JPH01314753A - Weft-inserting unit in jet loom - Google Patents

Weft-inserting unit in jet loom

Info

Publication number
JPH01314753A
JPH01314753A JP63144148A JP14414888A JPH01314753A JP H01314753 A JPH01314753 A JP H01314753A JP 63144148 A JP63144148 A JP 63144148A JP 14414888 A JP14414888 A JP 14414888A JP H01314753 A JPH01314753 A JP H01314753A
Authority
JP
Japan
Prior art keywords
wall surface
weft
weft insertion
upper wall
inclination
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
JP63144148A
Other languages
Japanese (ja)
Other versions
JP2623701B2 (en
Inventor
Masao Shiraki
雅雄 白木
Shinichiro Matsuyama
松山 新一郎
Kunihiro Ishikawa
石川 国広
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Toyota Industries Corp
Original Assignee
Toyoda Automatic Loom Works Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Toyoda Automatic Loom Works Ltd filed Critical Toyoda Automatic Loom Works Ltd
Priority to JP63144148A priority Critical patent/JP2623701B2/en
Publication of JPH01314753A publication Critical patent/JPH01314753A/en
Application granted granted Critical
Publication of JP2623701B2 publication Critical patent/JP2623701B2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • DTEXTILES; PAPER
    • D03WEAVING
    • D03DWOVEN FABRICS; METHODS OF WEAVING; LOOMS
    • D03D47/00Looms in which bulk supply of weft does not pass through shed, e.g. shuttleless looms, gripper shuttle looms, dummy shuttle looms
    • D03D47/27Drive or guide mechanisms for weft inserting
    • D03D47/277Guide mechanisms
    • D03D47/278Guide mechanisms for pneumatic looms

Landscapes

  • Engineering & Computer Science (AREA)
  • Textile Engineering (AREA)
  • Looms (AREA)

Abstract

PURPOSE:To provide the title unit so designed that an auxiliary nozzle injection tip is located at a position of the lowermost height of the weft-inserting channel, and the both upper and lower walls and deep wall of guide holes are tilted against the weft-inserting direction to control fluid leakage to suppress weft running troubles, thereby enhancing the running speed. CONSTITUTION:In a jet loom, an injection tip 2a of a weft-inserting auxiliary nozzle 2 is located at a position of the lowermost height of the weft-inserting channel S formed with a row of guide holes 4 of deformed guide bars 3. Each of said guide holes 4, being approximately tetragonal, is formed by a nearly horizontal upper wall surface 4a, a nearly perpendicular deep wall surface 4b and a lower wall surface 4c somewhat tilted against said upper wall surface 4a with the inclination of said upper wall surface 4a greater than that of the deep wall surface 4b for the weft inserting direction P; thereby controlling fluid leakage from the releasing port of the guide holes 4 along with properly arranging the pulling action of weft yarns due to said fluid leakage.

Description

【発明の詳細な説明】 [産業上の利用分野コ 本発明は筬羽の前面にガイド孔を持つ変形筬を用いた緯
入れ装置に関するものである。
DETAILED DESCRIPTION OF THE INVENTION [Field of Industrial Application] The present invention relates to a weft insertion device using a modified reed having guide holes in the front surface of the reed.

[従来の技術] 変形筬の前記ガイド孔の列により形成される緯入れ通路
を飛走する緯糸の速度を一ヒげる一方法として、例えば
特公昭59−26688号公報及び特公昭60−148
65号公報に開示されるようにガイド孔の形成壁面を緯
入れ方向に対して傾斜させ、緯入れ通路内を流れるエア
の漏洩を防止して流速を高める方法がある。特公昭59
−26688号公報ではガイド孔を形成する上壁面、下
壁面及び奥壁面を同じ傾斜角に設定してあり、特公昭6
0i4865号公報では上壁面及び下壁面に傾斜を持た
せ、奥壁面は傾斜なしとしている。
[Prior Art] As a method for increasing the speed of the weft yarn flying through the weft insertion path formed by the rows of guide holes of the modified reed, for example, Japanese Patent Publication No. 59-26688 and Japanese Patent Publication No. 60-148 disclose
As disclosed in Japanese Patent No. 65, there is a method in which the wall surface of the guide hole is inclined with respect to the weft insertion direction to prevent leakage of air flowing in the weft insertion passage and increase the flow velocity. Special Public Service 1987
In Publication No. 26688, the upper wall surface, lower wall surface, and back wall surface forming the guide hole are set at the same angle of inclination.
In 0i4865, the upper wall surface and the lower wall surface are sloped, and the back wall surface is not sloped.

