CN219348995U - Detection device of aviation fire-extinguishing bottle electric detonator - Google Patents

Detection device of aviation fire-extinguishing bottle electric detonator Download PDF

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Publication number
CN219348995U
CN219348995U CN202320179886.5U CN202320179886U CN219348995U CN 219348995 U CN219348995 U CN 219348995U CN 202320179886 U CN202320179886 U CN 202320179886U CN 219348995 U CN219348995 U CN 219348995U
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China
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pair
supporting seat
electric detonator
sliding
blocks
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CN202320179886.5U
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Chinese (zh)
Inventor
贺凯歌
任昊天
刘艺
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Lanzhou Lanyi Aircraft Equipment Manufacture Ltd
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Lanzhou Lanyi Aircraft Equipment Manufacture Ltd
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    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02ATECHNOLOGIES FOR ADAPTATION TO CLIMATE CHANGE
    • Y02A40/00Adaptation technologies in agriculture, forestry, livestock or agroalimentary production
    • Y02A40/10Adaptation technologies in agriculture, forestry, livestock or agroalimentary production in agriculture
    • Y02A40/28Adaptation technologies in agriculture, forestry, livestock or agroalimentary production in agriculture specially adapted for farming

Abstract

The utility model discloses a detection device of an electric detonator of an aviation fire-extinguishing bottle, which relates to the technical field of fire extinguisher detection devices and comprises an operation table, wherein a supporting seat is arranged below the operation table, one side of the supporting seat is provided with the supporting table, a circuit detection mechanism is arranged on the supporting table, one side of the upper end of the operation table is provided with a motor case, the other side of the upper end of the operation table is provided with a slot, the slot is provided with a trigger mechanism, a sliding clamping mechanism is arranged below the slot, the supporting seat is provided with a pair of fastening mechanisms, a driving motor is started to drive a cam to rotate so as to drive a rubber elastic button to repeatedly contact with a switch button of the electric detonator, the on-off of a warning lamp on the rubber elastic button is observed to record and observe the on-off of the rubber elastic button, the on-off of the lamp is observed to carry out actual debugging, the on-off of the lamp is observed, the electric detonator is clamped and fixed by pulling the sliding clamping mechanism, and the electric detonator is convenient to detach and fix, and operate.

