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Aviation shockproof plug with automatic power-off function

An automatic power-off and functional technology, applied in electric vehicle charging technology, circuits, electric vehicles, etc., can solve problems such as affecting work, the plug cannot be automatically pulled out from the socket, and the plug falls off, so as to save time.

Pending Publication Date: 2022-08-02
李洁
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] In order to overcome the situation that the vibration occurs, the plug may fall off, causing a power outage and affecting people's work. Secondly, when there is a leakage, the plug cannot be pulled out from the socket automatically, which is likely to cause the failure of the entire power supply system. The technical problem to be solved is: to provide an aviation shockproof plug with an automatic power-off function that will not affect people's normal work and can avoid accidents

Method used

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  • Aviation shockproof plug with automatic power-off function
  • Aviation shockproof plug with automatic power-off function
  • Aviation shockproof plug with automatic power-off function

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0074] A shockproof plug with automatic power-off function for aviation, such as Figure 1-6 As shown, it includes a first fixing plate 1, a first supporting plate 2, a first connecting plate 3, a manual disconnecting mechanism 4, a first clamping mechanism 5, a second clamping mechanism 6 and a manual releasing mechanism 7. A first support plate 2 is arranged on the upper part of the front side of a fixed plate 1 , a first connecting plate 3 is arranged on the front side of the first support plate 2 , and a manual disconnection mechanism 4 is arranged in the first support plate 2 . A first clamping mechanism 5 is provided, a second clamping mechanism 6 is provided on the top of the first fixing plate 1 , and a manual releasing mechanism 7 is provided on the first clamping mechanism 5 .

[0075] The manual disconnection mechanism 4 includes a first movable plate 40, a pulling plate 41 and a first spring 42. The first supporting plate 2 is slidably provided with a first movable...

Embodiment 2

[0081] On the basis of Example 1, as figure 1 , figure 2 , Figure 7 , Figure 8 and Figure 9 As shown, it also includes an automatic disconnection mechanism 8. The automatic disconnection mechanism 8 includes a second fixing plate 80, an electric wire 81 and an electromagnet 82. A second fixing plate 80 is connected in the middle of the top of the first fixing plate 1. The plate 80 is provided with an electromagnet 82 , and the electromagnet 82 is provided with an electric wire 81 , and the electric wire 81 is connected to the upper part of the first fixing plate 1 .

[0082] When leakage occurs, electricity is conducted to the electromagnet 82 through the wire 81, the electromagnet 82 is energized, and the electromagnet 82 generates a suction force on the first movable plate 40, so that the first movable plate 40 moves upward, and the power is automatically cut off to avoid When an accident occurs, the first spring 42 is compressed, and when there is no leakage, the el...

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Abstract

The invention relates to a shockproof plug, in particular to an aviation shockproof plug with an automatic power-off function. The technical problem to be solved is to provide a shockproof plug with an automatic power-off function for aviation, which does not affect normal work of people and can avoid accidents. An aviation shockproof plug with an automatic power-off function comprises a first fixing plate and a first supporting plate, and the first supporting plate is arranged on the upper portion of the first fixing plate; the first connecting plate is arranged on the first supporting plate; and the manual disconnecting mechanism is arranged in the first supporting plate. The position of the first supporting plate can be fixed through the first clamping mechanism, the second clamping mechanism can block the first supporting plate, the first supporting plate is prevented from loosening, the situation of power failure is avoided, normal work of people cannot be affected, power failure can be automatically conducted through the automatic disconnection mechanism, and accidents are avoided.

Description

technical field [0001] The invention relates to an anti-vibration plug, in particular to an anti-vibration plug with an automatic power-off function for aviation. Background technique [0002] The plug is a common connector in the electronics industry. It is used to transmit electrical energy and can be used in the aviation field. The plug is generally inserted into the socket and does not have the function of fixing the plug. If there is vibration, the plug may fall off, causing broken The electricity situation affects people's work. Secondly, when there is a leakage of electricity, the plug cannot be automatically pulled out from the socket, which may easily cause the failure of the entire power supply system. [0003] To this end, we design a device that will not interfere with people's normal work and avoid accidents. SUMMARY OF THE INVENTION [0004] In order to overcome the situation of vibration, the plug may fall off, causing a power failure and affecting people's...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): H01R13/639H01R13/66H01R13/713H01R13/508H01R13/533H01R13/635
CPCH01R13/639H01R13/533H01R13/635H01R13/713H01R13/6691H01R13/508Y02T90/14
Inventor 李洁
Owner 李洁
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