両公報のいずれの場合にも、ガイド孔形成壁面の傾斜角
を増大するにつれて流速が増大し、緯糸の飛走速度を高
めることができる。
In both cases, as the inclination angle of the guide hole forming wall surface increases, the flow velocity increases, and the flying speed of the weft yarn can be increased.

[発明が解決しようとする課題] しかしながら、特公昭59−26688号公報の場合に
は傾斜角の増大に伴ってガイド孔の開放口からのエア煽
洩が大きくなり、この漏洩エアに乗って緯糸先端部が緯
入れ通路から外部へ飛び出してしまうという飛走I・ラ
ブルが多発する。特公昭60−14865号公報の場合
には各筬羽の傾斜のない奥壁面間から外部へ漏洩するエ
ア流量が傾斜のある奥壁面間からの漏洩量に比して多く
、このエア漏洩が緯入れ通路内の緯糸先端部を奥壁面側
へ引き付ける作用として働く。そのため、飛走トラブル
の発生割合は極めて少ないが、このエア漏洩により緯入
れ通路内の流速低下が比較的大きく、緯糸飛走速度の高
速化が阻害される。
[Problems to be Solved by the Invention] However, in the case of Japanese Patent Publication No. 59-26688, air leakage from the opening of the guide hole increases as the inclination angle increases, and the weft yarn is carried by this leakage air. There are many cases where the leading edge jumps out from the weft insertion path, resulting in flying problems. In the case of Japanese Patent Publication No. 60-14865, the amount of air leaking to the outside between the non-slanted back wall surfaces of each reed blade is larger than the amount of leakage from between the sloped back wall surfaces, and this air leakage is caused by It works to attract the tip of the weft yarn in the input passage toward the back wall surface. Therefore, although the rate of occurrence of flying troubles is extremely low, this air leakage causes a relatively large decrease in the flow velocity in the weft insertion passage, which impedes an increase in the weft flying speed.

クローズドタイプの緯糸ガイドを特徴とする特公昭47
−23357号公報では、糸抜は部と対向する奥部の壁
面傾斜角が他の形成壁面に比して大きく設定されており
、緯糸先端部を糸抜は部から遠ざける作用が得られるが
、緯糸ガイドとは異なって筬羽が密に近接する変形筬で
は奥壁面の傾斜角を大きく設定すれば奥壁面間からのエ
ア漏洩が減り、飛走トラブルが多発する。
Special Publication of 1977 featuring a closed type weft guide
In Publication No. 23357, the angle of inclination of the wall surface of the inner part facing the thread removal section is set to be larger than the other forming wall surfaces, and the effect of moving the weft tip away from the thread removal section is obtained. Unlike a weft guide, in a modified reed in which the reed blades are closely adjacent to each other, if the inclination angle of the back wall surface is set large, air leakage from between the back wall surfaces will be reduced, and flying problems will occur frequently.

本発明は緯糸の飛走速度の高速化及び飛走トラブルの低
減を共に満たし得る変形筬使用の緯入れ装置を提供する
ことを目的とするものである。
SUMMARY OF THE INVENTION An object of the present invention is to provide a weft inserting device using a modified reed, which can both increase the flying speed of the weft thread and reduce flying troubles.

