CN213338980U - Aviation plug fixing alarm device - Google Patents
Aviation plug fixing alarm device Download PDFInfo
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- CN213338980U CN213338980U CN202022317534.0U CN202022317534U CN213338980U CN 213338980 U CN213338980 U CN 213338980U CN 202022317534 U CN202022317534 U CN 202022317534U CN 213338980 U CN213338980 U CN 213338980U
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- aviation plug
- shell
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- plug
- warning
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Abstract
An aviation plug fixing alarm device comprises an aviation plug I, an aviation plug II, an alarm assembly I and an alarm assembly II; the first alarm component is arranged on the first aviation plug; the alarm assembly II is arranged on the aviation plug II; the first alarm component comprises a first shell, a second shell, a top block, a rod, a stop block, a spring, a pressure sensor, a control center and a warning lamp; the second alarm component comprises a pressing block; the utility model discloses in, the device sets up warning subassembly one and warning subassembly two, can forget to screw up the screw thread solid fixed ring and the plug is not hard up when droing to send light and sound suggestion, warns the installer to carry out inspection, maintenance or reinstallation to the junction, avoids appearing the aviation plug because fixed insecure takes place to drop, causes whole transmission line trouble, causes the condition emergence of safety problem even; the device has the advantages of simple structure, convenient operation, convenient installation and disassembly, high result precision and good application prospect and commercial value.
Description
Technical Field
The utility model relates to an aviation plug technical field especially relates to an aviation plug fixed alarm device.
Background
Aviation plugs are one type of connector, originating from the military industry. An aviation plug is an electromechanical element that connects electrical lines, and therefore its own electrical parameters are the first issues to consider in selecting an aviation plug. Proper selection and use of the aviation plug is an important aspect of ensuring circuit reliability. At present, the circular thread aviation plug which is generally adopted can not be screwed down in place by the thread fixing ring in the installation process, and even installation personnel can only insert the aviation plug into equipment and forget to screw down the thread fixing ring, so that the safe connection between a cable and the equipment can not be ensured. The aviation plug is an important device for connecting a cable and power transmission equipment, and can fall off once being not firmly fixed, so that the fault of the whole power transmission line is easily caused, and serious potential safety hazards exist.
In order to solve the problem, the application provides an aviation plug fixing alarm device.
SUMMERY OF THE UTILITY MODEL
Objects of the invention
In order to solve the technical problems existing in the background technology, the utility model provides an aviation plug fixing alarm device, which can send out light and sound prompts when an installer forgets to screw a thread fixing ring and a plug is loosened and falls off, and warn the installer to check, maintain or reinstall a connection part, thereby avoiding the situations that the aviation plug falls off due to infirm fixation, causing the fault of the whole power transmission line and even causing the safety problem; the device has the advantages of simple structure, convenient operation, convenient installation and disassembly, high result precision and good application prospect and commercial value.
(II) technical scheme
In order to solve the problems, the utility model provides an aviation plug fixing alarm device, which comprises an aviation plug I, an aviation plug II, an alarm component I and an alarm component II; the first alarm component is arranged on the first aviation plug; the alarm assembly II is arranged on the aviation plug II; an internal thread fixing ring is rotatably arranged on the first aviation plug; an external thread fixing ring is arranged on the aviation plug II; the aviation plug I is connected with an aviation plug II through the matching of the internal thread fixing ring and the external thread fixing ring; the first alarm component comprises a first shell, a second shell, a top block, a rod, a stop block, a spring, a pressure sensor, a control center and a warning lamp; the first shell is arranged on one side of the first aviation plug, and a second shell is arranged at one end close to the interface of the first aviation plug and communicated with the second shell; the control center is arranged inside the first shell; the warning lamp is arranged on the outer wall of the first shell; the pressure sensor is arranged in the first shell and is positioned at the communication position of the first shell and the second shell; the spring is arranged in the shell II, one end of the spring is connected with the pressure sensor, and the other end of the spring is provided with a stop block; one end of the rod is connected with the stop block, and the other end of the rod extends out of the second shell and is connected with the top block; the second alarm component comprises a pressing block; the pressing block is arranged on one side of the second aviation plug and is opposite to the top block in position.
Preferably, the first alarm assembly further comprises a first hoop; the first shell is arranged on one side of the first aviation plug through the first hoop; the alarm assembly II also comprises a hoop II; the pressing block is arranged on one side of the second aviation plug through the second hoop.
Preferably, bolts are arranged on the first clamp and the second clamp and are fixedly clamped through the bolts.
Preferably, the pressure sensor and the warning lamp are in signal connection with the control center.
Preferably, the first alarm component further comprises a buzzer and a timer; the buzzer is arranged on the outer wall of the first shell; the timer is arranged in the first shell; the buzzer and the timer are in signal connection with the control center.
