CN217196807U - Cable extruder clamp - Google Patents
Cable extruder clamp Download PDFInfo
- Publication number
- CN217196807U CN217196807U CN202123313712.3U CN202123313712U CN217196807U CN 217196807 U CN217196807 U CN 217196807U CN 202123313712 U CN202123313712 U CN 202123313712U CN 217196807 U CN217196807 U CN 217196807U
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- groove
- section arc
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Abstract
The utility model discloses a cable extruder anchor clamps, press from both sides the groove including the middle section arc, the middle section arc presss from both sides that groove left end articulates there is left section arc to press from both sides the groove, the middle section arc presss from both sides the groove right-hand member and articulates there is right section arc to press from both sides the groove, left side section arc presss from both sides the groove end and right section arc presss from both sides the groove end and passes through retaining member activity lock, left side section arc presss from both sides the inboard in groove, middle section arc clamp groove and right section arc clamp groove and constitutes annular (holding) chuck, annular (holding) chuck is connected with linear motion mechanism. The utility model discloses a linear motion mechanism makes anchor clamps be close to or keep away from aircraft nose and fuselage junction, replaces the manual work to lift up the action, reduces anchor clamps handheld time, avoids scalding safe and reliable.
Description
Technical Field
The utility model relates to a cable extruder anchor clamps belongs to cable manufacture equipment field.
Background
In order to ensure the safety of electric conduction and prevent signal leakage or attenuation, the insulating layer coated on the wire core is necessary. In the production process of the cable, the insulation layer is generally heated and melted by an extruder, and then a material flow is extruded into a machine head through an extruder screw, and is molded and coated on the surface of the wire core through a proper mold under the pressure of the extruder screw. In the process, due to the requirements of different materials or different colors, the die needs to be disassembled and assembled, and the honeycomb plate needs to be cleaned and replaced, so that the purpose of replacing the materials is achieved. The machine head and the machine body of the extruder are generally fixedly connected through a machine clamp, the honeycomb plate is positioned in a flange plate at the joint of the machine head and the machine body, and the machine clamp is locked and clamped on the flange plate.
For example, the wire extruder clamp disclosed in the publication No. CN 204706398U requires manual lifting and locking of the two-piece clamp at the joint of the machine head and the machine body during the actual use process. Because of the aircraft nose temperature is higher, lead to the machine to press from both sides the temperature and scald the hand equally high temperature, and machine presss from both sides self weight great, at the dismouting in-process, not only waste time and energy, also have scald operator's potential safety hazard.
SUMMERY OF THE UTILITY MODEL
The utility model aims at providing a rational in infrastructure, the security is high, and easy and simple to handle's cable extruder anchor clamps.
In order to achieve the technical purpose, the technical scheme of the utility model is that:
cable extruder anchor clamps, including middle section arc double-layered groove, middle section arc double-layered groove left end articulates there is left section arc double-layered groove, middle section arc double-layered groove right-hand member articulates there is right section arc double-layered groove, left side section arc double-layered groove end and right side section arc double-layered groove end pass through retaining member activity lock, the inboard that left side section arc double-layered groove, middle section arc double-layered groove and right side section arc double-layered groove constitutes annular (holding) chuck, annular (holding) chuck is connected with linear motion mechanism, linear motion mechanism is used for annular (holding) chuck along straight reciprocating motion, makes annular (holding) chuck be close to or keep away from aircraft nose and fuselage junction.
When the clamping device is used, the locking part is detached, the left section arc-shaped clamping groove and the right section arc-shaped clamping groove are separated, the linear motion mechanism drives the clamp to move to the joint of the machine head and the machine body, the left section arc-shaped clamping groove, the middle section arc-shaped clamping groove and the right section arc-shaped clamping groove are closed, the left section arc-shaped clamping groove, the middle section arc-shaped clamping groove and the right section arc-shaped clamping groove are attached to the machine head and the machine body, and the machine head and the machine body are locked and fixed through the locking part and then fixedly connected; when dismantling anchor clamps, dismantle the retaining member, separation left side section arc presss from both sides groove and right side section arc and presss from both sides the groove, and linear motion mechanism drive anchor clamps are kept away from aircraft nose and fuselage junction to dismouting mould, clearance change honeycomb panel.