[課題を解決するだめの手段] そのために本発明では、上壁面、下壁面及び奥壁面から
なるガイド孔の下壁面の開放端近傍に緯入れ相補助ノス
ルの噴射口を設定すると共に、前記上壁面と奥壁面とに
交差する噴射流路を持つように緯入れ用補助ノズルの噴
射方向を設定し、緯入れ方向へ向かうにつれて緯入れ通
路側へ入り込む傾斜を上壁面及び奥壁面に設けると共に
、上壁面の傾斜角を奥壁面の傾斜角よりも大きくした。
[Means for Solving the Problem] To achieve this, in the present invention, the injection port of the weft insertion phase auxiliary nostle is set near the open end of the lower wall surface of the guide hole consisting of the upper wall surface, the lower wall surface, and the inner wall surface, and The injection direction of the weft insertion auxiliary nozzle is set so as to have an injection flow path that intersects the wall surface and the back wall surface, and an inclination is provided on the upper wall surface and the back wall surface that enters the weft insertion path as it goes toward the weft insertion direction, and The angle of inclination of the upper wall was made larger than the angle of inclination of the back wall.

[作用] 緯入れ用補助ノズルからの噴射エアは専ら上壁面及び奥
壁面に当たる。奥壁面に向かったエアの一部は奥壁面か
ら漏洩し、このエア漏洩が飛走緯糸を開放口から奥壁面
側へ引き付ける作用をもたらす。奥壁面からの反射流は
上壁面からの反射流により押さえこまれ、奥壁面からの
反則流か開放口から漏洩することを抑制される。この漏
洩抑Hil1作用と前記引き付は作用との兼ね合いは緯
入れ通路内の流速及び飛走l・ラブルの発生割合を左右
するが、奥壁面の傾斜角を上壁面の傾斜角よりも小さく
することにより漏洩抑制作用と引きイ」す作用との兼ね
合いを最も適正に設定することができ、飛走トラブルの
発生割合を抑制しつつ緯糸飛走速度を高めることができ
る。
[Function] The air jetted from the auxiliary nozzle for weft insertion exclusively hits the upper wall surface and the back wall surface. A part of the air heading toward the back wall surface leaks from the back wall surface, and this air leakage brings about the effect of attracting the flying weft yarn from the open opening toward the back wall surface side. The reflected flow from the back wall surface is suppressed by the reflected flow from the upper wall surface, and the counterflow from the back wall surface or leakage from the open opening is suppressed. The balance between this leakage suppressing Hil1 effect and the above-mentioned attracting effect influences the flow velocity in the weft insertion passage and the occurrence rate of flying l/rubble, but the angle of inclination of the back wall surface is made smaller than the angle of inclination of the upper wall surface. As a result, the balance between the leakage suppressing effect and the pulling effect can be set most appropriately, and the weft flying speed can be increased while suppressing the occurrence rate of flying troubles.

[実施例コ 以下、本発明を具体化した一実施例を図面に基づいて説
明する。
[Example 1] Hereinafter, an example embodying the present invention will be described based on the drawings.

スレイ1の前面には緯入れ用補助ノズル2が緯入れ方向
へ取付位置調整可能に装着されており、緯入れ相補助ノ
スル2の噴射口2aが変形筬3のガイド孔4の列により
形成される緯入れ通路Sの最下位の高さ位置に設定され
ている。変形筬3のガイド孔4は、略水平な上壁面4a
と、略垂立な奥壁面4bと、上壁面4aに対して若干傾
斜する下壁面4cとにより略四角形状に形成されており
、各壁面4a、4b、4cには緯入れ方向に対する傾斜
が設けられている。
An auxiliary weft insertion nozzle 2 is attached to the front of the sleigh 1 so that its mounting position can be adjusted in the weft insertion direction, and the injection port 2a of the weft insertion auxiliary nozzle 2 is formed by the row of guide holes 4 of the deformed reed 3. It is set at the lowest height position of the weft insertion path S. The guide hole 4 of the deformed reed 3 is formed on a substantially horizontal upper wall surface 4a.
It is formed into a substantially rectangular shape by a substantially vertical back wall surface 4b and a lower wall surface 4c slightly inclined with respect to the upper wall surface 4a, and each wall surface 4a, 4b, and 4c is inclined with respect to the weft insertion direction. It is being

