Power-on tool

Abstract

The utility model discloses a power-on tool. The power-on tool comprises a copper column; a magnet is arranged on the surface of the front panel; the front panel and the rear panel are attached to each other, and copper column limiting holes are formed in the front panel and the rear panel; according to the utility model, the aviation plug is connected to the detection power supply system, after the air conditioner is connected with the detection system, the power-on tool is adsorbed on the power supply terminal of the air conditioner, and after the system power-on detection and the heating test are completed, the toggle switch is switched to the refrigeration test, so that the problems of power supply difficulty and electric shock risk in the production detection process of the air conditioner are solved.

Description

Technical Field

[0001] The utility model relates to the field of electrical technology, in particular to an upper electrical installation tool. Background Art

[0002] The power supply terminals and detection modes of different air conditioners are different. Some conventional upper electrical installation tools cannot meet the power supply and detection requirements, and only manual wiring can be used for power-on detection, which increases the working hours and has the risk of electric shock. Summary of the Utility Model

[0003] The main purpose of the utility model is to provide an upper electrical installation tool, aiming to solve the existing technical problems.

[0004] To achieve the above purpose, the utility model provides an upper electrical installation tool, including:

[0005] Copper posts;

[0006] A front panel with magnets on its surface; and,

[0007] A rear panel, the front panel and the rear panel are mutually attached, and copper post limiting holes are provided on both the front panel and the rear panel.

[0008] Further, the surface of the front panel has an L-shaped surface, and the magnets are arranged on both segmented surfaces of the L-shaped surface.

[0009] Further, wire grooves are provided on both the front panel and the rear panel for connecting wire harnesses, and the wire harnesses are connected to aviation plugs.

[0010] Further, the front panel and the rear panel are detachably connected through a locking structure.

[0011] Further, the locking structure includes a locking rod, the locking rod has a T-shaped structure, and the locking rod penetrates through the front panel and extends into the rear panel, and a card slot adapted to the end of the locking rod is provided on the rear panel.

[0012] Further, the locking rod is a threaded rod.

[0013] The beneficial effects of the utility model are reflected in:

[0014] In the utility model, an aviation plug is connected to the detection power supply system. After waiting for the air conditioner to be connected to the detection system, the upper electrical installation tool is adsorbed on the power supply terminal of the air conditioner, and the system is powered on for detection. After the heating test is completed, the switch is toggled to switch to the cooling test, solving the problems of power supply difficulties and electric shock risks during the production and detection of air conditioners. Description of the Drawings

[0015] Figure 1 It is a schematic exploded view of the structure of the upper electrical installation tool of the utility model;

[0016] Figure 2 This is a schematic side cross-sectional view of the structure of the present utility model.

[0017] Explanation of reference numerals in the drawings:

[0018] 100, copper column; 200, front panel; 201, magnet; 202, locking rod. Specific embodiments

[0019] Next, the technical solutions in the embodiments of the present utility model will be clearly and completely described in conjunction with the accompanying drawings in the embodiments of the present utility model. Obviously, the described embodiments are only a part of the embodiments of the present utility model, rather than all the embodiments. Without conflict, the embodiments in the present application and the features in the embodiments can be combined with each other. Based on the embodiments in the present utility model, all other embodiments obtained by those of ordinary skill in the art without making creative efforts belong to the scope of protection of the present utility model.

[0020] Please refer to Figure 1 , the present utility model provides an upper electrical tooling, including:

[0021] Copper column 100;

[0022] Front panel 200, with a magnet 201 provided on the surface; and,

[0023] Rear panel 300, the front panel 200 and the rear panel 300 are mutually attached, and copper column limiting holes are provided on both the front panel 200 and the rear panel 300.

[0024] In this embodiment, the upper electrical tooling is adsorbed on the power supply terminal of the air conditioner, the system is powered on for detection, and after the heating test is completed, the toggle switch is switched to the cooling test, solving the problems of power supply difficulty and electric shock risk during the production and detection process of the air conditioner.

[0025] In one embodiment, the surface of the front panel 200 has an L-shaped surface, and the magnet 201 is provided on both segmented surfaces of the L-shaped surface. With this setting in this embodiment, reliable stability can be provided for the upper electrical tooling, ensuring that it will not easily fall due to external forces during use.

