JP2013162995A - Partition type fastener slider - Google Patents

Abstract

PROBLEM TO BE SOLVED: To provide a slider which can be easily removed and replaced without using another tool even when a fabric is rolled in the slider since a fabric is not easily removed when being erroneously rolled in the slider when a fastener is closed and also the slider alone cannot be easily removed, so that it is hard for an individual to replace the slider.SOLUTION: A fastener slider is configured in such a way that the fastener slider is assembled and completed by separating a trunk body, arranging a key shape hook at an upper end of a column support, inserting the hook into an upper side trunk body and fixing the hook. Thus, the trunk body is separated again as necessary thereby to easily remove a bitten fabric without using another tool, and the slide itself can be attached/detached to/from an element.

Description

  The present invention relates to a split fastener slider.

In the past, when clothes cloth was wrapped around a zipper slider, you had to struggle to lower the slider carefully while opening the cloth left and right with your fingers. There were inconveniences such as hurting.
Also, it took a lot of work to replace only the slider, and those who did not have the technology needed to replace the entire fastener.
In addition, a split type slider that is fixed to the column part through a screw from the back side is known, but this is intended to eliminate the inconvenience when sewing the fastener on the clothes, and it can be easily removed whenever necessary. This is not intended (see Patent Document 1).

Japanese Patent Publication No. 7-100007

When closing the zipper, if the cloth of the clothes is accidentally caught in the slider, it cannot be easily removed. There is a tendency to tear the dough forcibly and damage the slider itself.
This is also not easy when only the slider is to be replaced.
The present invention is intended to solve the above problems without any other tools.

A fastener slider comprising an upper body and a lower body.
The upper part of the fuselage is parallel to the fuselage upper top plate and the fuselage upper fixed plate facing each other with a certain space in parallel, and the upper part of the fuselage upper side wall is formed around the entire periphery. Department is installed. A knob shaft hole is provided in the upper body top plate. The fuselage upper fixed platen is provided with a support post fixing portion, and a hook through hole is provided at substantially the center of the support post fixing portion. Out of the four sides of the fuselage upper fixed platen, shallower fuselage upper rails are formed only on the left and right sides, and project toward the lower fuselage.
The rotation lock part is installed so that the knob mounting plate and the hook receiving plate face each other in parallel with a certain distance, and both are integrally connected by two shafts, a stopper shaft that is too closed and a stopper shaft that is opened too much. A hook insertion slot is provided at the center of the panel, and a knob shaft is attached to the outside of the knob mounting panel as viewed from the hook receiving panel. The knob shaft is formed so as to protrude from the knob shaft hole of the upper body top plate, and the knob extends in one direction substantially perpendicular to the protruding knob shaft.
The lower part of the fuselage has four sides of the lower part of the lower part of the fuselage. And a hook is formed from the hook shaft substantially perpendicular to the shaft. The hook shaft and the hook are formed so as to pass through the hook through hole of the column fixing portion at the upper part of the body, protrude the hook insertion port of the hook receiving panel, and ground the knob mounting plate responsively to the knob shaft. .
As a whole, the upper part of the fuselage and the lower part of the fuselage formed in this way are combined, and the rotation lock part is opened and closed by the knob, so that the fastener slider is divided when necessary.
This is a split fastener slider characterized by the above.

Even if the fabric is involved when closing the zipper, it can be easily removed without tools.
Since only the slider can be easily exchanged without tools, you can replace it yourself when you find a slider of your favorite design.

The perspective view which visualized the internal structure by making the upper part of the body which is a part of the present invention transparent The perspective view of the fuselage lower part which is a part of this invention The perspective view of the fuselage upper fixed platen which is a part of the present invention The perspective view of the rotation lock part which is a part of this invention Sectional drawing seen from the front which shows the state before closing the knob of this invention Sectional drawing seen from the side which shows the state after closing the knob of this invention

