JP2005315334A - Cold forging type manufacturing method of butterfly screw - Google Patents

Cold forging type manufacturing method of butterfly screw Download PDF

Info

Publication number
JP2005315334A
JP2005315334A JP2004133319A JP2004133319A JP2005315334A JP 2005315334 A JP2005315334 A JP 2005315334A JP 2004133319 A JP2004133319 A JP 2004133319A JP 2004133319 A JP2004133319 A JP 2004133319A JP 2005315334 A JP2005315334 A JP 2005315334A
Authority
JP
Japan
Prior art keywords
individual
butterfly
winged
circular
fed
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.)
Pending
Application number
JP2004133319A
Other languages
Japanese (ja)
Inventor
Horyu Go
豐隆 呉
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to JP2004133319A priority Critical patent/JP2005315334A/en
Publication of JP2005315334A publication Critical patent/JP2005315334A/en
Pending legal-status Critical Current

Links

Images

Abstract

<P>PROBLEM TO BE SOLVED: To provide a cold forging type manufacturing method of a butterfly screw having favorable strength, hardly causing fracture of both blade parts, and hardly causing corrosion. <P>SOLUTION: In a first process, a circular wire rod material is fed into a rolling machine, and the rolling machine rolls the circular wire rod material into a circular wing material having both blades. In a second process, the wing material is cut to individual wing materials one by one by a cutting die and scissors. In a third process, both cut surfaces of the invididual wing material is retouched smooth to hold the circular part of the central part and oblong blades on both sides. In a fourth process, a recess is formed on both side surfaces of the central part of the individual wing material by pressing. In a fifth process, the bottom of the recess of the individual wing material is removed to form a through hole. In a sixth process, the blade parts on both sides of the individual wing material is bent upward and shaped like a butterfly to form the individual butterfly material. In a seventh process, a female screw is threaded in the through hole of the individual butterfly material. Thus, a butterfly screw is manufactured. <P>COPYRIGHT: (C)2006,JPO&NCIPI

Description

本発明は、蝶形ねじの製造方法に関するものである。   The present invention relates to a method for manufacturing a butterfly screw.

雄ねじと雌ねじの相互ねじ合せは、機械組合せ上重要な方式で、使用状態や目的の差異により、ねじを持つ部品、例えば、ナットでは、六角形や四角形のものが最も普通に使用されている。もし特別に強力なねじ合せを必要としないならば、取りはずしに便利な蝶形ねじがよく選択される。なぜなら、蝶形ねじは、使用上、工具(例えば、スパナ)がいらず、人手でしめ付けたり、はずしたりできる。蝶形ねじは、しめ付けたあと、相当に結合しているので、色々な日常よく使用される器具用品、例えば、バッテリーの電極、TVのアンテナ、折り畳み式自転車又はスケート板等の中に使用されている。   The mutual screwing of the male screw and the female screw is an important method in the machine combination, and hexagonal or quadrangular ones are most commonly used for parts having screws, for example, nuts, depending on the use state and purpose. If specially strong screw alignment is not required, a butterfly screw that is convenient for removal is often selected. This is because the butterfly screw does not require a tool (for example, a wrench) in use, and can be manually clamped or removed. Since the butterfly screw is fairly connected after it is fastened, it is used in various everyday equipment such as battery electrodes, TV antennas, folding bicycles or skateboards. ing.

目下使用されている従来の蝶形ねじの一種として、図9Aに示している薄板材をプレスで成形したものがある。この蝶形ナットは、中が中空であるので、次の欠点がある。
1.金属材料は、厚みが薄く、ねじを切る工程中に、よく破損し、不合格になるものが少なくない。
One type of conventional butterfly screw currently in use is a thin plate material shown in FIG. 9A formed by pressing. Since this wing nut is hollow, it has the following drawbacks.
1. Metal materials are thin and often break and fail during the threading process.

2.中が中空なので、屋外にあると、風に吹かれたり、日光に照らされたりして、空気により酸化して錆びたりする。それで、両翼部が捩ねられると、断裂し易くなり、取り付けと取りはずしが難しくなる。   2. Since the inside is hollow, when it is outdoors, it is blown by the wind or illuminated by sunlight, and is oxidized and rusted by the air. Therefore, when both wings are twisted, it becomes easy to tear, and attachment and removal become difficult.

