JPH0149558B2 - - Google Patents
Info
- Publication number
- JPH0149558B2 JPH0149558B2 JP61061578A JP6157886A JPH0149558B2 JP H0149558 B2 JPH0149558 B2 JP H0149558B2 JP 61061578 A JP61061578 A JP 61061578A JP 6157886 A JP6157886 A JP 6157886A JP H0149558 B2 JPH0149558 B2 JP H0149558B2
- Authority
- JP
- Japan
- Prior art keywords
- sewing
- sheet material
- wing
- lace
- sewn
- 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
Links
- 238000009958 sewing Methods 0.000 claims description 83
- 239000000463 material Substances 0.000 claims description 71
- 238000000034 method Methods 0.000 claims description 27
- 238000004519 manufacturing process Methods 0.000 claims description 20
- 239000004745 nonwoven fabric Substances 0.000 claims description 3
- 229920003002 synthetic resin Polymers 0.000 claims description 2
- 239000000057 synthetic resin Substances 0.000 claims description 2
- 239000002759 woven fabric Substances 0.000 claims description 2
- 230000000694 effects Effects 0.000 description 5
- 238000010586 diagram Methods 0.000 description 4
- 239000004677 Nylon Substances 0.000 description 3
- 229920001778 nylon Polymers 0.000 description 3
- 239000010802 sludge Substances 0.000 description 3
- 239000000835 fiber Substances 0.000 description 2
- 230000014759 maintenance of location Effects 0.000 description 2
- 244000005700 microbiome Species 0.000 description 2
- 239000002689 soil Substances 0.000 description 2
- 239000002351 wastewater Substances 0.000 description 2
- OEPOKWHJYJXUGD-UHFFFAOYSA-N 2-(3-phenylmethoxyphenyl)-1,3-thiazole-4-carbaldehyde Chemical compound O=CC1=CSC(C=2C=C(OCC=3C=CC=CC=3)C=CC=2)=N1 OEPOKWHJYJXUGD-UHFFFAOYSA-N 0.000 description 1
- 241000251468 Actinopterygii Species 0.000 description 1
- 101100008044 Caenorhabditis elegans cut-1 gene Proteins 0.000 description 1
- 101100008047 Caenorhabditis elegans cut-3 gene Proteins 0.000 description 1
- 238000005273 aeration Methods 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- 229920006248 expandable polystyrene Polymers 0.000 description 1
- 230000007774 longterm Effects 0.000 description 1
- 230000010355 oscillation Effects 0.000 description 1
- 229920002635 polyurethane Polymers 0.000 description 1
- 239000004814 polyurethane Substances 0.000 description 1
- 230000000717 retained effect Effects 0.000 description 1
- 239000002893 slag Substances 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 238000004065 wastewater treatment Methods 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Classifications
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02A—TECHNOLOGIES FOR ADAPTATION TO CLIMATE CHANGE
- Y02A40/00—Adaptation technologies in agriculture, forestry, livestock or agroalimentary production
- Y02A40/80—Adaptation technologies in agriculture, forestry, livestock or agroalimentary production in fisheries management
- Y02A40/81—Aquaculture, e.g. of fish
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02P—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
- Y02P60/00—Technologies relating to agriculture, livestock or agroalimentary industries
- Y02P60/60—Fishing; Aquaculture; Aquafarming
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02W—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO WASTEWATER TREATMENT OR WASTE MANAGEMENT
- Y02W10/00—Technologies for wastewater treatment
- Y02W10/10—Biological treatment of water, waste water, or sewage
Landscapes
- Braiding, Manufacturing Of Bobbin-Net Or Lace, And Manufacturing Of Nets By Knotting (AREA)
- Cultivation Of Plants (AREA)
- Pit Excavations, Shoring, Fill Or Stabilisation Of Slopes (AREA)
- Biological Treatment Of Waste Water (AREA)
- Artificial Fish Reefs (AREA)
- Hydroponics (AREA)
- Sewing Machines And Sewing (AREA)
Description
【発明の詳細な説明】
〔産業上の利用分野〕
この発明は排水処理ろ床の接触材のほか、例え
ば土工事用の土留剤、水耕栽培用の床材、魚礁
(産卵用)などにも使用できるひも状の部材に関
する。[Detailed Description of the Invention] [Industrial Application Field] This invention is applicable not only to contact materials for wastewater treatment filter beds, but also to earth retention agents for earthworks, bed materials for hydroponic cultivation, fish reefs (for spawning), etc. The present invention relates to a string-like member that can also be used.
以下、接触材を例に説明する。 Hereinafter, the contact material will be explained as an example.