Preferably, a power supply for supplying power to the device is also arranged in the first shell.
Preferably, the outer wall of the internal thread fixing ring is provided with anti-skid lines convenient to screw down.
The above technical scheme of the utility model has following profitable technological effect:
the utility model discloses in, the device sets up warning subassembly one and warning subassembly two, can forget to screw up the screw thread solid fixed ring and the plug is not hard up when droing to send light and sound suggestion, warns the installer to carry out inspection, maintenance or reinstallation to the junction, avoids appearing the aviation plug because fixed insecure takes place to drop, causes whole transmission line trouble, causes the condition emergence of safety problem even; the device has the advantages of simple structure, convenient operation, convenient installation and disassembly, high result precision and good application prospect and commercial value.
Drawings
Fig. 1 is the utility model provides an aviation plug fixes alarm device unconnected state's schematic structure diagram.
Fig. 2 is the utility model provides an aviation plug fixes alarm device connection status's schematic structure diagram.
FIG. 3 is the schematic structural diagram of a first clamp in the aviation plug fixing alarm device
Reference numerals: 1. an aviation plug I; 2. an aviation plug II; 3. a first alarm component; 4. a second alarm component; 5. an internal thread fixing ring; 6. an external thread fixing ring; 7. a first hoop is clamped; 8. a first shell; 9. a second shell; 10. a top block; 11. a rod; 12. a stopper; 13. a spring; 14. a pressure sensor; 15. a power source; 16. a control center; 17. a warning light; 18. a buzzer; 19. a second hoop; 20. briquetting; 21. a timer; 22. and (4) bolts.
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 detail with reference to the accompanying drawings. It should be understood that the description is intended to be illustrative only and is not intended to limit the scope of the present invention. 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. 1-3, the utility model provides an aviation plug fixing alarm device, which comprises an aviation plug 1, an aviation plug 2, an alarm component 3 and an alarm component 4; the alarm assembly I3 is arranged on the aviation plug I1; the second alarm assembly 4 is arranged on the second aviation plug 2; an internal thread fixing ring 5 is rotatably arranged on the aviation plug I1; an external thread fixing ring 6 is arranged on the aviation plug II 2; the aviation plug I1 is connected with the aviation plug II 2 through the matching of the internal thread fixing ring 5 and the external thread fixing ring 6; the first alarm component 3 comprises a first shell 8, a second shell 9, a top block 10, a rod 11, a stop block 12, a spring 13, a pressure sensor 14, a control center 16 and a warning lamp 17; the first shell 8 is arranged on one side of the first aviation plug 1, and a second shell 9 is arranged at one end, close to the interface of the first aviation plug 1, and is communicated with the second shell 9; the control center 16 is arranged inside the first shell 8; the warning lamp 17 is arranged on the outer wall of the first shell 8; the pressure sensor 14 is arranged inside the first shell 8 and is positioned at the position where the first shell 8 is communicated with the second shell 9; the spring 13 is arranged inside the second shell 9, one end of the spring is connected with the pressure sensor 14, and the other end of the spring is provided with a stop block 12; one end of the rod 11 is connected with the stop block 12, and the other end of the rod extends out of the second shell 9 and is connected with the top block 10; the second alarm component 4 comprises a pressing block 20; the pressing block 20 is arranged on one side of the aviation plug II 2 and is opposite to the top block 10.
In an optional embodiment, the first alarm assembly 3 further comprises a first hoop 7; the first shell 8 is arranged on one side of the first aviation plug 1 through the first hoop 7; the second alarm component 4 further comprises a second hoop 19; the pressing block 20 is arranged on one side of the aviation plug II 2 through the hoop II 19.
In an alternative embodiment, bolts 22 are arranged on the first clamping hoop 7 and the second clamping hoop 19, and the two clamping hoops are fixedly clamped through the bolts 22.
In an alternative embodiment, the pressure sensor 14 and the warning light 17 are both in signal communication with the control center 16.
In an alternative embodiment, the first alarm component 3 further comprises a buzzer 18 and a timer 21; the buzzer 18 is arranged on the outer wall of the first shell 8; the timer 21 is arranged inside the first shell 8; the buzzer 18 and the timer 21 are both in signal connection with the control center 16.
In an alternative embodiment, a power supply 15 for supplying power to the device is also arranged inside the first shell 8.
In an alternative embodiment, the outer wall of the internally threaded fixing ring 5 is provided with anti-slip lines for facilitating screwing.