3.プレス方式で成形されるので、縁に鋭い毛の様なとげができ易く、それが手指に傷害を与える。
4.プレス方式で成形されるので、金属材料の一部分が屑になり、浪費となり、利益が減少される。
3. Since it is molded by the press method, it is easy to make sharp hair-like thorns at the edges, which damages the fingers.
4). Since it is formed by the press method, a part of the metal material becomes waste, is wasted, and profits are reduced.

次に、従来の蝶形ねじは、図9Bが示す別の一種があり、熔解した材料を砂の鋳型の中に注ぎ込んで成形され、中空でない実心であるが、次の欠点がある。
1.表面が粗雑で滑らかでなく、触感が悪い。
Next, there is another type of conventional butterfly screw as shown in FIG. 9B, which is formed by pouring molten material into a sand mold and is not hollow, but has the following drawbacks.
1. The surface is rough and not smooth, and the touch is poor.

2.成形後に鋳型をはずしたあと、鋳型の注ぎ込み口にでこぼこの欠け口が生じて、手指に傷害を与え易い。
3.鋳型を冷却したら、収縮するので、応力の集中現象が発生し易く、両翼部が比較的大きい外力を受けた場合は断裂し易い。
2. After the mold is removed after molding, bumps are formed at the pouring opening of the mold, and the fingers are easily damaged.
3. Since the mold shrinks when the mold is cooled, a stress concentration phenomenon is likely to occur, and when both wings receive a relatively large external force, they tend to tear.

上述の従来の製造方法による二種の蝶形ねじの欠点に鑑み、強度が良好で容易に両翼部が断裂せず、又、容易に腐触しない蝶形ねじを製造する方法を提供し、又、その製造方法は不合格品を最小限度にし、生産速度を早くし、流水作業を順調な自動式にすることを本発明の課題とする。   In view of the shortcomings of the two types of butterfly screws according to the above-described conventional manufacturing method, there is provided a method for manufacturing a butterfly screw that has good strength and does not easily tear both wings and does not easily corrode, The object of the present invention is to minimize the number of rejected products, increase the production speed, and make the running water work smoothly and automatically.

本発明が提供する手段としては、製造工程の第一工程として、コイル状の円柱状の線材を自動式に圧延機で両翼を保持する線状にしてから、第二工程の切断工程に送入する。翼つき材料の中央部は直径がやや大きい円柱に、又、その両側面は長方形の翼形にする。   As a means provided by the present invention, as a first step of the manufacturing process, a coiled cylindrical wire is automatically formed into a linear shape that holds both blades with a rolling mill, and then sent to the cutting step of the second step. To do. The center of the winged material is a cylinder with a slightly larger diameter, and both sides are rectangular wings.

第二工程の切断工程は、切断型とカムで作動される鋏を持つ切断機で以って前記翼状線材を個別の翼つき材料に切断する。
第三工程として、第二工程を完了した個別翼つき材料を整形型の中に入れ込み、粗雑で不平坦な両切断面を修整して平坦にする。
In the second cutting step, the winged wire is cut into individual winged materials with a cutting machine having a cutting die and a cam operated by a cam.
As a third step, the individual bladed material that has completed the second step is put into a shaping mold, and both rough and uneven flat cut surfaces are modified and flattened.

第四工程として、第三工程を完了した個別翼つき材料にプレスで中央部の円形部の相対両側面に二個の対称的な開き口が底部よりやや大きい凹みを形成させる。
第五工程として、第四工程を完了した個別翼つき材料の二個の凹みの底部をプレスで取り除いて貫通孔を成形させる。
As a fourth step, the material with individual blades that has completed the third step is pressed to form a dent having two symmetrical openings on the opposite side surfaces of the circular portion at the central portion that is slightly larger than the bottom portion.
As a fifth step, the bottoms of the two dents of the individual winged material that have completed the fourth step are removed with a press to form a through hole.