第7図は従来のひも状接触材を示す図で、同図
aは側面図、同図bはその断面図である。この接
触材20は、外面が多数の塩化ビニリデンなどの
細い繊維の輪状体で覆われているひも状の部材で
あつて、例えばモール状外径は25mmφ、引張強度
は10Kg程度に構成されている。 FIG. 7 shows a conventional string-like contact material, in which FIG. 7A is a side view and FIG. 7B is a sectional view thereof. This contact material 20 is a string-like member whose outer surface is covered with a large number of rings of thin fibers such as vinylidene chloride, and has a molded outer diameter of 25 mmφ and a tensile strength of about 10 kg, for example. .
この接触材20は、例えば1m幅の展張棹に、
長さ1〜5mの接触材20の上下端を締結するよ
うにして30〜50mmの間隔でもつて複数本張り渡
し、接触はつ気槽内に所定の間隔でもつて吊下げ
方式で装着して使用されるもので、従来の接触材
に比べて、空〓率が高く、槽内流速が速くとれ
るので接触効果が良好であるとともに、保持汚泥
量が多いので容積負荷を大きくとることができ
る。ひも状であるため、槽内への取付が自由で
あり、槽の構造および容積負荷に適した設定がで
きる。といつた利点がある。 This contact material 20 can be applied to, for example, a 1 m wide expanded rod.
A plurality of contact materials 20 having a length of 1 to 5 m are tied together at the upper and lower ends at intervals of 30 to 50 mm, and used by hanging them in a contact aeration tank at predetermined intervals. Compared to conventional contact materials, the porosity is higher and the flow rate in the tank can be faster, so the contact effect is better, and the amount of sludge retained is larger, so a larger volume load can be achieved. Since it is string-shaped, it can be installed freely inside the tank, and settings can be made to suit the structure and volumetric load of the tank. There are some advantages.
しかし、上記ひも状接触材20は、輪状体の繊
維に活性汚泥が付着してゆくと、その表面が粘着
性の物質で覆われてゆき、遂には全体が1つの捧
状となる目づまりを生じ、接触面積が著しく減少
するという問題点があつた。
However, as the activated sludge adheres to the fibers of the ring-shaped contact material 20, its surface becomes covered with a sticky substance, and the string-like contact material 20 eventually becomes clogged and becomes a single slag. However, there was a problem in that the contact area was significantly reduced.
この発明はかかる問題点の解決を目的としてな
されたもので、ひも状接触材20の上記特性を保
有しながら接触効率が低下しない接触材を得るこ
と、およびその生産性の良い製造方法を得ること
を目的とする。 The present invention has been made to solve these problems, and aims to obtain a contact material that maintains the above-mentioned characteristics of the string-like contact material 20 and which does not reduce the contact efficiency, and to obtain a method for manufacturing the same with high productivity. With the goal.
(1) この発明に係るウイングレースは、帯状のシ
ート材と、このシート材に、その幅より小さい
波高の波形パターンで縫いつけられている所定
の引張強さを有する縫糸と、上記帯状のシート
材の両縁から、上記縫糸の各波形パターンの波
高部近傍に達する横向の切り目を形成してなる
ものである。
(1) The wing lace according to the present invention includes a belt-shaped sheet material, a sewing thread having a predetermined tensile strength that is sewn to the sheet material in a wave pattern with a wave height smaller than the width of the sheet material, and Horizontal cuts are formed from both edges of the sewing thread to the vicinity of the crest of each wave pattern of the sewing thread.
(2) この発明に係るウイングレースの第1の製造
方法は、幅広のシート材に、所定の幅間隔でも
つて複数列の波形パターンに縫糸を縫いつけて
ゆく縫製工程と、上記シート材の上記各波形パ
ターンの中間部から各波高部近傍への横向の切
り目を形成する工程と、上記シート材を上記波
形パターンの中間部で縦方向に切断してゆく工
程とを含む製造方法である。(2) A first method for manufacturing wing lace according to the present invention includes a sewing step of sewing sewing thread into a wide sheet material in a plurality of rows of wavy patterns at predetermined width intervals; This manufacturing method includes the steps of forming horizontal cuts from the middle part of the wave pattern to the vicinity of each wave height, and cutting the sheet material in the longitudinal direction at the middle part of the wave pattern.
