A 4.3KV high voltage test device

Abstract

The present invention relates to the technical field of machine tool loading, and specifically to a 4.3KV high-voltage test device for switches. It comprises a sliding rod, on which a sliding part is provided, on which a fixing part is provided, on which a guide rail is provided, on which the fixing part slides; a straight plate, symmetrically arranged on the fixing part, the straight plate and the fixing part are arranged vertically, on which a rotating part is provided, a clamping straight plate is connected between the two rotating parts, and clamping claws are respectively provided on both sides of the clamping straight plate, which are used to push small airplane parts to a specified position for limited fixing; a driving part, which is arranged on any straight plate, and the driving part is connected to any rotating part; a probe detection assembly, which is arranged on one side of the clamping claw, and is used to detect small airplane parts. The position of the entire small airplane part is adjusted by the sliding part, and the driving part drives the adjustment clamping claw to fix it, and finally the probe detection assembly is used for detection, so that the fixed detection is more time-saving and labor-saving.

Description

Technical Field

[0001] The invention relates to the technical field of machine tool loading, and in particular to a 4.3KV high voltage testing device. Background Art

[0002] The loading and unloading device of a machine tool is an automatic or semi-automatic mechanical device that delivers the workpiece to be processed to the processing position on the machine tool and removes the processed workpiece from the processing position. It is also called an automatic workpiece loading and unloading device. The clamp is an important structure for realizing loading and unloading. The manipulator clamp is in the middle process of the double-arm manipulator automatic line, and is mainly used to load and unload the machine tool. This part is a key structure and determines the execution effect of loading and unloading the machine tool. The loading and unloading of the machine tool requires safety, stability and precision, and has corresponding structures to realize its functions.

[0003] In the prior art, the small airplane parts are fixed in position, and then the small airplane parts are probed for circuit conduction. In the process of limiting and fixing the small airplane, the small airplane parts at the specified positions are tested during the probe test, and the two parts of the small airplane need to be manually fixed in position, making the entire testing process time-consuming and labor-intensive. Summary of the invention

[0004] Therefore, the technical problem to be solved by the present invention is to overcome the defect in the prior art that manual operation is performed during the probe detection process and during the process of fixing the limit plane, making the entire detection process time-consuming and labor-intensive, thereby providing a 4.3KV high-voltage testing device.

[0005] In order to solve the above problems, a 4.3KV high-voltage testing device is provided, including a sliding rod, a sliding piece is provided on the sliding piece, a fixing piece is provided on the sliding piece, a guide rail is provided on the sliding piece, and the fixing piece slides on the guide rail; a straight plate is symmetrically arranged on the fixing piece, the straight plate is vertically arranged to the fixing piece, a rotating piece is provided on the straight plate, a clamping straight plate is connected between the two rotating pieces, and clamping claw assemblies are respectively provided on both sides of the clamping claw straight plate, which are used to push the small aircraft parts to the specified position for limited fixing; a driving piece is arranged on any straight plate, the driving piece is connected to the rotating piece, and is used to drive the rotating piece to rotate and adjust; a probe detection assembly is arranged on one side of the clamping claw assembly, and is used to detect the small aircraft parts.

[0006] The clamping jaw assembly comprises a limiting member, which is fixed on a clamping jaw straight plate. A clamping jaw is arranged on the limiting member, the cross section of the clamping jaw is U-shaped, and an abutting member is arranged on the clamping jaw.

[0007] A fixing frame is provided on one side of the fixing member, a carrier block is provided on the upper end of the fixing frame, and a lifting and positioning device is provided in the inner cavity of the fixing frame.

[0008] Dual-station carriers are provided on both sides of the carrier block, and the dual-station carrier includes a limit frame, which is arranged on a side away from the carrier block, a limit rod is provided through the limit frame, a limit block is provided at one end of the fixed frame, and the limit rod is fixed to the limit block.

[0009] The lifting and positioning device includes a sliding frame, which is located in the fixed frame. A second guide rail is provided on the inner side of the fixed frame, and a second guide block is provided relative to the limit frame. A fixing bolt is provided at the upper end of the sliding frame, which is fixed with a fixing hole and a fixing pin at the lower end relative to the carrier block. A cylinder is provided on the fixed frame, and a piston rod of the cylinder is fixedly connected to the sliding frame.

[0010] The technical solution of the present invention has the following advantages:

[0011] 1. A 4.3KV high-voltage testing device provided by the present invention comprises straight plates symmetrically arranged on a fixing part, a rotating part arranged on the straight plates, a clamping straight plate arranged between the two rotating parts, the clamping straight plate connected to the rotating part so that the clamping straight plate can be rotated and adjusted by the rotating part, the driving part drives the rotating part to rotate so that the adjustment is faster, clamping claw assemblies are respectively arranged on both sides of the clamping straight plate for limiting and fixing the small aircraft parts to the specified position, and finally the probe detection assembly is used for detection, which saves time and effort.