第2図に示す奥壁面4bの傾斜角θ2は第3図に示す上
壁面4aの傾斜角θ1の略半分に設定されており、下壁
面4cの傾斜角θ3は」二壁面4aの傾斜角θ1と同じ
に設定されている。そして、第1〜3図に矢印Pで示す
ように、下壁面4cの開放端近傍の噴射口2aの噴射方
向I)は上壁面4aと奥壁面4bとの境界付近を指向す
るように設定されており、外側流線ρで区切られる噴射
流路が上壁面4a及び奥壁面4bと交差する。
The inclination angle θ2 of the rear wall surface 4b shown in FIG. 2 is set to approximately half the inclination angle θ1 of the upper wall surface 4a shown in FIG. is set the same as. As shown by arrow P in FIGS. 1 to 3, the injection direction I) of the injection port 2a near the open end of the lower wall surface 4c is set to point near the boundary between the upper wall surface 4a and the inner wall surface 4b. The jet flow path delimited by the outer streamline ρ intersects the upper wall surface 4a and the inner wall surface 4b.

奥壁面4bの傾斜角θ2が比較的小さいため、第2図に
示すように奥壁面4bへ向かう噴射流の一部(記号Δで
示すンが奥壁面4b間から漏洩する。一方、上壁面4a
の傾斜角θ1は比較的大きく設定されているため、上壁
面4aへ向かう噴射流が上壁面4a間から漏洩する割合
が少なく、上壁面4aへ向かう噴射流の反則割合か大き
い。このような反射割合の大きい上壁面4aがらの反射
流は奥壁面4bからの反射流がガイド孔4の開放口へ向
かう作用を抑制する。従って、緯入れ用メインノズル5
から緯入れ通路Sへ創出された緯糸は奥壁面4b間から
の漏洩作用とガイド孔4の開数日からの漏洩抑制作用と
を受iJつつ緯入れ通路S内を飛走する。
Since the inclination angle θ2 of the back wall surface 4b is relatively small, a part of the jet flow toward the back wall surface 4b (indicated by the symbol Δ) leaks from between the back wall surfaces 4b as shown in FIG.
Since the inclination angle θ1 is set relatively large, the proportion of the jet flow toward the upper wall surface 4a leaking from between the upper wall surfaces 4a is small, and the proportion of the jet flow directed toward the upper wall surface 4a is high. The reflected flow from the upper wall surface 4a having a large reflection ratio suppresses the effect of the reflected flow from the inner wall surface 4b toward the opening of the guide hole 4. Therefore, the main nozzle 5 for weft insertion
The weft created from the weft to the weft insertion passage S flies through the weft insertion passage S while receiving the leakage effect from between the back wall surfaces 4b and the leakage suppressing effect from the opening number of the guide hole 4.