(3) この発明に係るウイングレースの第2の製造
方法は、縦、横両方向に伸展したとき、網目が
形成されるように構成されているものの製造方
法であつて、広幅のシート材の縦方向に、所定
の幅間隔で、所定の波数ごとに左、右交互に波
高の高い波形パターンに複数列の縫糸を縫つけ
てゆく第1の縫製工程と、これらの縫糸の中間
を上記波形パターンとは逆向の波形パターンで
もつてかつ、波高の高い部分で隣りの縫糸の波
高の高い部分と交叉するように縫糸を縫いつけ
てゆく第2の縫製工程と、上記シート材の上記
各波形パターンの波高部と隣りの波高部との間
の部分に横方向の切り目を形成する第1の切り
目形成工程と、上記シート材の各波形パターン
の交叉部と隣りの交叉部との間の部分に縦向の
切り目を形成する第2の切り目形成工程とを含
む製造方法である。(3) The second method for manufacturing a wing lace according to the present invention is a method for manufacturing a wing lace that is configured to form a mesh when stretched in both the vertical and horizontal directions, and is a method for manufacturing a wing lace made of a wide sheet material in the longitudinal direction. A first sewing process in which multiple rows of sewing thread are sewn in a waveform pattern with high wave height alternately on the left and right sides at predetermined width intervals and every predetermined wave number, and the middle of these sewing threads is sewn into the above-mentioned waveform pattern. A second sewing process in which the sewing thread is sewn in a wave pattern in the opposite direction to that of the previous sewing thread in such a way that the high wave height part intersects the high wave height part of the adjacent sewing thread, and the wave height of each of the wave patterns of the sheet material. A first cut forming step of forming a horizontal cut in a portion between a portion and an adjacent wave height portion, and a vertical cut forming step in a portion between an intersection portion of each wave pattern of the sheet material and an adjacent intersection portion. This is a manufacturing method including a second cut forming step of forming a cut.
(1) この発明に係るウイングレースは、縫糸の両
端を持つて伸張すると、シート材は切り目が開
き、直線状に伸長した縫糸に対して傾斜した曲
面を持つ翼片となつて起立する。起立した各翼
片の表面は、接触面として作用し、縫糸はこの
部材に加わる引張荷重を支承する部材として作
用する。このウイングレースを接触材に用いた
場合には、翼片の表面に微生物が付着するとと
もに、汚水の流れにしたがつて、各翼片が揺動
するので汚水との接触効率が高く、微生物の付
着量が増加しても表面積がほとんど変化しない
ので、接触効率の低下を生じない。
(1) When the wing lace according to the present invention is stretched by holding both ends of the sewing thread, the sheet material opens the cut and stands up as a wing piece with a curved surface that is inclined with respect to the linearly stretched sewing thread. The surface of each raised wing acts as a contact surface, and the suture acts as a member to support the tensile loads applied to this member. When this wing race is used as a contact material, microorganisms adhere to the surface of the wing pieces, and each wing piece oscillates according to the flow of wastewater, so the contact efficiency with wastewater is high and the microorganisms are Even if the amount of adhesion increases, the surface area hardly changes, so there is no decrease in contact efficiency.
(2) この発明に係るウイングレースの第1の製造
方法は、シート材に所定の引張強さをもつ縫糸
を所定の幅間隔でもつて波形パターンに縫いつ
けてゆく縫製工程と、上記シート材を上記各波
形パターンの中間部から各波高部近傍への横向
の切り目を形成する工程と、上記シート材を上
記波形パターンの中間部で縦向に切断してゆく
工程とを一連の流れ工程として施すことができ
るので生産性が向上する。(2) A first method for manufacturing wing lace according to the present invention includes a sewing process in which a sewing thread having a predetermined tensile strength is sewn onto a sheet material in a wavy pattern at predetermined width intervals; A step of forming a horizontal cut from the middle part of each wave pattern to the vicinity of each wave height part, and a step of cutting the sheet material vertically at the middle part of the wave pattern are performed as a series of flow steps. This improves productivity.
(3) この発明に係るウイングレースの第2の製造
方法は、第1のミシンと第2のミシンとを同じ
動作パターンで横方向に張りながらシート材を
縦方向に送つて縫うことにより所定の波数ごと
に、左・右交互に高い波高部で交叉する波形パ
ターンでもつて縫つてゆくことができ、この縫
製工程と、各波形パターンの中間部から隣りの
波高部近傍への横向の切り目形成工程と、上記
シート材の各波形パターンの交叉部と隣りの交
叉部との間を縦向に切断する工程とを一連の流
れ工程として施すことができ、網目状に締結さ
れたリングレースの生産性が向上する。(3) A second method for manufacturing wing lace according to the present invention is to sew a sheet material in the vertical direction by using the first sewing machine and the second sewing machine in the same operation pattern while stretching the sheet material in the horizontal direction. For each wave number, it is possible to sew waveform patterns that alternately intersect at high wave heights on the left and right sides, and this sewing process and the process of forming horizontal cuts from the middle of each waveform pattern to the vicinity of the adjacent wave height. and the process of vertically cutting between each intersection of each wave pattern of the sheet material and the adjacent intersection can be performed as a series of flow processes, increasing the productivity of the ring lace fastened in a mesh pattern. will improve.