Embodiments of the present invention will be described below.
(B) The knob shaft (5) connected to the rotation lock portion (3) passes through the knob shaft hole (7) formed in the top plate (6) of the upper body (1), and the knob (4) is displayed. The column fixing part (10) is provided on the upper fuselage fixing plate (9). A hook through hole (11) is opened at substantially the center of the column fixing portion (10). The fuselage upper top plate (6) and the fuselage upper fixed platen (9) face each other in parallel at regular intervals, and are provided with a fuselage upper side wall (8) that joins them along the edges and surrounds the entire circumference. It has been. A shallow fuselage upper rail (12) is formed only on the left and right sides of the four sides of the fuselage upper fixed platen (9) and protrudes toward the fuselage lower part (2).
(B) A key-like hook (21) and a hook shaft (22) are provided on the upper end of the support (20) installed in the lower body (2). A shallow fuselage lower rail (19) is provided only on the left and right sides of the four sides of the fuselage lower bottom plate (18).
(C) The rotation lock portion (3) is installed between the fuselage upper top plate (6) and the fuselage upper fixed platen (9). A knob shaft (5) that rotates with the knob (4) is attached to the knob mounting board (13), and a hook insertion port (17) is opened in the hook receiving board (14) to restrict the movement of the hook (21). An over-closed stopper (15) and an over-open stopper (16) are provided.
The present invention has the above structure.
When using the present invention, as shown in FIG. 1, the knob is turned counterclockwise to rotate the rotation lock portion (3), and the hook (21) is rotated too far until it hits the stopper (16) and stops. Align (17) with hook (21). If the knob shaft (5) is picked up as it is, the upper part of the fuselage (1) and the lower part of the fuselage (2) are separated.
Reverse this procedure when reassembling. That is, with the knob fully opened, the upper body (1) and the lower body (2) are aligned, the hook (21) is inserted into the hook insertion port (17), the knob (4) is turned clockwise, and the hook ( 21) Rotate the rotation lock (3) until it is closed too much and hits the stopper (15).
This is fundamentally different from Patent Document 1 in that all operations can be performed without tools.

  1 Upper body, 2 Lower body, 3 Rotation lock, 4 Knob, 5 Knob shaft, 6 Upper body top plate, 7 Knob shaft hole, 8 Upper body side wall, 9 Upper body fixing plate, 10 Post fixing portion, 11 Hook through Mouth, 12 Body upper rail, 13 Knob mounting panel, 14 Hook receiving panel, 15 Over-closed stopper shaft, 16 Over-opened stopper shaft, 17 Hook insertion port, 18 Body lower bottom plate, 19 Body lower rail, 20 Post, 21 Hook , 22 Hook shaft

Claims (1)

  Fastener slider consisting of upper fuselage and lower fuselage, upper fuselage upper plate and fuselage upper fixed plate facing each other in parallel with a certain space. A fuselage upper side wall is formed, a rotation lock part is installed therein, a knob shaft hole is provided in the fuselage upper top plate, a pillar fixing part is provided in the fuselage upper fixing plate, There is a hook hole in the center, and a shallow fuselage rail is formed only on the left and right sides of the four sides of the fuselage upper fixed plate, protruding toward the fuselage lower part. The receiving board is installed parallel to each other with a certain distance between them, and they are joined together by two shafts, the over-closed stopper shaft and the open stopper shaft, inside the hook receiving plate. Is provided with a hook insertion port, and a knob shaft is attached to the outside of the knob receiving panel as viewed from the hook receiving panel, and this knob shaft is formed in a shape protruding from the knob shaft hole of the upper body top plate, A knob extends in one direction almost perpendicular to the protruding knob shaft, and the fuselage lower part has shallow fuselage lower rails formed only on the opposite sides of the four sides of the fuselage lower bottom plate, and the inner surface of the fuselage lower bottom plate The hook shaft stands on the surface opposite to the bottom plate side of the column, and the hook is formed at a right angle from the hook shaft to the shaft. The hook shaft and the hook are hooks of the column fixing part at the top of the fuselage. The upper part of the fuselage and the lower part of the fuselage formed in this way are formed so as to pass through the through hole, protrude the hook insertion port of the hook receiving board, and ground the knob mounting plate responsively to the knob shaft. Combined with By rotating the locking unit is opened and closed by a knob, split fastener slider wherein the zipper slider is divided when necessary.

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