次に、第六工程として、第五工程を完了した個別翼つき材料を可動上型と固定下型でプレスして、両側の翼部を上に湾曲させて蝶形に形成する。
次に、第七工程を完了した個別蝶つき材料の中央の貫通穴に雌ねじを切れば、本発明の蝶形ねじの製造方法の全部の工程を完了し、個別蝶つき材料は完成した蝶形ねじになる。
本発明の蝶形ねじの製造方法は、材料を加熱せずに自動的に流水作業で長い線材から成品に形成するので、生産速度が速く、廃料もごく少なく、不合格品になるものも少ない。
Next, as a sixth step, the individual winged material that has completed the fifth step is pressed with a movable upper die and a fixed lower die, and the wings on both sides are curved upward to form a butterfly shape.
Next, if a female thread is cut in the central through hole of the individual butterfly material that has completed the seventh step, the entire process of the method for manufacturing the butterfly screw of the present invention is completed, and the individual butterfly material is a completed butterfly shape. Become a screw.
The method of manufacturing the butterfly screw of the present invention automatically forms a product from a long wire by running water without heating the material, so that the production speed is high, the waste is very small, and the product becomes a rejected product. Few.

本発明の冷鍛式の蝶形ねじの製造方法の第一実施例は、図1が示す様に、第一工程の圧延と、第二工程の切断と、第三工程の修整と、第四工程の凹み成形と、第五工程の貫通孔形成と、第六工程の蝶部成形と、第七工程のねじ形成の作業とで構成される。   As shown in FIG. 1, the first embodiment of the method for producing a cold forged butterfly screw according to the present invention includes rolling in the first step, cutting in the second step, modification in the third step, and fourth. It consists of the process of forming the recess in the process, forming the through hole in the fifth process, forming the butterfly part in the sixth process, and forming the screw in the seventh process.

第一工程の圧延は、コイル状に巻かれた円柱状の線材料を、コンベアーで自動的に圧延機に送って、材料の中央部に断面の直径がやや大きい円形部と、円形部の相対の両側に断面がやや長方形の二翼部とを形成する翼つき線材に形成する。次に、翼つき線材を次の第二工程に送り込む。   In the first rolling process, a cylindrical wire material wound in a coil shape is automatically sent to a rolling mill by a conveyer, and a circular portion having a slightly larger cross-sectional diameter at the center portion of the material and a relative portion of the circular portion. It is formed into a wire with wings that forms two wings having a slightly rectangular cross section on both sides. Next, the winged wire is fed to the next second step.

第二工程は、第一工程を完了した翼つき線材を切断型と鋏を具備する切断機およびカムで作動される鋏で一個一個の個別翼つき材料に切断する。次に、個別翼つき材料を第三工程に送り込む。   In the second step, the winged wire rod that has completed the first step is cut into individual winged materials one by one with a cutting machine having a cutting die and a scissor and a scissor operated by a cam. Next, the individual winged material is fed into the third step.

第三工程の修整は、第二工程を完了した個別翼つき材料を修整型の中にはめこみ、その粗雑で平らでない両切断面を修整して平滑にしたあと、個別翼つき材料を挟み具1で以って180度回転してから、第四工程に送り込む。   In the modification of the third step, the individual winged material that has completed the second step is inserted into the modified mold, both rough and non-planar cut surfaces are modified and smoothed, and then the individual winged material is sandwiched 1 Thus, after rotating 180 degrees, it is sent to the fourth step.

第四工程の圧縮凹み形成は、第三工程を完了した挟み具1に挟まれている個別翼つき材料を圧縮型の中に入れ込み、その中で個別翼つき材料の中央部の円形部の上側面と下側面を圧縮して各一個の凹みを対称的に形成させるが、この凹みは開き口を底部よりやや大きくしておく。次に、挟み具2で以って二個の凹みを持つ個別翼つき材料を挟んで、180度回転させてから、第五工程に送り込む。   In the fourth step, the compression dent is formed by putting the individual winged material sandwiched between the sandwiching tools 1 that has completed the third step into a compression mold, and in the middle of the circular portion at the center of the individual winged material. The side surface and the lower side surface are compressed to form each one dent symmetrically, but this dent keeps the opening slightly larger than the bottom. Next, the material with the individual wings having the two dents is sandwiched by the sandwiching tool 2 and rotated by 180 degrees before being fed into the fifth step.

