CN218386857U - Power supply unit suitable for FTU - Google Patents

Abstract

The utility model relates to a power supply unit suitable for FTU belongs to FTU power supply technical field, and it includes the shell, be provided with mounting plate in the shell, mounting plate fixes on the shell, the last battery jar that is provided with of mounting plate, be provided with the battery in the battery jar, be fixed with the battery layering on the battery jar, the battery warp the battery layering is fixed mounting plate is last, the other permanent magnetism energy storage capacitor plate that is provided with of battery. The connection problem of battery and permanent magnetism energy storage capacitor plate has been solved in this application, with the effectual seal of the connecting wire of battery and the connecting wire of permanent magnetism energy storage capacitor plate in the shell, operating personnel uses and does not have the potential safety hazard.

Description

Power supply unit for FTU

Technical field:

The present application relates to the technical field of FTU power supply, in particular to a power supply device suitable for FTU.

Background technique:

The existing FTU-powered battery box power supply device is supplied separately by the battery and the permanent magnet energy storage capacitor plate. Due to its spatial layout and structure, the wiring is more complicated, the safety reliability is also poor, and the efficiency is low. It is very difficult for users to use. inconvenient.

Utility model content:

In order to solve the problem of inconvenient use of the existing power supply device, the present application provides a power supply device suitable for FTU.

A power supply device suitable for FTU provided by this application adopts the following technical scheme:

A power supply device suitable for FTU, comprising a housing, the housing is provided with a mounting base plate, the mounting base plate is fixed on the housing, the mounting base plate is provided with a battery slot, and the battery slot is provided with a storage battery , the battery groove is fixed with a battery bead, the battery is fixed on the installation base plate through the battery bead, and a permanent magnet energy storage capacitor plate is arranged next to the battery, and the permanent magnet energy storage capacitor plate is screwed The column is fixed on the installation base plate, and the CT aviation plug is fixed on the installation base plate, and the battery and the permanent magnetic energy storage capacitor plate can supply power to the outside through the CT aviation plug.

By adopting the above technical scheme, the two-in-one wiring of the battery and the permanent magnet energy storage capacitor board is connected to the outside through the CT aviation plug. When using it, the customer only needs to hang the entire shell to use it. The connection is wrong one after another, and the space is compact, which also greatly increases the safety and reliability.

Preferably, the installation bottom plate is L-shaped, which includes a bottom plate and a side plate, the battery and the permanent magnet energy storage capacitor plate are arranged on the bottom plate, and the CT aerial plug is arranged on the side plate, The side plate and the shell are fixed by screws.

Preferably, the side plate is fitted on the housing, and a sealing ring is provided between the side plate and the housing.

By adopting the above technical solution, the arrangement of the sealing ring can reduce the entry of dust and water vapor into the housing, thereby improving the service life of the electronic components.

Preferably, the housing is provided with a connecting frame.

By adopting the above technical solution, the connecting frame can be used for the installation of the power supply device.

Preferably, several evenly distributed fins are provided on the surface of the housing.

By adopting the above technical solution, the fins can increase the contact area between the shell and the air, thereby improving the heat dissipation effect, ensuring that the temperature inside the shell can be quickly dissipated into the air, and effectively improving the service life of the electronic components.

Preferably, the edges of the housing and the installation base are rounded.

By adopting the above technical solution, there is no sharp edge in the setting of the rounded corners, which will not scratch the skin during use, and protect the safety of the operator to the greatest extent.

In summary, the present application includes at least one of the following beneficial technical effects:

1. This application solves the wiring problem of the battery and the permanent magnet energy storage capacitor board, and effectively seals the connection wires of the battery and the permanent magnet energy storage capacitor board in the casing, so that there is no potential safety hazard for operators to use;

2. The shell structure is designed with rounded corners, and the whole has no sharp corners to avoid scratching the operation and maintenance personnel;

3. Fins are provided on the surface of the shell, which can increase the contact area between the shell and the air, thereby improving the heat dissipation effect, ensuring that the temperature inside the shell can be quickly dissipated into the air, and effectively improving the service life of electronic components.

Description of drawings:

FIG. 1 is a schematic diagram of the overall structure of an embodiment of the present application.

Fig. 2 is a schematic diagram of an exploded structure of an embodiment of the present application.

Explanation of reference signs: 1. shell; 11. connecting frame; 12. fin; 13. ear block; 2. installation bottom plate; 21. bottom plate; 22. side plate; 3. battery; Magnetic energy storage capacitor plate; 6. CT aviation plug.

Detailed ways:

The present application will be described in further detail below in conjunction with accompanying drawings 1-2.