Preferably, the linear motion mechanism is fixedly connected with the middle arc-shaped clamping groove.
Preferably, the linear motion mechanism is a cylinder.
The linear motion mechanism is connected with a base and drives the annular chuck to be far away from or close to the base.
In order to facilitate the position adjustment, the locking piece is convenient for to connect the annular chuck, and in the annular chuck outside, left side section arc presss from both sides the groove and right side section arc presss from both sides the groove and all is provided with the push rod.
The locking piece is including setting up the bolt groove at left section arc double-layered groove end, the bolt groove is connected with locking screw through the bolt axle, locking screw has the bolt hole that supplies the bolt axle to pass through, locking screw threaded connection has lock nut, right section arc presss from both sides groove end and is provided with the U type groove that supplies locking screw to pass through, U type groove one side is provided with the draw-in groove of cooperation lock nut locking annular (holding) chuck.
Specifically, locking screw one end is through bolt axle swing joint plug pin groove, and locking nut is connected to the locking screw other end, and locking screw card goes into U type groove, and locking nut installs in draw-in groove department, through screwing locking nut, makes left section arc press from both sides the groove and press from both sides tightly with right section arc clamp groove, and then makes the locking of annular (holding) chuck.
And a locking pressing sleeve is sleeved on the locking screw rod between the U-shaped groove and the locking nut.
The utility model discloses a linear motion mechanism makes anchor clamps be close to or keep away from aircraft nose and fuselage junction, replaces the manual work to lift up the action, reduces anchor clamps handheld time, avoids scalding safe and reliable.
Drawings
The present invention will be described in further detail with reference to the accompanying drawings and specific embodiments.
Fig. 1 is a schematic structural diagram of the present invention.
Fig. 2 is the structural schematic diagram of the locking state of the present invention.
Detailed Description
As shown in fig. 1-2, cable extruder anchor clamps, including middle section arc clamp groove 11, middle section arc clamp groove 11 left end articulates there is left section arc clamp groove 12, middle section arc clamp groove 11 right-hand member articulates there is right section arc clamp groove 13, left side section arc clamp groove 12 is terminal to be pressed from both sides the groove 13 end through retaining member activity lock with right section arc, left side section arc clamp groove 12, middle section arc clamp groove 11 and the inboard of right section arc clamp groove 13 constitute annular (holding) chuck, middle section arc clamp groove 11 is connected with linear motion mechanism 21, linear motion mechanism 21 is connected with base 22, linear motion mechanism 21 is the cylinder, and cylinder drive middle section arc clamp groove 11 is pressed from both sides the aircraft nose and the fuselage junction (keeps away from or is close to the base) or keep away from aircraft nose and fuselage junction (keep away from or be close to).
The locking piece is including setting up the bolt groove at left section arc presss from both sides 12 end, bolt groove passes through bolt axle 31 swing joint locking screw 32, locking screw 32 has the bolt hole that supplies bolt axle 31 to pass through, locking screw 32 end threaded connection has lock nut 33, right side section arc presss from both sides 13 end and is provided with the U type groove 34 that supplies locking screw 32 to pass through, and locking screw 32 can rotate around bolt axle 31 and block into the U type inslot, also can rotate around bolt axle 31 and break away from U type groove 34, U type groove 34 one side is provided with the draw-in groove 35 that cooperates lock nut 33 locking ring chuck, and draw-in groove 35 is spacing to lock nut 33, makes left section arc press from both sides groove 12 and right section arc and presss from both sides the groove 13 and presss from both sides tightly, and then makes ring chuck locking, between U type groove 34 and lock nut 33, locking press the cover 36 has been cup jointed on the locking screw 32.
And push rods are arranged on the outer side of the annular chuck, and the left section arc-shaped clamping groove 12 and the right section arc-shaped clamping groove 13 are respectively provided with a push rod.