[0026] In one embodiment, wire grooves are provided on both the front panel 200 and the rear panel 300 for connecting wire harnesses, and the wire harnesses are connected to aviation plugs.

[0027] In this embodiment, the aviation plug is connected to the detection power supply system. After waiting for the air conditioner to be connected to the detection system, the upper electrical tooling is adsorbed on the power supply terminal of the air conditioner, the system is powered on for detection, and after the heating test is completed, the toggle switch is switched to the cooling test, solving the problems of power supply difficulty and electric shock risk during the production and detection process of the air conditioner.

[0028] It should be noted that the aviation plug and the wire harness are not shown in the figure, and those skilled in the art can make the connection through the prior art.

[0029] In one embodiment, the front panel 200 and the rear panel 300 are detachably connected through a locking structure. With this setting in this embodiment, the detachable connection between the front panel 200 and the rear panel 300 can facilitate the assembly and connection of the wire harness, as well as the disassembly and maintenance of the copper posts 100, adapting to scenarios with different numbers of power supply terminals.

[0030] In one embodiment, the locking structure includes a locking rod 202. The locking rod 202 has a T-shaped structure, and the locking rod 202 penetrates through the front panel 200 and extends into the rear panel 300. A card slot adapted to the end of the locking rod 202 is formed on the rear panel 300.

[0031] With this setting in this embodiment, during assembly, the front panel 200 and the rear panel 300 are joined together, so that the locking rod 202 is inserted into the rear panel 300, and then the locking rod 202 is rotated to form a limit between the locking rod 202 and the card slot in the rear panel 300. The operation is simple and fast, and the disassembly is convenient.

[0032] In one embodiment, the locking rod 202 is a threaded rod. With this setting in this embodiment, the fastening between the front panel 200 and the rear panel 300 can be further improved, avoiding the problem of loosening during normal use.

[0033] It should be noted that if there are directional indications such as up, down, left, right, front, rear... in the embodiments of the present invention, then such directional indications are only used to explain the relative positional relationship and movement conditions between components in a specific posture as shown in the drawings. If this specific posture changes, then the directional indications will also change accordingly.

[0034] In addition, if there are descriptions such as "first", "second", etc. in the embodiments of the present invention, then such descriptions of "first", "second", etc. are only for descriptive purposes and cannot be understood as indicating or implying their relative importance or implicitly indicating the quantity of the indicated technical features. Thus, the features defined with "first" and "second" may explicitly or implicitly include at least one such feature. In addition, the meaning of "and / or" appearing throughout the text includes three parallel solutions. Taking "A and / or B" as an example, it includes solution A, or solution B, or a solution where A and B are satisfied simultaneously. In addition, "multiple" means more than two. In addition, the technical solutions between various embodiments can be combined with each other, but it must be based on the ability of those skilled in the art to implement. When the combination of technical solutions results in contradictions or cannot be implemented, it should be considered that such a combination of technical solutions does not exist.

[0035] The above are only the preferred embodiments of the present utility model and are not intended to limit the present utility model. Any modifications, equivalent substitutions, improvements, etc. made within the spirit and principle of the present utility model shall be included within the protection scope of the present utility model.

Claims

1. Power-on tooling, characterized by ,include: Copper column (100); A front panel (200) having a magnet (201) disposed on its surface; and The rear panel (300) is affixed to the front panel (200) and the rear panel (300), and both the front panel (200) and the rear panel (300) are provided with copper column limiting holes.

2. The power-on tooling according to claim 1, characterized in that: The surface of the front panel (200) has an L-shaped surface, and the magnet (201) is arranged on two segmented surfaces of the L-shaped surface.

3. The power-on tooling according to claim 1, characterized in that: The front panel (200) and the rear panel (300) are both provided with wire grooves for connecting a wire harness, and the wire harness is connected to an aviation plug.

4. The power-on tooling as claimed in claim 1, characterized in that: The front panel (200) and the rear panel (300) are detachably connected via a locking structure.

5. The power-on tooling as claimed in claim 4, characterized in that: The locking structure comprises a locking rod (202), the locking rod (202) is in a T-shaped structure, and the locking rod (202) passes through the front panel (200) and extends into the rear panel (300), and the rear panel (300) is provided with a slot adapted to the end of the locking rod (202).

6. The power-on tooling as claimed in claim 5, characterized in that: The locking rod (202) is a threaded rod.

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