(1)第1図はウイングレースの一実施例の正面図
で、1は帯状のシート材で、例えば幅wが5cm、
長さ数十mの不織布で構成される。2は縫糸で、
例えばナイロンフイラメント縫糸品種番号3(引
張強さ9450g)で本縫、環縫もしくは二重環縫で
もつて、三角波パターンに縫われている。3はシ
ート材1の両側縁1aから、縫糸2の波高部の近
傍2aまで形成されている横向の切り目で、縫糸
2の両端をもつて伸長したとき、第2図に示すよ
うに、シート材1は切り目1から開き、縫糸2の
両側に、わん曲面を画いて起立する翼片1bが形
成される。
(1) Figure 1 is a front view of one embodiment of the wing lace. 1 is a belt-shaped sheet material, for example, the width w is 5 cm,
It is made of non-woven fabric with a length of several tens of meters. 2 is sewing thread,
For example, nylon filament sewing thread type number 3 (tensile strength 9450 g) is used to sew in a triangular wave pattern using lock stitch, chain stitch, or double chain stitch. 3 is a horizontal cut formed from both side edges 1a of the sheet material 1 to the vicinity 2a of the wave height of the sewing thread 2, and when the sewing thread 2 is stretched with both ends, as shown in FIG. 2, the sheet material 1 opens from the cut 1, and wing pieces 1b are formed on both sides of the sewing thread 2, forming curved surfaces and standing upright.
このウイングレース4は、縫糸2が2本の3番
のナイロンフイラメント縫糸で構成されているか
ら、その引張強さは約20Kgであり、長さ5mの接
触材として使用しても十分な引張強さを有してお
り、従来の接触材と同じ状態でろ床に使用して
も、目づまり、接触効率の低下のない接触材とし
て使用できる。 This wing lace 4 has a tensile strength of approximately 20 kg because the sewing thread 2 is composed of two No. 3 nylon filament sewing threads, which is sufficient even when used as a contact material with a length of 5 m. Even when used in filter beds in the same conditions as conventional contact materials, it can be used as a contact material without clogging or reducing contact efficiency.
第3図は第1図に示したウイングレースの製造
方法の一実施例を説明するための図で、5は広幅
のシート材で、この例では、製造しようとするウ
イング・レース4の幅wの4倍の幅を有し、矢印
A方向に定速度で送られる。6はミシンで、製造
しようとするウイングレース4の幅wと同じ間隔
で配設されている4連の縫針7を有し、幅wより
小さい振れ幅S1の範囲を、シート材5の送りと
連動して矢印Bl,Br方向に往復駆動され、三角
波パターンの縫目を形成してゆく。8は第1のス
リツタで、間隔wで配設されている4連の刃9を
有し、振れ幅S2の範囲を、シート材5の送りと
連動して矢印Cl,Cr方向に往復駆動されて切り
目3を形成してゆく。10は第2のスリツタで、
間隔wで配設されている3連の刃11を有し、シ
ート材5が矢印A方向に送られるのにしたがつ
て、シート材5の各三角波パターンの縫糸2の中
間部を所定の幅wでもつて切断して幅wのウイン
グレース4が形成される。 FIG. 3 is a diagram for explaining an embodiment of the method for manufacturing the wing lace shown in FIG. It has a width four times as wide as , and is sent at a constant speed in the direction of arrow A. Reference numeral 6 denotes a sewing machine, which has four sewing needles 7 arranged at the same intervals as the width w of the wing lace 4 to be manufactured, and feeds the sheet material 5 within a range of a runout width S1 smaller than the width w. They are interlocked and driven back and forth in the directions of arrows Bl and Br, forming triangular wave pattern stitches. A first slitter 8 has four blades 9 arranged at intervals w, and is driven reciprocally in the directions of arrows Cl and Cr in conjunction with the feeding of the sheet material 5 within a range of swing width S2. to form the cut 3. 10 is the second suritsuta,
It has three blades 11 arranged at intervals w, and as the sheet material 5 is fed in the direction of arrow A, the intermediate portion of the sewing thread 2 of each triangular wave pattern of the sheet material 5 is cut to a predetermined width. The wing lace 4 having a width w is formed by cutting the wing lace 4 at a width w.
第4図はこの発明の他の実施例を示す平面図
で、この例は、6条のウイングレース4を、ピツ
チPごとに、隣りのウイングレース4の縫糸2の
波高の高い部分と交叉するように波形パターンが
形成されており、縦および横方向に伸展したと
き、ウイングレース4が網目を形成するように構
成したもので、図中、13a,13bは縫糸2の
交叉部を示している。 FIG. 4 is a plan view showing another embodiment of the present invention. In this example, six wing laces 4 intersect, at every pitch P, a high-wave portion of the sewing thread 2 of the adjacent wing lace 4. A wave pattern is formed as shown in the figure, and the wing lace 4 is configured to form a mesh when stretched in the vertical and horizontal directions. In the figure, 13a and 13b indicate the intersection of the sewing threads 2. .