When in use, the locking nut 33 is rotated to enable the locking screw 32 to rotate around the bolt shaft 31 to be separated from the U-shaped groove 34; when the locking screw 32 is separated from the U-shaped groove 34, the push rod is pushed, and the left section arc-shaped clamping groove 12 and the right section arc-shaped clamping groove 13 are opened towards two sides; after the left section arc-shaped clamping groove 12 and the right section arc-shaped clamping groove 13 are opened towards two sides, the cylinder drives the middle section arc-shaped clamping groove 11 to be close to the connection part of the machine head and the machine body, so that the middle section arc-shaped clamping groove 11 is close to the machine head and the machine body; after the middle section arc-shaped clamping groove 11 is closed, the push rod is pushed, so that the left section arc-shaped clamping groove 12 and the right section arc-shaped clamping groove 13 are closed and close to the connection part of the machine head and the machine body; after the left arc-shaped clamping groove 12 and the right arc-shaped clamping groove 13 are closed and close to each other, the locking screw 32 is clamped into the U-shaped groove 34; after the locking screw 32 is clamped into the U-shaped groove 34, the locking nut 33 is rotated to clamp the left arc-shaped clamping groove 12, the right arc-shaped clamping groove 13 and the middle arc-shaped clamping groove 11, thereby fixedly connecting the machine head and the machine body.
When the clamp needs to be disassembled, all parts are disassembled in sequence.
This embodiment makes anchor clamps be close to or keep away from aircraft nose and fuselage junction through the cylinder, replaces the manual work to lift up the action, reduces anchor clamps handheld time, avoids scalding safe and reliable.
The above-mentioned embodiment does not limit the utility model in any way, and all the technical solutions that adopt the mode of equivalent replacement or equivalent transform to obtain all fall within the protection scope of the utility model.
Claims (7)
1. Cable extruder anchor clamps, its characterized in that: including middle section arc clamp groove, middle section arc clamp groove left end articulates there is left section arc clamp groove, middle section arc clamp groove right-hand member articulates there is right section arc clamp groove, left side section arc clamp groove end and right side section arc clamp groove end pass through retaining member activity lock, the inboard that left side section arc clamp groove, middle section arc clamp groove and right side section arc clamp groove constitutes annular (holding) chuck, annular (holding) chuck is connected with linear motion mechanism.
2. The cable extruder clamp of claim 1, wherein: the linear motion mechanism is fixedly connected with the middle arc-shaped clamping groove.
3. The cable extruder clamp of claim 1, wherein: the linear motion mechanism is a cylinder.
4. The cable extruder clamp of claim 1, wherein: the linear motion mechanism is connected with a base.
5. The cable extruder clamp of claim 1, wherein: and push rods are arranged on the left section arc-shaped clamping groove and the right section arc-shaped clamping groove on the outer side of the annular chuck.
6. The cable extruder clamp of claim 1, wherein: the locking piece is including setting up the bolt groove at left section arc double-layered groove end, the bolt groove is connected with locking screw through the bolt axle, locking screw has the bolt hole that supplies the bolt axle to pass through, locking screw threaded connection has lock nut, right section arc presss from both sides groove end and is provided with the U type groove that supplies locking screw to pass through, U type groove one side is provided with the draw-in groove of cooperation lock nut locking annular (holding) chuck.
7. The cable extruder clamp of claim 6, wherein: and a locking pressing sleeve is sleeved on the locking screw rod between the U-shaped groove and the locking nut.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202123313712.3U CN217196807U (en) | 2021-12-27 | 2021-12-27 | Cable extruder clamp |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202123313712.3U CN217196807U (en) | 2021-12-27 | 2021-12-27 | Cable extruder clamp |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN217196807U true CN217196807U (en) | 2022-08-16 |
Family
ID=82784906
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202123313712.3U Active CN217196807U (en) | 2021-12-27 | 2021-12-27 | Cable extruder clamp |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN217196807U (en) |
-
2021
- 2021-12-27 CN CN202123313712.3U patent/CN217196807U/en active Active
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| GR01 | Patent grant |