第五工程の貫通孔形成は、第四工程を完了した二つの凹みを持つ個別翼つき材料の二個の凹みの底部を除去して貫通孔を形成させて、挟み具3で挟んで、第六工程に送り込む。
第六工程の蝶部形成は、第五工程を完了した貫通孔を持つ個別翼つき材料を図5が示す可動上型5と固定下型6との間に入れて置き、可動上型5を下方の固定下型6に押し下して、個別翼つき材料の両側にある翼部を上向きに湾曲させて、蝶形に形成させ、可動上型5を又上に引きあげてから、個別蝶つき材料を挟み具4で挟み取って、第七工程に送り込む。
In the fifth step, the through hole is formed by removing the bottoms of the two dents of the individual winged material having two dents that have completed the fourth step, forming the through hole, Send in six steps.
In the sixth step, the butterfly portion is formed by placing the individual winged material having a through hole that has completed the fifth step between the movable upper die 5 and the fixed lower die 6 shown in FIG. Push down on the lower fixed lower mold 6 to bend the wings on both sides of the individual winged material upward to form a butterfly shape, and pull up the movable upper mold 5 again. The material is pinched by the pinching tool 4 and sent to the seventh step.

第七工程のねじ切りは、第六工程を完了した個別蝶つき材料をねじ切り機に送り、中央の貫通穴に雌ねじを切れば、本実施例の製造方法により完成される蝶形ねじの成品となる。   The threading of the seventh step is the product of the butterfly screw that is completed by the manufacturing method of this embodiment if the individual butterfly material that has completed the sixth step is sent to the threading machine and the internal thread is cut in the central through hole. .

次に、図6、図7および図8は、本発明の製造方法の第二実施例を示し、上述の第一実施例の第三工程の修整と第四工程の圧縮凹み成形との間に更にはめ溝成形の第三の工程を増加している。それで、第三工程を完了した個別翼つき材料は、挟み具1で挟み取って、180度回転されたあと、第三の工程のはめ溝成形に送り込まれる。この工程では、はめ溝型に個別翼つき材料を入れて、中央部の一側に開き口が底部よりやや大きい凹みと反対側に錐形はめ溝を圧縮形成させてから、挟み具2で以って個別翼つき材料を挟み取り、180度回転させてから、第四工程の圧縮凹み形成に送り込む。第四工程では、第三工程を完了した個別翼つき材料を圧縮型の中に入れておき、錐形はめ溝をプレスして階段付はめ溝を成形してから、挟み具(図8が示す)で挟み取り、更に180度に回転させてから、第五工程に送り込む。第五工程以後は上述の第一実施例の工程と同じである。   Next, FIG. 6, FIG. 7 and FIG. 8 show a second embodiment of the manufacturing method of the present invention, between the modification of the third step of the first embodiment and the compression dent molding of the fourth step. Furthermore, the third step of fitting groove forming is increased. Therefore, the individual bladed material that has completed the third step is pinched by the pinch 1 and rotated 180 degrees, and then fed into the groove forming of the third step. In this step, a material with individual wings is put into the fitting groove mold, and the conical fitting groove is compressed on the side opposite to the recess whose opening is slightly larger than the bottom at one side of the central portion. Then, the material with the individual wings is sandwiched and rotated 180 degrees, and then fed into the compression dent formation in the fourth step. In the fourth step, the individual winged material that has completed the third step is placed in a compression mold, the conical groove is pressed to form a stepped groove, and the pinch (FIG. 8 shows). ), And further rotated 180 degrees before feeding to the fifth step. The fifth and subsequent steps are the same as those in the first embodiment described above.