第5図はこの実施例を伸展した状態を示す平面
図で、この図は第4図に示した実施例のウイング
レースを伸展したときの状態を1/2の縮尺で示し
たものである。このように、この実施例のウイン
グレース4は縦および横方向に伸展すると、縫糸
2の縫目の全長でもつて締結した網状となるの
で、第5図に示したように、アンカ14でもつて
盛土法面などに固定し、網目内に容土すれば、土
壌の保持材としても使用できる。 FIG. 5 is a plan view showing this embodiment in an extended state, and this figure shows the wing race of the embodiment shown in FIG. 4 in an extended state on a 1/2 scale. In this way, when the wing lace 4 of this embodiment is stretched in the vertical and horizontal directions, it becomes a net-like shape in which the entire length of the stitches of the sewing thread 2 is tied together, so that the anchor 14 can also be used to secure the embankment as shown in FIG. It can also be used as a soil retention material by fixing it to a slope or other surface and filling it with soil within a mesh.
なお、この実施例のウイングレース4を、縦方
向のみに伸長して接触材などに使用でき、この場
合は翼片1bの配置が密になつて接触面積が増大
するとともに、各条のウイングレース4が適当な
ピツチPでもつて相互に締結されているので、大
きな引張力でもつて布設することができ、流水に
よつて揺動する振れ幅が小さくなるので、隣接す
る接触材と接触して付着している汚泥が剥離、脱
落することが少なくなる効果もある。 The wing lace 4 of this embodiment can be extended only in the longitudinal direction and used as a contact material, etc. In this case, the wing pieces 1b are arranged densely and the contact area increases, and the wing lace of each strip is 4 are connected to each other with an appropriate pitch P, so it can be laid with a large tensile force, and the amplitude of swinging due to running water is reduced, so it does not contact and adhere to adjacent contact materials. This also has the effect of reducing the amount of sludge that is being removed and falling off.
第6図は第5図に示した網状に締結したウイン
グレースの製造方法の一実施例を説明するための
平面図で、この図は便宜上、縫目の三角波パター
ンの波数を少なくして示している。図において、
ミシン6は、製造するウイングレース4の幅wの
2倍の間隔で縫針7が配設されている第1のミシ
ン6aと、同じ間隔2wでもつて、かつ、第1の
ミシン6aの縫針7の中間の位置に、かつ、第1
のミシン6aとは縦方向にピツチPと同じ距離だ
け離れた位置に縫針7が配設されている第2のミ
シン6bとで構成されており、振れ幅S1と、所
定波数ごとに左・右交互に大きな振れ幅S2で振
れるパターンでもつて矢印Bl,Br方向に往復駆
動され、ピツチPごとに隣りの三角波パターンの
縫糸2の波高の高い部分で縫糸2の交叉部13
a,13bが形成され、この交叉部13a,13
bで締結される。第1のスリツタ8は間隔2wで
もつて配設されている刃9を有し、シート材5が
三角波パターンの1/2波送られるたびに幅方向に
wだけシフトして矢印Cl,Cr方向に移動し、切
り目3a,3bを形成してゆく。15,16は第
2、第3のスリツタで、それぞれ2wの間隔でも
つて、かつ、間隔wだけ幅方向にずれた位置に配
設されている刃11を有し、シート材5の交叉部
13a,13bから次の交叉部13a,13bま
での間を、縦方向に切断して切目12a,12b
を形成してゆき、第5図に示した網状に締結され
たウイングレース4が形成される。 FIG. 6 is a plan view for explaining one embodiment of the method for manufacturing the wing lace fastened in a net shape shown in FIG. There is. In the figure,
The sewing machine 6 has sewing needles 7 disposed at intervals twice the width w of the wing lace 4 to be manufactured. in the middle position and the first
The sewing machine 6a is composed of a second sewing machine 6b in which a sewing needle 7 is disposed at a position vertically separated by the same distance as the pitch P. The sewing thread 2 is driven back and forth in the directions of arrows Bl and Br in a pattern that alternately oscillates with a large oscillation width S2, and at each pitch P, the intersection portion 13 of the sewing thread 2 of the adjacent triangular wave pattern is located at the high wave height part of the sewing thread 2.
a, 13b are formed, and these intersection parts 13a, 13
It is concluded in b. The first slitter 8 has blades 9 arranged at intervals of 2w, and each time the sheet material 5 is fed in a 1/2 wave in a triangular wave pattern, it shifts in the width direction by w in the direction of arrows Cl and Cr. It moves and forms cuts 3a and 3b. Reference numerals 15 and 16 denote second and third slitters, each having blades 11 arranged at an interval of 2w and at positions shifted in the width direction by the interval w, and the blades 11 are arranged at the intersection part 13a of the sheet material 5. , 13b to the next intersection 13a, 13b is cut in the longitudinal direction to form cuts 12a, 12b.