Description

Detection device of aviation fire-extinguishing bottle electric detonator
Technical Field
The utility model relates to the technical field of fire extinguisher detection devices, in particular to a detection device of an electric detonator of an aviation fire extinguishing bottle.
Background
The fire extinguisher is a portable fire extinguishing tool. Chemical substances are placed in the fire extinguisher to rescue and extinguish the fire. Fire extinguishers are one of the common fire protection facilities, and are stored in public places or places where fire is likely to occur, and different types of fire extinguishers are filled with different components and are specially designed for different fires. When in use, care must be taken to avoid adverse effects and danger, the fire extinguisher is found to have problems by functional inspection, maintenance units with maintenance qualification must be entrusted to carry out maintenance, damaged parts are replaced, the cylinder body is subjected to hydrostatic test, and the fire extinguishing agent and driving gas are refilled
The prior patent (CN 206002603U) discloses an electric detonator detection device which comprises an electric detonator protection device, a bridge resistance measuring instrument and an insulation resistance measuring instrument; the bridge resistance measuring instrument comprises a bridge resistance measuring meter and a bridge resistance testing socket, wherein a first switch is connected between the bridge resistance measuring meter and the bridge resistance testing socket; the insulation resistance measuring instrument comprises an insulation resistance measuring instrument and an insulation resistance testing socket, and a second switch is connected between the insulation resistance measuring instrument and the insulation resistance testing socket; the second switch is also connected with an electric initiator protection device; the device also comprises a metering socket which is connected with the bridge resistance measuring meter and the insulation resistance measuring meter through a third switch.
The inventors found that the following problems exist in the prior art in the process of implementing the present utility model: most of the existing electric detonator detection devices only detect the resistance of the electric detonator, if a certain value is extremely qualified, or the electric detonator detection devices are observed according to the parameters marked on the electric detonator detection devices instead of actual detection, for example, the electric detonator detection devices in the comparison document only carry out numerical calculation by measuring the resistance of the electric detonator so as to achieve the purpose of detecting the electric detonator, and do not carry out actual test on the electric detonator, for example, the internal resistor fails in the actual use process, so that the electric detonator can be damaged and cannot be used, and therefore, the electric detonator detection devices need to be subjected to actual operation and debugging.
Disclosure of Invention
Aiming at the defects of the prior art, the utility model provides a detection device of an electric detonator of an aviation fire-extinguishing bottle, which solves the problems that most of the existing detection devices of the electric detonator only detect the resistance of the electric detonator, if a certain value is extremely qualified, or the electric detonator is observed according to the parameter marked on the electric detonator instead of actually detecting the electric detonator, only the numerical calculation is carried out, for example, the electric detonator detection device in a comparison document only carries out the numerical calculation and does not actually test the electric detonator by measuring the resistance of the electric detonator, and if the internal resistor fails in the actual use process, the electric detonator can be damaged and cannot be used, so that the electric detonator needs to be actually operated and debugged.
In order to achieve the above purpose, the utility model is realized by the following technical scheme: the utility model provides a detection device of aviation fire-extinguishing bottle electric detonator, includes the operation panel, the operation panel below is equipped with the supporting seat, supporting seat one side is equipped with the supporting seat, be equipped with circuit detection mechanism on the supporting seat, operation panel upper end one side is equipped with the motor case, operation panel upper end opposite side is equipped with the fluting, be equipped with trigger mechanism on the fluting, be equipped with sliding clamping mechanism under the fluting, be equipped with a pair of fastening mechanism on the supporting seat.
Preferably, the trigger mechanism comprises a contact plate, two pairs of connecting rods are arranged at the upper end of the operating platform, the contact plate is sleeved on the two pairs of connecting rods, a spring is sleeved between the contact plate and the operating platform and positioned on the contact plate, a rubber supporting seat is arranged at the upper end of the middle part of the contact plate, a rubber elastic button is arranged at the lower end of the middle part of the contact plate, a driving motor is arranged in the motor case, a rotating rod is fixedly connected with the driving end of the driving motor, a cam is fixedly connected with the other end of the rotating rod, and the cam is tightly attached to the rubber supporting seat.
Preferably, the sliding clamping mechanism comprises a pair of connecting blocks, the pair of connecting blocks are arranged at the lower end of the operating platform, a pair of sliding cavities are formed in the connecting blocks, a pair of sliding grooves are formed in the sliding cavities, a pair of L-shaped connecting rods are arranged in the sliding cavities, a pair of sliding blocks are arranged on the L-shaped connecting rods, the two pairs of sliding blocks are respectively and slidably inserted in the two pairs of the sliding grooves, connecting plates are arranged on opposite sides of the L-shaped connecting rods, clamping blocks are fixedly connected between the connecting plates, detection cavities are formed in the clamping blocks, a pair of supporting platforms are arranged on the inner wall surfaces of the detection cavities, and handles are arranged on the outer side wall surfaces of the clamping blocks.
Preferably, the fastening mechanism comprises a pair of knobs, a pair of threaded rods are fixedly connected to the knobs, the threaded rods are all arranged in the side walls of the supporting seat, pushing rods are connected to the other sides of the threaded rods in a rotating mode, fastening sliding blocks are arranged on two sides of the pushing rods, a pair of fastening sliding grooves are formed in two side walls of the supporting seat, the fastening sliding blocks are respectively and slidably inserted into the two pairs of fastening sliding grooves, and clamping plates are arranged on the other sides of the pushing rods.
Preferably, the circuit detection mechanism comprises a circuit support seat, the circuit support seat is arranged at the upper end of the support table, a circuit board is arranged in the circuit support seat, a pair of conducting strips, a warning lamp and a storage battery are arranged on the circuit board, a pair of conducting strips, the warning lamp and the storage battery are connected with a conducting wire, and the conducting wire is positioned in the circuit board.
Preferably, the supporting seat is of a U-shaped structure.
Advantageous effects