第4図の曲線C1は上壁面4aの傾斜角θ1と奥壁面4
bの傾斜角θ2とを等しくした場合の緯糸飛走速度を示
し、曲線C2は本実施例の場合の飛走速度を示す。傾斜
角θ2を傾斜角θ1に等しくした場合には奥壁面4b間
からの流体漏洩が少なくなり、この流体漏洩に起因する
流速低下が少なくなる。そのため、θ1−02の場合の
傾斜角θ1の増加に伴う緯糸速度増加割合は本実施例の
場合(θ1〉θ2)に比して高く、緯糸飛走速度の高速
化には都合がよい。しかしながら、緯糸飛走速度がある
限界(第4図に■1で示す)、即ち傾斜角θ1がある限
界(第4図にαで示す)を越えると、奥壁面4bからの
反射流がガイド孔4の開放口へ向かう作用を−1−壁面
4aからの反射流により抑制する効果が奥壁面4b間か
らの流体漏洩減少に起因して急激に低減し、奥壁面4b
からの反則流量に起因するガイド孔4の開放口からの流
体漏洩が急激に増える。これにより緯糸先端部が緯入れ
通路Sから飛び出すという飛走ドラフルが多発するよう
になり、座標点×(α、■1)が緯入れ安定性の限界を
表すことになる。
The curve C1 in FIG. 4 represents the slope angle θ1 of the upper wall surface 4a and the back wall surface 4.
The weft flying speed is shown when the inclination angle θ2 of b is made equal, and the curve C2 shows the flying speed in the case of this example. When the inclination angle θ2 is made equal to the inclination angle θ1, fluid leakage from between the inner wall surfaces 4b is reduced, and a decrease in flow velocity due to this fluid leakage is reduced. Therefore, the rate of increase in weft speed as the inclination angle θ1 increases in the case of θ1-02 is higher than in the case of the present embodiment (θ1>θ2), which is convenient for increasing the weft flying speed. However, when the weft flying speed exceeds a certain limit (indicated by The effect of suppressing the action directed toward the opening of No. 4 by the reflected flow from the -1-wall surface 4a is rapidly reduced due to the reduction in fluid leakage from between the back wall surface 4b, and
Fluid leakage from the opening of the guide hole 4 due to the irregular flow rate increases rapidly. As a result, flying druffles in which the weft tip jumps out of the weft insertion path S occur frequently, and the coordinate point x (α, ■1) represents the limit of weft insertion stability.

本実施例の場合(θ1〉θ2)、奥壁面4b間からの流
体漏洩作用と上壁面4aからの反射流による前記抑制作
用とが効率よく整合し、飛走トラブルが多発するように
なる限界Yが座標点X(α。
In the case of this embodiment (θ1>θ2), the fluid leakage effect from between the inner wall surfaces 4b and the suppressing effect due to the reflected flow from the upper wall surface 4a are efficiently matched, and the limit Y at which flight troubles occur frequently is the coordinate point X(α.

V、)で表される緯入れ安定性の限界を越える。The limit of weft insertion stability expressed by V, ) is exceeded.

限界Yを座標点Y(β、V2)で表せは、β〉αかつv
2 >vlとなり、傾斜角θ1を適宜増大することによ
り飛走トラブルを抑制しつつ緯糸飛走速度を高めること
ができる。これは、ガイド孔4の開放口からの流体漏洩
を抑制する作用と奥壁面4b間からの流体漏洩による緯
糸引き付は作用との適切な整合により得られるものであ
り、この適切な整合性が奥壁面4bの傾斜角θ2を」二
壁面4aの傾斜角θ1よりも小さくすることにより得ら
れる。
Express the limit Y by the coordinate point Y (β, V2), if β>α and v
2>vl, and by appropriately increasing the inclination angle θ1, it is possible to increase the weft flying speed while suppressing flying troubles. This is because the action of suppressing fluid leakage from the opening of the guide hole 4 and the action of pulling the weft yarn due to fluid leakage from between the inner wall surface 4b are obtained by appropriate matching, and this proper matching This is obtained by making the inclination angle θ2 of the rear wall surface 4b smaller than the inclination angle θ1 of the second wall surface 4a.

本発明は勿論前記実施例にのみ限定されるものではなく
、例えば緯入れ用補助ノズル2の噴射方向が上壁面4a
と奥壁面4bとの境界から上壁面4a寄りあるいは奥壁
面4b寄りを指向するように設定してもよく、このよう
な設定によっても」二壁面4aからの反射流による奥壁
面4bからの反射流の制御は効果的に行われる。又、ガ
イド孔の下壁面の傾斜角を奥壁面の傾斜角に合わせても
よい。
Of course, the present invention is not limited to the above-mentioned embodiments. For example, the injection direction of the weft insertion auxiliary nozzle 2 is
It may be set to point toward the upper wall surface 4a or the rear wall surface 4b from the boundary between the upper wall surface 4b and the rear wall surface 4b. control is carried out effectively. Further, the angle of inclination of the lower wall surface of the guide hole may be made to match the angle of inclination of the inner wall surface.