As a result, the wing lace 4 fastened in a net shape as shown in FIG. 5 is formed.
このように、この実施例によれば、複雑な構成
の網状に締結されたウイングレースが、一連の流
れとして施工できる工程によつて製造できる効果
がある。 As described above, this embodiment has the advantage that wing laces fastened in a net-like configuration having a complicated structure can be manufactured by a process that can be executed in a series of steps.
なお、上記実施例では、シート材1に不織布を
用いた例を示したが、織布、または合成樹脂フイ
ルム材、もしくはこれらの一面または両面に、適
当な厚さの発泡ポリウレタンなどの発泡シート材
を貼合わせたもの、または発泡ポリスチレンなど
の発泡シート材そのものであつてもよい。 In addition, in the above embodiment, an example was shown in which a nonwoven fabric was used as the sheet material 1, but a woven fabric, a synthetic resin film material, or a foamed sheet material such as foamed polyurethane of an appropriate thickness may be used on one or both sides of these. It may also be a foamed sheet material such as a foamed polystyrene material or a foamed sheet material itself.
また、縫糸2には、ナイロンフイラメント縫糸
を用いた例を示したが、必要な引張強さの得られ
る縫糸であればよく、その縫い方も本縫いのほ
か、環=縫い、二重環=縫いなど、大きい引張強
さが得られる縫い方であればよいことはいうまで
もない。 Furthermore, although we have shown an example in which a nylon filament sewing thread is used as the sewing thread 2, any sewing thread that can provide the necessary tensile strength can be used, and the sewing methods include lock stitching, ring stitching, double ring stitching, etc. Needless to say, any stitching method that provides high tensile strength, such as stitching, may be used.
また、上記実施例では、三角波パターンに縫つ
た例を示したが、正弦波状、てい形波状などの波
形パターンであつてもよい。 Further, in the above embodiment, an example was shown in which the stitches were sewn in a triangular wave pattern, but a wave pattern such as a sinusoidal wave shape or a rectangular wave shape may also be used.
(1) この発明に係るウイングレースは、帯状のシ
ート材に波形パターンでもつて縫製した縫糸の
両端をもつて伸長したとき、シート材に形成し
た切り目が開いてそれぞれ縫糸に対して曲面を
画いて起立する翼片が形成されるもので、例え
ばろ床用接触材として用いた場合には高い接触
効率が得られるとともに、長期間使用しても、
接触効率の低下の少いものとなるなどの効果が
ある。
(1) In the wing lace according to the present invention, when both ends of a sewing thread sewn in a wave pattern on a band-shaped sheet material are stretched, the cuts formed in the sheet material open and each curved surface is created for the sewing thread. It forms upstanding blades, and when used as a contact material for filter beds, for example, high contact efficiency can be obtained, and even after long-term use,
This has the effect of reducing the drop in contact efficiency.
(2) この発明に係る第1のウイングレースの製造
方法は、複数の縫針を有するミシンで所定の波
形パターンで縫つていくとともに、第1、第2
のスリツタでシート材に幅方向の切り目を形成
するとともに縦方向の裁断とを行うようにした
ので、一連の工程でもつて複数条のウイングレ
ースが製造できる生産性のよい製造方法であ
る。(2) The first method for manufacturing wing lace according to the present invention includes sewing a predetermined wave pattern using a sewing machine having a plurality of sewing needles, and
Since the slitters are used to form cuts in the width direction of the sheet material and to cut the sheet material in the longitudinal direction, it is a highly productive manufacturing method that allows multiple wing laces to be produced in a series of steps.
(3) この発明に係る第2のウイングレースの製造
方法は、網目のピツチPだけ縦方向に離れてお
り、かつ、所定幅間隔ずつ横方向にずれた位置
に配設されている複数の縫針を備えている第
1、第2のミシンでもつて、所定の波数ごとに
左・右交互に高い波高をもつ波形パターンでも
つて縫糸で縫製してゆくとともに、第1のスリ
ツタで幅方向の切り目を、また、第2、第3の
スリツタで各波形パターンの交叉部とつぎの交
叉部との間の縦方向の切り目を形成するように
したので、一連の工程でもつて、複数条のウイ
ングレースが網目状に締結されているものを製
造することができる。(3) The second wing lace manufacturing method according to the present invention includes a plurality of sewing needles that are spaced apart in the vertical direction by the mesh pitch P and are disposed at positions shifted in the horizontal direction by predetermined width intervals. Using the first and second sewing machines equipped with In addition, since the second and third slitters are used to form vertical cuts between the intersections of each wave pattern and the next intersection, multiple wing laces can be formed in a series of steps. It is possible to manufacture products that are fastened in a mesh pattern.
