding wheel (11).
A method for manufacturing a wing feather according to claim 1.
切断し、当該凹所周縁の端面(6a)、(7a)、(8a)を
研削加工により加工する工程を含み、該研削加工は、研
削しようとする薄板を研削砥石車(11)の軸線に垂直な
第1の軸(12)回りと該軸線に平行な第2の軸(13)回
りとに同時に傾斜させて研削することを特徴とする、請
求項第1項記載のオサ羽の製造方法。3. A step of cutting a thin plate into a shape having a recess (3) on the cloth fell side, and processing end surfaces (6a), (7a) and (8a) of the periphery of the recess by grinding. The grinding is performed by simultaneously inclining a thin plate to be ground around a first axis (12) perpendicular to the axis of the grinding wheel (11) and around a second axis (13) parallel to the axis. 2. The method for manufacturing a wing feather according to claim 1, wherein:
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP63089447A JP2724587B2 (en) | 1988-04-12 | 1988-04-12 | Osa feather for air jet loom and method of manufacturing the same |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP63089447A JP2724587B2 (en) | 1988-04-12 | 1988-04-12 | Osa feather for air jet loom and method of manufacturing the same |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPH01266243A JPH01266243A (en) | 1989-10-24 |
| JP2724587B2 true JP2724587B2 (en) | 1998-03-09 |
Family
ID=13970936
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP63089447A Expired - Lifetime JP2724587B2 (en) | 1988-04-12 | 1988-04-12 | Osa feather for air jet loom and method of manufacturing the same |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JP2724587B2 (en) |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP3057886B2 (en) * | 1991-04-01 | 2000-07-04 | 株式会社豊田自動織機製作所 | Reed for weft insertion device in jet loom and method of manufacturing the reed |
| CN106400284B (en) * | 2015-07-30 | 2018-01-23 | 天津市纺织机械器材研究所 | A kind of steel foil for air-jet loom airslide air pressure value adjuster |
Family Cites Families (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS5729639A (en) * | 1980-07-28 | 1982-02-17 | Toyoda Chuo Kenkyusho Kk | Weft inserting apparatus in jet loom |
| JPS60194152A (en) * | 1984-03-09 | 1985-10-02 | 株式会社木地金筬製作所 | Metal shuttle polishing method and apparatus of air jet typeloom |
| JPH0318534Y2 (en) * | 1984-12-26 | 1991-04-18 | ||
| JPH0345969Y2 (en) * | 1986-11-19 | 1991-09-27 |
-
1988
- 1988-04-12 JP JP63089447A patent/JP2724587B2/en not_active Expired - Lifetime
Also Published As
| Publication number | Publication date |
|---|---|
| JPH01266243A (en) | 1989-10-24 |
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