次に、第二実施例は、第七工程を完了した個別蝶ねじ材料を更に第八工程に送り込む。第八工程は、リベット作業でナイロン片あるいは金属片をリベット机で階段付はめ溝(図7が示す)の中にはめ付けて、低温鬆るみ防止あるいは高温に耐えられかつ鬆るみ防止の蝶形ねじとすることができる。   Next, in the second embodiment, the individual thumbscrew material that has completed the seventh step is further fed to the eighth step. Eighth step is a butterfly shape that prevents cold spots or can withstand high temperatures by fitting nylon pieces or metal pieces into a stepped groove (shown in Fig. 7) with a rivet desk in a rivet operation. It can be a screw.

本発明の冷鍛式成形の蝶形ねじの製造方法は、伝統式の方法より工程が少なく、簡単で生産速度が速くなり、材料も十分使用されて廃材が極めて少なく、生産された成品は不合格率が至極低く、強度が良好で腐触防止性があり、外表面が平滑で使用が便利などの色々な効果がある。   The method of manufacturing a cold forge-shaped butterfly screw of the present invention has fewer steps than the traditional method, is simple and has a high production speed, uses much material, has very little waste, and produces no products. There are various effects such as extremely low acceptance rate, good strength, anticorrosive property, smooth outer surface and convenient use.

本発明の第一実施例による冷鍛式の蝶形ねじの製造方法の流れ作業を示すブロック図である。It is a block diagram which shows the flow operation | work of the manufacturing method of the cold forge type butterfly screw by 1st Example of this invention. 本発明の第一実施例による冷鍛式の蝶形ねじの製造方法の材料を示す断面図である。It is sectional drawing which shows the material of the manufacturing method of the cold forge type butterfly screw by 1st Example of this invention. 本発明の第一実施例による冷鍛式の蝶形ねじの製造方法の材料を示す上面図である。It is a top view which shows the material of the manufacturing method of the cold forge type butterfly screw by 1st Example of this invention. 本発明の第一実施例による冷鍛式の蝶形ねじの製造方法で使用される挟み具の側面図である。It is a side view of the pinch tool used with the manufacturing method of the cold forge type butterfly screw by the first example of the present invention. 本発明の第一実施例による冷鍛式の蝶形ねじの製造方法で使用される蝶型つまみ部をプレスして成形する型を示す側面図である。It is a side view which shows the type | mold which presses and shape | molds the butterfly type | mold knob part used with the manufacturing method of the cold forge type butterfly screw by 1st Example of this invention. 本発明の第二実施例による冷鍛式の蝶形ねじの製造方法の流れ作業を示すブロック図である。It is a block diagram which shows the flow operation | work of the manufacturing method of the cold forge type butterfly screw by 2nd Example of this invention. 本発明の第二実施例による冷鍛式の蝶形ねじの製造方法の材料を示す断面図である。It is sectional drawing which shows the material of the manufacturing method of the cold forge type butterfly screw by 2nd Example of this invention. 本発明の第一実施例による冷鍛式の蝶形ねじの製造方法に使用される挟み具を示す側面図である。It is a side view which shows the pinching tool used for the manufacturing method of the cold forge type butterfly screw by 1st Example of this invention. 従来の製造方法により生産される蝶形ねじの斜視図である。It is a perspective view of the butterfly screw produced by the conventional manufacturing method. 従来の製造方法により生産される他の蝶形ねじの斜視図である。It is a perspective view of the other butterfly screw produced by the conventional manufacturing method.

符号の説明Explanation of symbols

1 挟み具、2 挟み具、3 挟み具、4 挟み具、5 可動式上型、6 固定式下型、21 挟み具   DESCRIPTION OF SYMBOLS 1 Clamp, 2 Clamp, 3 Clamp, 4 Clamp, 5 Movable upper mold, 6 Fixed lower mold, 21 Clamp

Claims (2)