第1図はこの発明の一実施例の平面図、第2図
はこの実施例のウイングレースを伸長した状態を
示す平面図、第3図はこの第2図に示したウイン
グレースの製造方法の一実施例を説明するための
図、第4図はこの発明の他の実施例の平面図で、
複数条のウイングレースを網状に締結したものを
示す図、第5図はこの第4図に示したウイングレ
ースを縦および横方向に伸展したときの状態を示
す平面図、第6図は第4図に示した網状に締結し
たウイングレースの製造方法の一実施例を説明す
るための図、第7図は従来のひも状接触材を示す
図である。
1……帯状のシート材、1a……側縁、1b…
…翼片、2……縫糸、2a……波高部の近傍、3
……横向の切り目、4……ウイング・レース、5
……広幅のシート材、6,6a,6b……ミシ
ン、7……縫針、8,10,15,16……スリ
ツタ、9,11……刃、12a,12b……縦向
の切り目、13a,13b……縫糸の交叉部。な
お、各図中、同一符号はそれぞれ同一、または相
当部分を示す。
FIG. 1 is a plan view of an embodiment of the present invention, FIG. 2 is a plan view showing the wing lace of this embodiment in an extended state, and FIG. 3 is a plan view of the wing lace manufacturing method shown in FIG. 2. A diagram for explaining one embodiment, FIG. 4 is a plan view of another embodiment of the present invention,
Fig. 5 is a plan view showing the wing lace shown in Fig. 4 when it is stretched in the vertical and horizontal directions; FIG. 7 is a diagram illustrating an embodiment of the method for manufacturing the wing lace fastened into a mesh shown in the figure, and FIG. 7 is a diagram showing a conventional string-like contact material. 1... Band-shaped sheet material, 1a... Side edge, 1b...
... Wing piece, 2 ... Sewing thread, 2a ... Near the wave height, 3
...Horizontal cut, 4...Wing lace, 5
... Wide sheet material, 6, 6a, 6b ... Sewing machine, 7 ... Sewing needle, 8, 10, 15, 16 ... Sliver, 9, 11 ... Blade, 12a, 12b ... Vertical cut, 13a , 13b... intersection of sewing threads. In each figure, the same reference numerals indicate the same or corresponding parts.
Claims (1)
心線を越えて他縁に向う横向の切り目が形成され
ている帯状のシート材と、このシート材の上記各
切り目の終端部近傍に波高部をもつ波形パターン
に縫いつけられている所定の引張強さを有する縫
糸とよりなり、上記縫糸の両端をもつて伸張した
とき上記シート材が各切り目から開き、それぞれ
伸張した縫糸に対して傾斜した曲面を画いて起立
する翼片を形成するように構成してなるウイング
レース。 2 縫糸が、本縫、環縫または二重環縫で縫製さ
れてなる特許請求の範囲第1項記載のウイングレ
ース。 3 複数条のウイングレースの縫糸が、それぞれ
両隣りのウイングレースの縫糸とそれぞれ所定の
波間隔でもつて左右交互に縫い合わされてなり、
各レースの縫糸を伸長するとともに横方向にも伸
長したとき、各レースが網目を形成するように構
成した特許請求の範囲第1項記載のウイングレー
ス。 4 シート材が、織布、不織布、合成樹脂シート
材、または少なくとも一面が発泡体であるシート
材である特許請求の範囲第1項または第3項記載
のウイングレース。 5 幅広のシート材の縦方向に、所定の幅間隔で
もつて複数列の波形パターンに縫糸を縫いつけて
ゆく縫製工程と、上記シート材を上記波形パター
ンの中間部から各波高部近傍への横向の切り目を
形成する工程と、上記シート材を上記波形パター
ンの中間部で縦方向に切断してゆく工程とを含む
ウイングレースの製造方法。 6 幅広のシート材の縫方向に所定の幅間隔で、
所定の波数ごとに左右交互に波高の高い波形パタ
ーンに複数列の縫糸を縫いつけてゆく第1の縫製
工程と、これらの縫糸の中間を上記波形パターン
とは逆向の波形パターンでもつて、かつ、波高の
高い部分で隣りの縫糸の波高の高い部分と交叉す
るように縫糸を縫いつけてゆく第2の縫成工程
と、上記シート材の上記各波形パターンの波高部
と隣りの波高部との間の部分に横方向の切り目を
形成する第1の切り目形成工程と、上記シート材
の各波形パターンの交叉部と隣りの交叉部との間
の部分に縫向の切り目を形成する第2の切り目形
成工程とを含むウイングレースの製造方法。 7 シート材の幅方向に、所定の幅間隔でもつて
複数の縫針が配設されている第1のミシンと、こ
の第1のミシンの各縫針の間に、かつ、縦方向に
所定距離離れた位置にそれぞれ配設されている複
数の縫針を有する第2のミシンとを備え、上記第
1、第2のミシンを同時にかつ、所定の波数ごと
に振幅を大きくして隣の縫糸と交叉するように横
方向に変位させながらシート材を縦方向に送つて
第1、第2の縫製工程を施すようにした特許請求
の範囲第6項記載のウイングレースの製造方法。[Scope of Claims] 1. A belt-shaped sheet material in which horizontal cuts are formed alternately from both side edges to the other edge beyond the center line at a predetermined pitch, and the terminal ends of each of the above-mentioned cuts of this sheet material. It consists of a sewing thread having a predetermined tensile strength that is sewn into a wave pattern with crests near the edges, and when both ends of the sewing thread are stretched, the sheet material opens from each cut, and the stretched sewing thread A wing race that is constructed to form wing pieces that stand up with curved surfaces that are slanted. 2. The wing lace according to claim 1, wherein the sewing thread is sewn by lock stitch, chain stitch, or double chain stitch. 3 Multiple threads of wing lace are sewn together alternately on the left and right with the threads of the wing lace on both sides at a predetermined wave interval, respectively,