さらに、奥壁面4bは第1図のように緯入れ側から見て
、実施例のように筬羽の長手方向に直線的な壁面に限ら
ず、湾曲状あるいはほぼ湾曲に近い壁面に形成しても本
発明を実施することができる。
Furthermore, when viewed from the weft insertion side as shown in FIG. 1, the back wall surface 4b is not limited to a wall surface that is straight in the longitudinal direction of the reed blades as in the embodiment, but may be formed into a curved or almost curved wall surface. The present invention can also be practiced.

[発明の効果] 以上詳述したように本発明は、上壁面及び奥壁面に交差
する噴射流路を持つように緯入れ用補助ノズルの噴射方
向を設定し、上壁面及び奥壁面を緯入れ方向に対して傾
斜させると共に、上壁面の傾斜角を奥壁面の傾斜角より
も大きくしたので、上壁面からの反射流による奥壁面か
らの反射流の適切な制御、即ちガイド孔の開放口からの
流体漏洩を抑制する作用と奥壁面4b間からの流体漏洩
による緯糸引き付は作用とを適切に整合することができ
、これにより飛走トラブル発生を抑制しつつ緯糸飛走速
度を高め得るという優れた効果を奏する。
[Effects of the Invention] As detailed above, the present invention sets the injection direction of the auxiliary nozzle for weft insertion so as to have an injection flow path that intersects the upper wall surface and the back wall surface, and inserts the weft into the upper wall surface and the back wall surface. Since the angle of inclination of the upper wall surface is made larger than the angle of inclination of the rear wall surface, it is possible to appropriately control the reflected flow from the rear wall surface by the reflected flow from the upper wall surface, that is, from the opening of the guide hole. It is possible to appropriately match the action of suppressing fluid leakage between the inner wall surface 4b and the action of pulling the weft yarn due to fluid leakage from between the back wall surfaces 4b, thereby increasing the weft flight speed while suppressing the occurrence of flying troubles. It has excellent effects.

【図面の簡単な説明】[Brief explanation of the drawing]

図面は本発明を具体化した一実施例を示し、第1図は側
断面図、第2図は第1図のA−A線拡大断面図、第3図
は第1図の13−B線拡大断面図、第4図は上壁面の傾
斜角と緯糸飛走速度との関係を示すグラフである。 緯入れ用補助ノズル2、噴射口2a、変形筬3、ガイド
孔4、上壁面4a、奥壁面4b、緯入れ通路S、傾斜角
θ1.θ2、噴射方向P。
The drawings show an embodiment embodying the present invention; FIG. 1 is a side sectional view, FIG. 2 is an enlarged sectional view taken along line A-A in FIG. 1, and FIG. 3 is taken along line 13-B in FIG. 1. The enlarged sectional view, FIG. 4, is a graph showing the relationship between the inclination angle of the upper wall surface and the weft flying speed. Weft insertion auxiliary nozzle 2, injection port 2a, deformed reed 3, guide hole 4, upper wall surface 4a, back wall surface 4b, weft insertion passage S, inclination angle θ1. θ2, injection direction P.