[0012] 2. The present invention provides a 4.3KV high-voltage testing device, in which a fixing bolt is arranged at the upper end of a sliding frame, and a fixing hole and a fixing pin are arranged at the lower end of a carrier block for fixing. When the components are clamped onto the carrier block, the fixing bolt slides upward to the fixing hole and the fixing pin for sliding fixation. A cylinder is arranged on the fixing frame, and a piston rod of the cylinder is fixedly connected to the sliding frame, thereby providing kinetic energy for the fixing frame and realizing rapid sliding fixation of the fixing frame.

[0013] 3. The present invention provides a 4.3KV high-voltage testing device, in which a lifting and positioning device is used to adjust the sliding movement of parts arranged on a carrier block in a vertical direction. After the parts are adjusted to a specified position, the parts are fixed to the carrier block through the lifting and positioning device. A double-station carrier is arranged on one side of the carrier block, and the double-station carrier further limits and fixes the parts, making the adjustment and fixation more convenient. BRIEF DESCRIPTION OF THE DRAWINGS

[0014] In order to more clearly illustrate the specific implementation methods of the present invention or the technical solutions in the prior art, the drawings required for use in the specific implementation methods or the description of the prior art will be briefly introduced below. Obviously, the drawings described below are some implementation methods of the present invention. For ordinary technicians in this field, other drawings can be obtained based on these drawings without paying creative work.

[0015] Figure 1 A partial structural schematic diagram of a 4.3KV high voltage test device;

[0016] Figure 2 The overall structural diagram provided for a 4.3KV high voltage test device;

[0017] Figure 3 A schematic diagram of the lifting and positioning structure provided for a 4.3KV high-voltage test device.

[0018] Description of reference numerals:

[0019] 1-sliding rod; 11-sliding member; 12-fixing member; 121-fixing frame; 122-carrier block; 13-guide rail; 15-straight plate; 16-rotating member; 17-clamping straight plate; 18-driving member; 2-clamping jaw assembly; 21-limiting member; 22-clamping jaw; 23-abutting member; 3-lifting and positioning device; 31-sliding frame; 32-second guide rail; 33-second guide block; 34-fixing bolt; 35-fixing hole; 36-cylinder; 4-double-station carrier; 41-limiting frame; 42-limiting rod; 43-limiting block. DETAILED DESCRIPTION

[0020] The technical solution of the present invention will be described clearly and completely below in conjunction with the accompanying drawings. Obviously, the described embodiments are only part of the embodiments of the present invention, not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the present invention.

[0021] A 4.3KV high voltage test device, such as Figure 1 As shown, it includes a sliding rod 1, a sliding member 11 is arranged on the sliding rod 1, so that the sliding member 11 can be adjusted on the sliding rod 1, a fixing member 12 is arranged on the sliding member 11, and a guide rail 13 is arranged on the sliding member 11, and the fixing member 12 slides on the guide rail 13, so that the sliding member 11 is fine-tuned, so that the assembly is more convenient and accurate; straight plates 15 are symmetrically arranged on the fixing member 12, and the straight plates 15 are perpendicular to the fixing member 12, and a rotating member 16 is arranged on the straight plate 15, and a clamping claw straight plate 17 is arranged between the two rotating members 16, and the clamping claw straight plate 17 is connected to the rotating member 16, so that the clamping claw straight plate 17 can be rotated and adjusted by the rotating member 16, and clamping claw assemblies 2 are respectively arranged on both sides of the clamping claw straight plate 17, which are used to limit and fix the small aircraft parts to the specified position for limit fixation.

[0022] like Figure 1 and Figure 2 As shown, a driving member 18 is provided on any straight plate 15, and the driving member 18 is connected to the rotating member 16. The rotating member 16 is driven to rotate by the driving member 18, so that the adjustment is more convenient. At the same time, a probe detection component 19 is provided on one side of the clamp 22 to detect the small aircraft parts.

[0023] like Figure 1 and Figure 2 As shown, the clamping jaw assembly 2 includes a limiting member 21, which is fixed on a limiting straight plate. A clamping jaw 22 is arranged on the limiting member 21, and the clamping jaw 22 is fixed on the limiting member 21 by adjusting bolts. The cross section of the clamping jaw 22 is U-shaped, so that the clamping jaw 22 can clamp and fix the small aircraft parts. An abutting member 23 is arranged on the clamping jaw 22, and the abutting member 23 abuts against the parts, so that the clamping jaw 22 is fixed more firmly.