コイル状に巻かれている円形状線材料を自動的に圧延機に送り込み、前記圧延機が前記円形状線材料を断面が長方形の両翼を持つ円形の翼つき材料に圧延する第一過程と、
前記第一過程を完了してから送り込まれる前記翼つき材料を、切断機が具備する切断型と、カムで作動される鋏とで個別の一個一個の個別翼つき材料に切断する第二過程と、
前記第二過程を完了して送り込まれる前記個別翼つき材料を、修整型の中に入れておき、前記個別翼つき材料の粗雑な平滑でない両切断面を平滑に修整して中央部の円形部と両側の長方形の翼を保持する第三過程と、
前記第三過程から送り込まれる前記個別翼つき材料の中央部の両側面にそれぞれ、開き口が底部よりやや大きい凹みをプレスにより形成させる第四過程と、
前記第四過程を完了した前記個別翼つき材料の前記凹みの底部を除去して貫通孔を形成させる第五過程と、
前記第五過程を完了して送り込まれる前記個別翼つき材料を、可動上型と固定下型の中間に置き、前記上型を下に移動させて前記下型の中に前記個別翼つき材料を圧入して、前記個別翼つき材料は両側の翼部を上方に湾曲させて、蝶形に形成させて個別蝶つき材料となる第六過程と、
前記第六過程を完了して送り込まれる前記個別蝶つき材料の中央部の貫通孔にねじ切り機で雌ねじを切る第七過程と、
を含むことを特徴とする冷鍛式の蝶形ねじの製造方法。
A circular wire material wound in a coil shape is automatically fed to a rolling mill, and the rolling mill rolls the circular wire material into a circular winged material having a wing having a rectangular cross section,
A second step of cutting the winged material fed after completion of the first process into individual winged materials by a cutting die provided in a cutting machine and a scissor operated by a cam; ,
The individual winged material to be fed after completion of the second process is placed in a modified mold, and both rough and non-smooth cut surfaces of the individual winged material are smoothly modified to obtain a circular portion at the center. And a third process to hold the rectangular wings on both sides,
A fourth process in which a depression having a slightly larger opening than the bottom is formed by pressing on both side surfaces of the center part of the individual bladed material fed from the third process;
A fifth step of forming a through hole by removing a bottom of the dent of the individually bladed material that has completed the fourth step;
The material with individual wings fed after completion of the fifth process is placed between the movable upper die and the fixed lower die, and the upper die is moved downward to put the material with individual wings into the lower die. The sixth process of press-fitting the individual winged material into a butterfly shape by curving the wings on both sides upward to form an individual butterfly material;
A seventh process of cutting the female thread with a threading machine into the through hole in the center of the individual butterfly material fed in after completing the sixth process;
A method for producing a cold-forged butterfly screw, comprising:
前記第三過程と前記第四過程との間に設けられ、前記個別翼つき材料の中央部の円形部の側面に開き口が底部よりやや大きい凹みをプレスにより形成し、前記中央部の円形部の他側面に錐形のはまり溝をプレスして形成し、更に前記錐形のはまり溝をプレスして階段状のはまり溝を形成させるはまり溝形成の第三過程と、
前記第七過程を完了した蝶形ねじを受け入れて、前記はまり溝の中にナイロン片あるいは金属片をはめ付けて、前記蝶形ねじに低温鬆るみ防止性あるいは高温度に耐えて鬆るみ防止性のある蝶形ねじにする第八過程と、
を更に含むことを特徴とする請求項1記載の冷鍛式の蝶形ねじの製造方法。
Provided between the third process and the fourth process, a depression having a slightly larger opening than the bottom is formed on the side surface of the circular part of the central part of the individual winged material by pressing, and the circular part of the central part Forming a conical groove on the other side surface, and further pressing the conical groove to form a stepped groove;
Receiving the butterfly screw that has completed the seventh process, and fitting a nylon piece or metal piece into the fitting groove to prevent low temperature or high temperature resistance against the butterfly screw. The eighth process of making a butterfly screw with
The method of manufacturing a cold forged butterfly screw according to claim 1, further comprising:
JP2004133319A 2004-04-28 2004-04-28 Cold forging type manufacturing method of butterfly screw Pending JP2005315334A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP2004133319A JP2005315334A (en) 2004-04-28 2004-04-28 Cold forging type manufacturing method of butterfly screw

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2004133319A JP2005315334A (en) 2004-04-28 2004-04-28 Cold forging type manufacturing method of butterfly screw

Publications (1)

Publication Number Publication Date
JP2005315334A true JP2005315334A (en) 2005-11-10

