CN217280435U

CN217280435U - Pulse capacitor for laser engineering

Info

Publication number: CN217280435U
Application number: CN202220147102.6U
Authority: CN
Inventors: 王海奔; 占竹林; 傅胜春
Original assignee: Shanghai Qiyu Optoelectronics Technology Co ltd
Current assignee: Shanghai Qiyu Optoelectronics Technology Co ltd
Priority date: 2022-01-20
Filing date: 2022-01-20
Publication date: 2022-08-23
Anticipated expiration: 2032-01-20

Abstract

The utility model relates to the technical field of capacitors, and discloses a pulse capacitor for laser engineering, which comprises a pulse capacitor, wherein two sides of the pulse capacitor are both provided with guide shells; the guide shells are fixedly provided with inserting blocks, the inserting blocks are sleeved with limiting frames in a sliding mode, and the limiting frames and the inserting blocks are sleeved with wing-shaped bolts in a threaded mode; the guide shell is internally provided with a buffer part in a sliding manner, and the buffer part is connected with the limiting frame through a blowing part; and an airflow disturbance part is arranged at the bottom of the pulse capacitor. The utility model provides a pulse capacitor for laser engineering, the utility model discloses a be equipped with the bolster, cushion pulse capacitor's vibrations, pulse capacitor's vibrations are pressed and are stretched air current disturbance spare, and then carry out the disturbance to pulse capacitor's air current on every side to cool down.

Description

Pulse capacitor for laser engineering

Technical Field

The utility model relates to a condenser field especially relates to a pulse capacitor for laser engineering.

Background

Due to the ultrahigh reliability of the pulse capacitor, the pulse capacitor can be applied to most high-tech military equipment. Such as laser (opto-electronic) weapons, electromagnetic guns, electromagnetic weapons, electronic interference, radar equipment, communications transmissions, and the like. The method has good application in high-end civil markets, such as the mechanical field of laser cutting and the like.

Because pulse capacitor is applied to laser engineering field, present some pulse capacitors receive vibrations when using and reduce life, and the production that accompanies heat when using is unfavorable for its stable use if be in high temperature for a long time simultaneously.

In order to solve the above problems, a pulse capacitor for laser engineering is proposed in the present application.

SUMMERY OF THE UTILITY MODEL

Objects of the first utility model

For solving the technical problem that exists among the background art, the utility model provides a pulse capacitor for laser engineering, the utility model discloses a be equipped with the bolster, cushion pulse capacitor's vibrations, pulse capacitor's vibrations are pressed and are stretched air current disturbance spare, and then carry out the disturbance to the air current around pulse capacitor to cool down.

(II) technical scheme

In order to solve the problems, the utility model provides a pulse capacitor for laser engineering, which comprises a pulse capacitor, wherein two sides of the pulse capacitor are provided with guide shells;

the guide shells are fixedly provided with inserting blocks, the inserting blocks are sleeved with limiting frames in a sliding mode, and the limiting frames and the inserting blocks are sleeved with wing-shaped bolts in a threaded mode;

the guide shell is internally provided with a buffer piece in a sliding manner, and the buffer piece is connected with the limiting frame through a blowing piece;

and an airflow disturbance part is arranged at the bottom of the pulse capacitor.

Preferably, the buffer piece includes deflector and buffer spring, the deflector slides and sets up in the inside of direction shell to with pulse capacitor fixed connection, buffer spring's one end and deflector fixed connection.

Preferably, the blowing piece comprises a mounting plate and a first air bag, the mounting plate is fixedly mounted at the top of the guide shell, the first air bag is fixedly mounted on the mounting plate, and the first air bag is fixedly connected with the other end of the buffer spring.

Preferably, the air flow disturbance element comprises an air bag II and an air inlet valve, the air bag II is fixedly installed at the bottom of the pulse capacitor, the air inlet valve is fixedly communicated with the air bag II, and an air hole is formed in the air bag II.

Preferably, the number of the air holes is multiple.

The above technical scheme of the utility model has following profitable technological effect:

one limiting frame is fixed with the fixing surface, and the other limiting frame is connected with the fixing surface through a wing-shaped bolt, so that the effects of facilitating installation and relieving limiting are achieved; the pulse capacitor receives vibrations to drive and reciprocates, drives the deflector and acts on buffer spring, in order to play buffering absorbing effect, the pulse capacitor removes at vertical direction and compresses two gasbags, two inside gas of gasbag are discharged by the gas pocket, blow pulse capacitor surrounding gas, in order to play supplementary radiating effect, along with the pulse capacitor removes the extrusion to two gasbags, outside gas gets into to two gasbags through the admission valve, in order to do benefit to next use.

Drawings

Fig. 1 is a schematic structural diagram of a pulse capacitor for laser engineering according to the present invention.

Fig. 2 is a schematic diagram of a partially disassembled structure in a pulse capacitor for laser engineering according to the present invention.

Reference numerals are as follows: 1. a pulse capacitor; 2. a guide housing; 3. inserting a block; 4. a limiting frame; 5. a wing bolt; 6. a buffer member; 61. a guide plate; 62. a buffer spring; 7. a blowing member; 71. mounting a plate; 72. a first air bag; 8. an airflow disruption member; 81. a second air bag; 82. an intake valve; 83. and (4) air holes.

Detailed Description

In order to make the objects, technical solutions and advantages of the present invention more apparent, the present invention will be described in further detail with reference to the accompanying drawings in combination with the following embodiments. It should be understood that the description is intended for purposes of illustration only and is not intended to limit the scope of the present disclosure. Moreover, in the following description, descriptions of well-known structures and techniques are omitted so as to not unnecessarily obscure the concepts of the present invention.