Claims (1)

【特許請求の範囲】[Claims] 1 多数枚の筬羽の前面に凹設されたガイド孔の列によ
り形成される緯入れ通路に向けて緯入れ用メインノズル
から緯糸を射出すると共に、複数の緯入れ用補助ノズル
からの噴射流により緯入れ通路内の緯糸の飛走を助勢す
るジェットルームにおいて、上壁面、下壁面及び奥壁面
からなる前記ガイド孔の下壁面の開放端近傍に緯入れ用
補助ノズルの噴射口を設定すると共に、前記上壁面及び
奥壁面に交差する噴射流路を持つように緯入れ用補助ノ
ズルの噴射方向を設定し、緯入れ方向へ向かうにつれて
緯入れ通路側へ入り込む傾斜を上壁面及び奥壁面に設け
ると共に、上壁面の傾斜角を奥壁面の傾斜角よりも大き
くしたジェットルームにおける緯入れ装置。
1 The weft is ejected from the main nozzle for weft insertion toward the weft insertion path formed by the row of guide holes recessed in the front surface of a large number of reed blades, and the jet stream is ejected from the plurality of auxiliary nozzles for weft insertion. In the jet loom that assists the flight of the weft yarn in the weft insertion passage, the injection port of the weft insertion auxiliary nozzle is set near the open end of the lower wall surface of the guide hole consisting of an upper wall surface, a lower wall surface, and a back wall surface. The injection direction of the weft insertion auxiliary nozzle is set so as to have an injection flow path that intersects with the upper wall surface and the back wall surface, and an inclination is provided on the upper wall surface and the back wall surface so that the weft insertion path enters the weft insertion path as it goes in the weft insertion direction. Also, a weft insertion device in a jet loom in which the angle of inclination of the upper wall surface is larger than the angle of inclination of the back wall surface.
JP63144148A 1988-06-10 1988-06-10 Weft insertion device in jet loom Expired - Lifetime JP2623701B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP63144148A JP2623701B2 (en) 1988-06-10 1988-06-10 Weft insertion device in jet loom

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP63144148A JP2623701B2 (en) 1988-06-10 1988-06-10 Weft insertion device in jet loom

Publications (2)

Publication Number Publication Date
JPH01314753A true JPH01314753A (en) 1989-12-19
JP2623701B2 JP2623701B2 (en) 1997-06-25

Family

ID=15355334

Family Applications (1)

Application Number Title Priority Date Filing Date
JP63144148A Expired - Lifetime JP2623701B2 (en) 1988-06-10 1988-06-10 Weft insertion device in jet loom

Country Status (1)

Country Link
JP (1) JP2623701B2 (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1992017630A1 (en) * 1991-04-01 1992-10-15 Kabushiki Kaisha Toyoda Jidoshokki Seisakusho Weft inserting device in jet loom
JPH0586544A (en) * 1991-04-01 1993-04-06 Toyota Autom Loom Works Ltd Picking device of jet loom, reed for picking device and production of the reed
EP1400617A2 (en) * 2002-09-18 2004-03-24 Tsudakoma Kogyo Kabushiki Kaisha Running weft control device of air-jet loom
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
CN111663232A (en) * 2019-03-06 2020-09-15 株式会社丰田自动织机 Weft insertion device of air jet loom

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1992017630A1 (en) * 1991-04-01 1992-10-15 Kabushiki Kaisha Toyoda Jidoshokki Seisakusho Weft inserting device in jet loom
JPH0586544A (en) * 1991-04-01 1993-04-06 Toyota Autom Loom Works Ltd Picking device of jet loom, reed for picking device and production of the reed
US5323814A (en) * 1991-04-01 1994-06-28 Kabushiki Kaisha Toyoda Jidoshokki Seisakusho Reed pieces with recessed weft guide openings having inclined surfaces
EP1400617A2 (en) * 2002-09-18 2004-03-24 Tsudakoma Kogyo Kabushiki Kaisha Running weft control device of air-jet loom
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
CN111663232A (en) * 2019-03-06 2020-09-15 株式会社丰田自动织机 Weft insertion device of air jet loom
CN111663232B (en) * 2019-03-06 2021-07-06 株式会社丰田自动织机 Weft insertion device of air jet loom

Also Published As

Publication number Publication date
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