Family

ID=35442976

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2004133319A Pending JP2005315334A (en) 2004-04-28 2004-04-28 Cold forging type manufacturing method of butterfly screw

Country Status (1)

Country Link
JP (1) JP2005315334A (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR100850225B1 (en) 2006-07-27 2008-08-06 박영호 Self-clinching Type Fastener and Manufacturing Method Thereof
CN103042131A (en) * 2013-01-06 2013-04-17 张家港市新艺五金有限公司 Nut production and processing technology and die thereof
CN104439939A (en) * 2014-11-07 2015-03-25 通裕重工股份有限公司 Integrated forming method for large pipe molds
CN109702429A (en) * 2017-10-26 2019-05-03 沈阳黎明国际动力工业有限公司 A kind of odd-shaped cross section cone segmental arc rolling processing process
CN110625343A (en) * 2019-11-06 2019-12-31 广州市通晓越大门业有限公司 Production process of steel door panel
CN114986095A (en) * 2022-06-01 2022-09-02 重庆宏华唯实达汽车部件有限公司 Hole flanging and wire extruding process for sheet metal part

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR100850225B1 (en) 2006-07-27 2008-08-06 박영호 Self-clinching Type Fastener and Manufacturing Method Thereof
CN103042131A (en) * 2013-01-06 2013-04-17 张家港市新艺五金有限公司 Nut production and processing technology and die thereof
CN104439939A (en) * 2014-11-07 2015-03-25 通裕重工股份有限公司 Integrated forming method for large pipe molds
CN109702429A (en) * 2017-10-26 2019-05-03 沈阳黎明国际动力工业有限公司 A kind of odd-shaped cross section cone segmental arc rolling processing process
CN110625343A (en) * 2019-11-06 2019-12-31 广州市通晓越大门业有限公司 Production process of steel door panel
CN114986095A (en) * 2022-06-01 2022-09-02 重庆宏华唯实达汽车部件有限公司 Hole flanging and wire extruding process for sheet metal part

Similar Documents

Publication Publication Date Title
US8176813B2 (en) Methods for manufacturing combination wrenches without generating carbon scale
JP2005315334A (en) Cold forging type manufacturing method of butterfly screw
US6893354B2 (en) Method for manufacturing cold-forged wing nuts
CN101934310B (en) Wrench tool and bend manufacture procedure thereof
CN105537415B (en) Elbow forming blank and pressing forming die thereof
US20110034259A1 (en) Method of making a washer
US2294802A (en) Thumbscrew and method of making same
CN108296298B (en) A kind of cold extruding processing method of coupling yoke
CN1317090C (en) Method for producing cold forging wing-shaped screw nut
CN201448318U (en) Pipe clamp head
CN113102946A (en) Lantern type rivet nut production process
CA3142347A1 (en) Extrusion forming method and forming apparatus for manufacturing self-clinching rivet
TWI590891B (en) High and low teeth of the chassis manufacturing methods
JPH05277619A (en) Washer and production thereof
CN110076525A (en) A kind of production method using cold-heading technology processing and forming high-precision pedal tooth
TWI478779B (en) A method for making a screw
RU2084305C1 (en) Method of making heads of box wrenches with stepped outer surface
CN103962799B (en) A kind of drawing process of workpiece with flange
CN107685116A (en) A kind of one time punching molded device of bolt
KR950007768B1 (en) Washer and method for manufacturing same
CN214263741U (en) Screw forming die
CN117380857A (en) Device for bending clamps with multiple specifications
US20120198906A1 (en) Method for manufacturing cold-forged wing bolts
TWI277467B (en) Manufacturing method of sleeve
US1535553A (en) Method of threading a blank

Legal Events

Date Code Title Description
A977 Report on retrieval

Free format text: JAPANESE INTERMEDIATE CODE: A971007

Effective date: 20060810

A131 Notification of reasons for refusal

Free format text: JAPANESE INTERMEDIATE CODE: A131

Effective date: 20061003

A521 Written amendment

Free format text: JAPANESE INTERMEDIATE CODE: A523

Effective date: 20061211

A02 Decision of refusal

Free format text: JAPANESE INTERMEDIATE CODE: A02

Effective date: 20070424