The wing lace according to claim 1, wherein each lace is configured to form a mesh when the threads of each lace are stretched and also stretched in the lateral direction. 4. The wing lace according to claim 1 or 3, wherein the sheet material is a woven fabric, a nonwoven fabric, a synthetic resin sheet material, or a sheet material whose at least one side is a foamed material. 5 A sewing process in which sewing thread is sewn into multiple rows of wavy patterns at predetermined width intervals in the longitudinal direction of a wide sheet material, and a sewing process in which the sheet material is sewn horizontally from the middle part of the wavy pattern to the vicinity of each crest. A method for manufacturing a wing lace comprising the steps of forming a cut, and cutting the sheet material in the longitudinal direction at an intermediate portion of the wave pattern. 6 At specified width intervals in the sewing direction of the wide sheet material,
A first sewing process in which multiple rows of sewing thread are sewn in a waveform pattern with a high wave height alternately on the left and right for each predetermined number of waves, and the middle of these sewing threads is sewn in a waveform pattern in the opposite direction to the above waveform pattern, and a second sewing step in which the sewing thread is sewn so as to intersect with the high wave portion of the adjacent sewing thread at the high portion of the sheet material; a first cut forming step of forming a transverse cut in the section; and a second cut forming step of forming a cut in the sewing direction in a portion between each intersection of each wave pattern of the sheet material and an adjacent intersection. A method for manufacturing wing lace including a process. 7 A first sewing machine in which a plurality of sewing needles are arranged at predetermined width intervals in the width direction of the sheet material, and a sewing machine with a predetermined distance between each sewing needle of this first sewing machine and a predetermined distance in the vertical direction. and a second sewing machine having a plurality of sewing needles respectively arranged at different positions, the first sewing machine and the second sewing machine simultaneously operate the sewing thread by increasing the amplitude at each predetermined wave number so as to intersect adjacent sewing threads. 7. The method of manufacturing a wing lace according to claim 6, wherein the first and second sewing steps are performed by feeding the sheet material in the longitudinal direction while displacing it in the lateral direction.
Priority Applications (5)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP61061578A JPS62241599A (en) | 1986-03-18 | 1986-03-18 | Wing lace and its production |
| EP19870902138 EP0273053B1 (en) | 1986-03-18 | 1987-03-18 | Sheet for forming twisted surface and production thereof |
| US07/130,383 US4818579A (en) | 1986-03-18 | 1987-03-18 | Sheet for forming twisted flaps in continuous arrangement and method of producing same |
| DE3789144T DE3789144T2 (en) | 1986-03-18 | 1987-03-18 | SHEET FOR THE FORMATION OF A FOLDED SURFACE AND THE PRODUCTION THEREOF. |
| PCT/JP1987/000169 WO1987005642A1 (en) | 1986-03-18 | 1987-03-18 | Sheet for forming twisted surface and production thereof |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP61061578A JPS62241599A (en) | 1986-03-18 | 1986-03-18 | Wing lace and its production |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS62241599A JPS62241599A (en) | 1987-10-22 |
| JPH0149558B2 true JPH0149558B2 (en) | 1989-10-25 |
Family
ID=13175148
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP61061578A Granted JPS62241599A (en) | 1986-03-18 | 1986-03-18 | Wing lace and its production |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS62241599A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR20150091990A (en) * | 2014-02-03 | 2015-08-12 | 가부시키가이샤 도요다 지도숏키 | Variable displacement type swash plate compressor |
-
1986
- 1986-03-18 JP JP61061578A patent/JPS62241599A/en active Granted
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR20150091990A (en) * | 2014-02-03 | 2015-08-12 | 가부시키가이샤 도요다 지도숏키 | Variable displacement type swash plate compressor |
Also Published As
| Publication number | Publication date |
|---|---|
| JPS62241599A (en) | 1987-10-22 |
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