The utility model provides a detection device of an electric detonator of an aviation fire-extinguishing bottle, which is characterized in that a driving motor is started to drive a cam to rotate so as to drive a rubber elastic button to repeatedly contact a switch button of the electric detonator, so that a circuit board arranged in a circuit supporting seat below the circuit board is observed, the on-off of a warning lamp on the circuit board is observed to record and observe the electric detonator, the purpose of detecting the electric detonator is achieved, the electric detonator is actually debugged, the on-off of lamplight is observed, the electric detonator is detected, the electric detonator is clamped and fixed by pulling a sliding clamping mechanism, the electric detonator is convenient to detach and fix, and meanwhile, the electric detonator is fastened by a fastening mechanism arranged, so that the electric detonator is convenient to operate.
Drawings
Fig. 1 is a front view of the whole structure of a detection device of an electric detonator of an aviation fire bottle.
Fig. 2 is a side view of the whole structure of a detection device of an electric detonator of an aviation fire bottle.
Fig. 3 is a partial top view of a slide clamping mechanism of a detection device for an electric detonator of an aviation fire bottle.
Fig. 4 is a schematic diagram of a detection circuit of a detection device of an electric detonator of an aviation fire bottle.
In the figure: 1. an operation table; 2. a contact plate; 3. a support base; 4. a support table; 5. a motor case; 6. a cam; 7. a rubber support seat; 8. a rubber elastic button; 9. a connecting rod; 10. a spring; 11. a connecting block; 12. an L-shaped connecting rod; 13. a slide block; 14. a connecting plate; 15. a circuit support base; 16. a clamping block; 17. a knob; 18. a threaded rod; 19. a push rod; 20. a clamping plate; 21. a support platform; 22. a rotating lever; 23. and driving the motor.
Detailed Description
The following description of the embodiments of the present utility model will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present utility model, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the utility model without making any inventive effort, are intended to be within the scope of the utility model.
Referring to fig. 1-4, the present utility model provides a technical solution: the utility model provides a detection device of aviation fire-extinguishing bottle electric detonator, includes operation panel 1, operation panel 1 below is equipped with supporting seat 3, supporting seat 3 one side is equipped with supporting bench 4, be equipped with circuit detection mechanism on the supporting bench 4, operation panel 1 upper end one side is equipped with motor case 5, operation panel 1 upper end opposite side is equipped with the fluting, be equipped with trigger mechanism on the fluting, the fluting has sliding clamping mechanism down, be equipped with a pair of fastening mechanism on the supporting seat 3.
Further, trigger mechanism includes contact plate 2, the operation panel 1 upper end is equipped with two pairs of connecting rods 9, and two pairs the cover is equipped with on the connecting rod 9 contact plate 2, contact plate 2 with between the operation panel 1 and be located the cover and be equipped with spring 10, contact plate 2 middle part upper end is equipped with rubber supporting seat 7, contact plate 2 middle part lower extreme is equipped with rubber elastic button 8, be equipped with driving motor 23 in the motor case 5, driving motor 23 drive end fixedly connected with dwang 22, dwang 22 other end fixedly connected with cam 6, cam 6 with rubber supporting seat 7 closely pastes mutually.
Further, the slip fixture includes a pair of connecting block 11, a pair of connecting block 11 sets up operation panel 1 lower extreme, a pair of be equipped with the slip cavity in the connecting block 11, a pair of all be equipped with a pair of slip spout in the slip cavity, a pair of all be equipped with L type connecting rod 12 in the slip cavity, a pair of all be equipped with a pair of slider 13 on the L type connecting rod 12, two pairs slider 13 slip cartridge respectively in two pairs of slip spout, a pair of L type connecting rod 12 opposite side all is equipped with connecting plate 14, a pair of fixedly connected with grip block 16 between the connecting plate 14, be equipped with the detection cavity in the grip block 16, be equipped with a pair of supporting platform 21 on the detection cavity internal face, be equipped with the handle on the grip block 16 lateral wall face.
Further, the fastening mechanism comprises a pair of knobs 17, a pair of threaded rods 18 are fixedly connected to the knobs 17, the threaded rods 18 are arranged in the side walls of the supporting seat 3, push rods 19 are connected to the other sides of the threaded rods 18 in a rotating mode, fastening sliding blocks are arranged on two sides of the push rods 19, a pair of fastening sliding grooves are formed in two side walls of the supporting seat 3, the two pairs of fastening sliding blocks are respectively and slidably inserted into the two pairs of fastening sliding grooves, and clamping plates 20 are arranged on the other sides of the push rods 19.
Further, the circuit detection mechanism comprises a circuit supporting seat 15, the circuit supporting seat 15 is arranged at the upper end of the supporting table 4, a circuit board is arranged in the circuit supporting seat 15, a pair of conducting strips, a warning lamp and a storage battery are arranged on the circuit board, a pair of conducting strips, the warning lamp and the storage battery are connected with a conducting wire, and the conducting wire is located in the circuit board.
Further, the supporting seat 3 has a U-shaped structure.
The following components are of the present case:
the detailed connection means are known in the art, and the following mainly describes the working principle and process, and the specific work is as follows.
Examples: when the electric detonator of the aviation fire-extinguishing bottle needs to be detected, firstly, the handle on the clamping block 16 can be pulled out to further drive the connecting plates 14 fixed on two sides of the clamping block 16 to be provided with the L-shaped connecting rods 12, further drive the pair of sliding blocks 13 arranged at the upper ends of the pair of L-shaped connecting rods 12 to slide in the pair of connecting blocks 11, thereby enabling the clamping block 16 to slide out, afterwards placing the electric detonator on the pair of supporting platforms 21, pushing back the clamping block 16, enabling positive and negative wires at the lower ends of the electric detonator to be respectively contacted with the conductive sheets, enabling the buttons at the upper ends to be opposite to the lower ends of the rubber elastic buttons 8, then screwing the pair of knobs 17, further driving the threaded rods 18 to rotate, further driving the pushing rods 19 to move, enabling the pair of sliding blocks arranged on the pushing rods to slide in the pair of sliding grooves respectively, further driving the clamping plates 20 to clamp the pair of L-shaped connecting rods 12, thereby achieving the purpose of fastening the positions of the clamping block 16, afterwards starting the driving motor 23 arranged in the motor box 5 on the operating platform 1, further enabling the driving end thereof to drive the rotating rods 22 to rotate, further driving the clamping block 16 arranged on the electric detonator to rotate, further driving the electric detonator to be in contact with the rubber supporting plate 6 to be in contact with the electric detonator to be closely contacted with the rubber supporting plate 7, and simultaneously, and enabling the electric detonator to be closely contacted with the rubber supporting plate 2 to be closely arranged under the supporting plate 2 to be in contact with the electric detonator seat 2, and the electric detonator to be closely contacted with the electric detonator seat, and the electric detonator is closely arranged under the electric conduit 2, and then, and the electric conduit is in contact with the electric conduit is closely and placed under the electric conduit, and observed, and then, and the electric conduit is placed under the electric conduit and observed.
It is noted that relational terms such as first and second, and the like are used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions.