[0024] like Figure 3 As shown, a fixing frame 121 is arranged on one side of the fixing member 12, and the upper end of the fixing frame 121 is arranged on a carrier block 122, and small aircraft parts are placed on the carrier block 122. A lifting and positioning device 3 is arranged in the inner cavity of the fixing frame 121, and the small aircraft parts located on the carrier block 122 are adjusted by the lifting and positioning device 3, and are adjusted and fixed in the vertical direction, making the adjustment more convenient.

[0025] like Figure 3 As shown, a double-station carrier 4 is provided on either side of the carrier block 122, and the double-station carrier 4 includes a limit frame 41, a limit rod 42 is set through the limit frame 41, and a limit block 43 is set at one end of the fixed frame 121, and the limit rod 42 and the limit block 43 are fixedly arranged, wherein the limit rod 42 plays a guiding role to adjust the small aircraft parts, so that the parts are more convenient to adjust in the horizontal direction.

[0026] like Figure 3 As shown, the lifting and positioning device 3 includes a sliding frame 31, which is located in the fixed frame 121. A second guide rail 32 is arranged on the inner side of the fixed frame 121, and a second guide block 33 is arranged on the fixed frame 121, so that the sliding frame 31 slides at a specified position in the fixed frame 121. A fixing bolt 34 is arranged on the upper end of the sliding frame 31, and a fixing hole 35 is arranged on the lower end relative to the carrier block 122 for fixing with a pin. When the parts are clamped to the carrier block 122, the fixing bolt 34 slides upward to the fixing hole 35 for fixing with a pin for sliding. A cylinder 36 is arranged on the fixed frame 121, and a piston rod of the cylinder 36 is fixedly connected to the sliding frame 31 to provide kinetic energy for the fixed frame 121, thereby realizing rapid sliding and fixing of the fixed frame 121.

[0027] Working principle: The sliding member 11 adjusts the limit fixing device on the sliding rod 1 to the specified position, the driving member 18 drives the clamping jaw straight plate 17, adjusts the selection clamping jaw 22, and adjusts and fixes the vertical position of the small aircraft parts set on the carrier block 122 through the jacking positioning device 3, and then slides the small aircraft parts in the horizontal position through the double-station carrier 4, and finally detects them through the probe detection component 19.

[0028] In addition, the technical features involved in the different embodiments of the present invention described above can be combined with each other as long as they do not conflict with each other.

Claims

1. A 4.3KV high voltage test device, characterized in that: include: A sliding rod (1), wherein the sliding rod (1) is provided with a sliding member (11), the sliding member (11) is provided with a fixing member (12), the sliding member (11) is provided with a guide rail (13), and the fixing member (12) slides on the guide rail (13); A straight plate (15) is symmetrically arranged on the fixing member (12), the straight plate (15) and the fixing member (12) are arranged perpendicularly, a rotating member (16) is arranged on the straight plate (15), a clamping claw straight plate (17) is connected between the two rotating members (16), and clamping claw assemblies (2) are respectively arranged on both sides of the clamping claw straight plate (17) for limiting and fixing the small aircraft parts to a specified position for limiting and fixing; A driving member (18) is arranged on any straight plate (15), wherein the driving member (18) is connected to the rotating member (16) and is used to drive the rotating member to rotate and adjust; A probe detection assembly (19) is arranged on one side of the clamp assembly (2) and is used to detect small aircraft parts; A fixing frame (121) is provided on one side of the fixing member (12), a carrier block (122) is provided at the upper end of the fixing frame (121), and a lifting and positioning device (3) is provided in the inner cavity of the fixing frame (121); A double-station carrier (4) is provided on either side of the carrier block (122), the double-station carrier (4) comprising a limit frame (41), a limit rod (42) penetrating the limit frame (41), a limit block (43) is provided at one end of the fixed frame (121), and the limit rod (42) is fixed to the limit block (43); The lifting and positioning device (3) comprises a sliding frame (31), wherein the sliding frame (31) is located in the fixed frame (121), a second guide rail (32) is provided on the inner side surface of the fixed frame (121), and a second guide block (33) is provided relative to the limit frame (41), a fixing bolt (34) is provided at the upper end of the sliding frame (31), and a fixing hole (35) is provided at the lower end relative to the carrier block (122) for fixing by a bayonet, and a cylinder (36) is provided on the fixed frame (121), and a piston rod of the cylinder (36) is fixedly connected to the sliding frame (31).

2. A 4.3KV high voltage test device according to claim 1, characterized in that: The clamping jaw assembly (2) comprises a limiting member (21), the limiting member (21) being fixed on the clamping jaw straight plate (17), the limiting member (21) being provided with a clamping jaw (22), the clamping jaw (22) having a U-shaped cross section, and the clamping jaw (22) being provided with an abutment member (23).

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