In the utility model, the working principle of the device is that the first aerospace plug 1 is aligned with the second aerospace plug 2 and is spliced together, then the internal thread fixing ring 5 is rotated, and the first aerospace plug 1 and the second aerospace plug 2 are fixed together through the matching of the internal thread fixing ring 5 and the external thread fixing ring 6; in the fixing process, the pressing block 20 pushes the top block 10 and the rod 11 to compress the spring 13, and the spring 13 transmits the received force to the pressure sensor 14; the pressure sensor 14 continuously transmits the pressure data to the control center 16 in real time from the generation of the data, if the internal thread fixing ring 5 and the external thread fixing ring 6 are not screwed, the data value output by the pressure sensor 14 does not reach the preset value or the connection is loose, and the control center 16 detects that the received data value is reduced, a signal is sent to the warning lamp 17, the warning lamp 17 flickers, a signal is sent to the timer 21 at the same time, the timer 21 starts to time, after the time is accumulated for a period of time, the timer 21 sends a signal to the control center 16, and the control center 16 controls the buzzer 18 to send an alarm; in the process, if the data reaches the preset value, the control center 16 sends signals to the warning lamp 17 and the timer 21, so that the warning lamp 17 stops flashing, and the timer 21 stops timing.
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 (7)
1. An aviation plug fixing alarm device is characterized by comprising a first aviation plug (1), a second aviation plug (2), a first alarm component (3) and a second alarm component (4); the first alarm component (3) is arranged on the first aviation plug (1); the second alarm component (4) is arranged on the second aviation plug (2); an internal thread fixing ring (5) is rotatably arranged on the aviation plug I (1); an external thread fixing ring (6) is arranged on the aviation plug II (2); the aviation plug I (1) is connected with the aviation plug II (2) through the matching of the internal thread fixing ring (5) and the external thread fixing ring (6);
the first alarm component (3) comprises a first shell (8), a second shell (9), a top block (10), a rod (11), a stop block (12), a spring (13), a pressure sensor (14), a control center (16) and a warning lamp (17); the first shell (8) is arranged on one side of the first aviation plug (1), and a second shell (9) is arranged at one end close to the interface of the first aviation plug (1) and communicated with the second shell (9); the control center (16) is arranged inside the first shell (8); the warning lamp (17) is arranged on the outer wall of the first shell (8); the pressure sensor (14) is arranged inside the first shell (8) and is positioned at the position where the first shell (8) is communicated with the second shell (9); the spring (13) is arranged inside the second shell (9), one end of the spring is connected with the pressure sensor (14), and the other end of the spring is provided with a stop block (12); one end of the rod (11) is connected with the stop block (12), and the other end of the rod extends out of the second shell (9) and is connected with the top block (10); the second alarm component (4) comprises a pressing block (20); the pressing block (20) is arranged on one side of the aviation plug II (2) and is opposite to the top block (10).
2. The aircraft plug attachment warning device of claim 1, wherein the first warning assembly (3) further comprises a first clip (7); the first shell (8) is arranged on one side of the first aviation plug (1) through the first hoop (7); the second alarm component (4) also comprises a second hoop (19); the pressing block (20) is arranged on one side of the aviation plug II (2) through the hoop II (19).
3. The aviation plug fixing alarm device as claimed in claim 2, wherein bolts (22) are arranged on the first clamping hoop (7) and the second clamping hoop (19), and the first clamping hoop and the second clamping hoop are fixedly clamped through the bolts (22).
4. The aircraft plug attachment warning device of claim 1, wherein the pressure sensor (14) and the warning light (17) are in signal connection with a control center (16).
5. The aviation plug fixation warning device of claim 1, wherein the first warning component (3) further comprises a buzzer (18) and a timer (21); the buzzer (18) is arranged on the outer wall of the first shell (8); the timer (21) is arranged inside the first shell (8); the buzzer (18) and the timer (21) are in signal connection with the control center (16).
6. The aviation plug attachment alarm device of claim 1, wherein a power supply (15) for supplying power to the device is further disposed inside the first housing (8).
7. The aviation plug fixing alarm device as claimed in claim 1, wherein the outer wall of the internal thread fixing ring (5) is provided with anti-skid lines which are convenient to screw.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022317534.0U CN213338980U (en) | 2020-10-16 | 2020-10-16 | Aviation plug fixing alarm device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022317534.0U CN213338980U (en) | 2020-10-16 | 2020-10-16 | Aviation plug fixing alarm device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN213338980U true CN213338980U (en) | 2021-06-01 |
Family
ID=76072912
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202022317534.0U Active CN213338980U (en) | 2020-10-16 | 2020-10-16 | Aviation plug fixing alarm device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN213338980U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114534154A (en) * | 2022-03-02 | 2022-05-27 | 上海瀚金照明科技有限公司 | Automatic fire-fighting method and system |
-
2020
- 2020-10-16 CN CN202022317534.0U patent/CN213338980U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114534154A (en) * | 2022-03-02 | 2022-05-27 | 上海瀚金照明科技有限公司 | Automatic fire-fighting method and system |
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