The embodiment of the present application discloses a power supply device suitable for FTU. Referring to Fig. 1 and Fig. 2, it includes a housing 1, and the housing 1 is provided with a connecting frame 11 and several uniformly distributed fins 12, and the connecting frame 11 is used for the power supply device. Installation, the fins 12 can increase the contact area between the shell 1 and the air, thereby improving the heat dissipation effect, ensuring that the temperature inside the shell 1 can be quickly dissipated into the air, and effectively improving the service life of the electronic components. The shell 1 is provided with a mounting base 2 , the installation base plate 2 is fixed on the shell 1, the installation base plate 2 is provided with a battery slot, the battery slot is provided with a battery 3, the battery slot is fixed with a battery bead 4, the battery 3 is fixed on the installation base plate 2 through the battery bead 4, and the battery There is a permanent magnet energy storage capacitor plate 5 next to the 3, and the permanent magnet energy storage capacitor plate 5 is fixed on the installation base plate 2 by studs, and the CT aviation plug 6 is fixed on the installation base plate 2, and the battery 3 and the permanent magnet energy storage capacitor plate 5 The battery 3 and the permanent magnet energy storage capacitor plate 5 can supply power to the outside through the CT aviation plug 6. The battery 3 and the permanent magnet energy storage capacitor plate 5 are arranged inside the shell 1, which effectively isolates the battery from the outside. Physical contact, so as to achieve safe and reliable protection, and there is no potential safety hazard for operators to use.

When customers use it, they only need to hang the entire shell 1 to use it. The steps are simple, the installation efficiency is high, the connection errors are avoided, the space is compact, and the safety and reliability are greatly increased. It can make the output voltage of the FTU equipment Stable, improve the stability and security of FTU equipment power supply.

Referring to Fig. 2, the installation bottom plate 2 is L-shaped, which includes a bottom plate 21 and a side plate 22, the battery 3 and the permanent magnet energy storage capacitor plate 5 are arranged on the bottom plate 21, the CT aviation plug 6 is arranged on the side plate 22, and the side plate 22 It is fixed with the shell 1 by screws. In order to facilitate installation, ear pieces 13 are provided on both sides of the inner wall of the shell 1. There are threaded grooves on the ear pieces 13, and the screws can be screwed in the threaded grooves. The side plate 22 is fitted on the shell 1. In addition, a sealing ring is provided between the side plate 22 and the housing 1 . The sealing ring can reduce dust and water vapor from entering the housing 1 , thereby improving the service life of the electronic components.

Referring to FIG. 2 , the edges of the housing 1 and the mounting base 2 are rounded, and the rounded corners have no sharp edges, which will not scratch the skin during use and maximize the safety of the operator.

All of the above are preferred embodiments of the application, and are not intended to limit the protection scope of the application. Therefore, all equivalent changes made according to the structure, shape, and principle of the application should be covered by the protection scope of the application. Inside.

Claims (6)

1. A power supply unit suitable for FTU which characterized in that: including shell (1), be provided with mounting plate (2) in shell (1), mounting plate (2) are fixed on shell (1), be provided with the battery jar on mounting plate (2), be provided with battery (3) in the battery jar, be fixed with battery layering (4) on the battery jar, battery (3) warp battery layering (4) are fixed on mounting plate (2), the other permanent magnetism energy storage capacitor plate (5) that is provided with of battery (3), permanent magnetism energy storage capacitor plate (5) are fixed through the double-screw bolt on mounting plate (2), be fixed with CT aviation plug (6) on mounting plate (2), battery (3) with permanent magnetism energy storage capacitor plate (5) can pass through CT aviation plug (6) are to the outside power supply.

2. A power supply unit adapted for an FTU according to claim 1, further comprising: the mounting bottom plate (2) is L-shaped and comprises a bottom plate (21) and a side plate (22), the storage battery (3) and the permanent magnet energy storage capacitor plate (5) are arranged on the bottom plate (21), the CT aerial plug (6) is arranged on the side plate (22), and the side plate (22) and the shell (1) are fixed through screws.

3. A power supply apparatus adapted for use in an FTU according to claim 2, wherein: the side plate (22) is embedded on the shell (1), and a sealing ring is arranged between the side plate (22) and the shell (1).

4. A power supply apparatus adapted for use in an FTU according to claim 1, wherein: the shell (1) is provided with a connecting frame (11).

5. A power supply unit adapted for an FTU according to claim 1, further comprising: the surface of the shell (1) is provided with a plurality of uniformly distributed fins (12).

6. A power supply unit adapted for an FTU according to claim 1, further comprising: the edges of the shell (1) and the mounting bottom plate (2) are all arranged in a round angle mode.

Images