As shown in fig. 1-2, the pulse capacitor for laser engineering provided by the present invention comprises a pulse capacitor 1, wherein both sides of the pulse capacitor 1 are provided with a guiding shell 2;

the guide shell 2 is fixedly provided with an insert block 3, the insert block 3 is sleeved with a limiting frame 4 in a sliding manner, and the limiting frame 4 and the insert block 3 are both sleeved with wing-shaped bolts 5 in a threaded manner;

a buffer part 6 is arranged in the guide shell 2 in a sliding manner, and the buffer part 6 is connected with the limiting frame 4 through a blowing part 7;

the bottom of the pulse capacitor 1 is provided with an airflow disturbance element 8.

In an alternative embodiment, in order to buffer and damp the pulse capacitor 1, the buffer member 6 includes a guide plate 61 and a buffer spring 62, the guide plate 61 is slidably disposed inside the guide housing 2 and is fixedly connected to the pulse capacitor 1, and one end of the buffer spring 62 is fixedly connected to the guide plate 61.

In an alternative embodiment, the blowing member 7 includes a mounting plate 71 and a first airbag 72, the mounting plate 71 is fixedly mounted on the top of the guide housing 2, the first airbag 72 is fixedly mounted on the mounting plate 71, the first airbag 72 is fixedly connected with the other end of the buffer spring 62, and a through hole is opened in an end surface of the first airbag 72 facing the pulse capacitor 1, so that when the first airbag 72 is compressed by the buffer spring 62, air is exhausted through the through hole to dissipate heat of the pulse capacitor 1.

In an alternative embodiment, the airflow disturbance element 8 includes a second air bag 81 and an air inlet valve 82, the second air bag 81 is fixedly installed at the bottom of the pulse capacitor 1, the air inlet valve 82 is fixedly communicated with the second air bag 81, an air hole 83 is formed in the second air bag 81, and the air inlet valve 82 is a one-way air inlet valve, so that external air enters the inside of the second air bag 81.

In an alternative embodiment, the number of the air holes 83 is multiple, and the multiple air holes 83 are evenly distributed on the air bag two 81 at equal intervals.

In the utility model, one limiting frame 4 (no wing bolt on the limiting frame 4) is fixed with the fixed surface, and the other limiting frame 4 is connected with the fixed surface through the wing bolt 5, so as to achieve the effect of facilitating installation and relieving the limiting, when relieving the limiting to the pulse capacitor 1, the wing bolt 5 is screwed out, the limiting frame 4 which is shifted out the wing bolt 5 is separated from the insert block 3, and the pulse capacitor 1 is moved in the horizontal direction to drive the insert block 3 to be separated from the other limiting frame 4, thereby achieving the effect of convenient disassembly; pulse capacitor 1 receives vibrations to drive and reciprocates, it acts on buffer spring 62 to drive deflector 61, in order to play buffering absorbing effect, pulse capacitor 1 removes at vertical direction and compresses two 81 gasbags, two 81 inside gases of gasbags are discharged by gas pocket 83, blow around pulse capacitor 1 gas, in order to play supplementary radiating effect, along with pulse capacitor 1 removes the extrusion to two 81 gasbags, outside gas gets into two 81 gasbags through admission valve 82, in order to do benefit to next use.

It is to be understood that the above-described embodiments of the present invention are merely illustrative of or explaining the principles of the invention and are not to be construed as limiting the invention. Therefore, any modification, equivalent replacement, improvement and the like made without departing from the spirit and scope of the present invention should be included in the protection scope of the present invention. Further, it is intended that the appended claims cover all such variations and modifications as fall within the scope and boundaries of the appended claims or the equivalents of such scope and boundaries.

Claims

1. A pulsed capacitor for laser engineering, comprising a pulsed capacitor (1), characterized in that: guide shells (2) are arranged on two sides of the pulse capacitor (1);

the guide shell (2) is fixedly provided with inserting blocks (3), the inserting blocks (3) are slidably sleeved with limiting frames (4), and the limiting frames (4) and the inserting blocks (3) are both sleeved with wing-shaped bolts (5) in a threaded manner;

a buffer piece (6) is arranged in the guide shell (2) in a sliding manner, and the buffer piece (6) is connected with the limiting frame (4) through a blowing piece (7);

and an airflow disturbance element (8) is arranged at the bottom of the pulse capacitor (1).

2. The pulse capacitor for laser engineering according to claim 1, wherein the buffer member (6) comprises a guide plate (61) and a buffer spring (62), the guide plate (61) is slidably arranged inside the guide shell (2) and is fixedly connected with the pulse capacitor (1), and one end of the buffer spring (62) is fixedly connected with the guide plate (61).

3. The pulse capacitor for laser engineering according to claim 2, wherein the blowing piece (7) comprises a mounting plate (71) and a first air bag (72), the mounting plate (71) is fixedly mounted on the top of the guide shell (2), the first air bag (72) is fixedly mounted on the mounting plate (71), and the first air bag (72) is fixedly connected with the other end of the buffer spring (62).

4. The pulse capacitor for laser engineering according to claim 1, wherein the air flow disturbing part (8) comprises a second air bag (81) and an air inlet valve (82), the second air bag (81) is fixedly installed at the bottom of the pulse capacitor (1), the air inlet valve (82) is fixedly communicated with the second air bag (81), and the second air bag (81) is provided with an air hole (83).

5. A pulse capacitor for laser engineering according to claim 4, characterized in that the number of the air holes (83) is plural.