Claims (6)

1. The utility model provides a detection device of aviation fire-extinguishing bottle electric detonator, includes operation panel (1), its characterized in that, operation panel (1) below is equipped with supporting seat (3), supporting seat (3) one side is equipped with supporting bench (4), be equipped with circuit detection mechanism on supporting bench (4), operation panel (1) upper end one side is equipped with motor case (5), operation panel (1) upper end opposite side is equipped with the fluting, be equipped with trigger mechanism on the fluting, be equipped with sliding clamping mechanism under the fluting, be equipped with a pair of fastening mechanism on supporting bench (3).
2. The detection device of the aviation fire-extinguishing bottle electric detonator according to claim 1, characterized in that the triggering mechanism comprises a contact plate (2), two pairs of connecting rods (9) are arranged at the upper end of the operating platform (1), the contact plate (2) is sleeved on the two pairs of connecting rods (9), a spring (10) is sleeved between the contact plate (2) and the operating platform (1) and is positioned on the upper part, a rubber supporting seat (7) is arranged at the upper end of the middle part of the contact plate (2), a rubber elastic button (8) is arranged at the lower end of the middle part of the contact plate (2), a driving motor (23) is arranged in the motor box (5), a rotating rod (22) is fixedly connected to the driving end of the driving motor, a cam (6) is fixedly connected to the other end of the rotating rod (22), and the cam (6) is tightly attached to the rubber supporting seat (7).
3. The detection device of the aviation fire-extinguishing bottle electric primer according to claim 1, wherein the sliding clamping mechanism comprises a pair of connecting blocks (11), the pair of connecting blocks (11) are arranged at the lower end of the operating platform (1), a pair of sliding cavities are arranged in the connecting blocks (11), a pair of sliding grooves are formed in the pair of sliding cavities, L-shaped connecting rods (12) are arranged in the pair of sliding cavities, a pair of sliding blocks (13) are arranged on the pair of L-shaped connecting rods (12), the two pairs of sliding blocks (13) are respectively and slidably inserted in the two pairs of sliding grooves, connecting plates (14) are arranged on opposite sides of the pair of L-shaped connecting rods (12), clamping blocks (16) are fixedly connected between the pair of connecting plates (14), detection cavities are arranged in the clamping blocks (16), a pair of supporting platforms (21) are arranged on the inner wall surfaces of the detection cavities, and handles are arranged on the outer side walls of the clamping blocks (16).
4. The detection device of the aviation fire-extinguishing bottle electric primer according to claim 1, wherein the fastening mechanism comprises a pair of knobs (17), a pair of threaded rods (18) are fixedly connected to the knobs (17), the threaded rods (18) are all arranged in the side walls of the supporting seat (3), pushing rods (19) are screwed on the other sides of the threaded rods (18), fastening sliding blocks are arranged on two sides of the pushing rods (19), a pair of fastening sliding grooves are formed in two side walls of the supporting seat (3), the two pairs of fastening sliding blocks are respectively and slidably inserted in the two pairs of fastening sliding grooves, and clamping plates (20) are arranged on the other sides of the pushing rods (19).
5. The device for detecting the electric detonator of the aviation fire-extinguishing bottle according to claim 1, wherein the circuit detection mechanism comprises a circuit supporting seat (15), the circuit supporting seat (15) is arranged at the upper end of the supporting table (4), a circuit board is arranged in the circuit supporting seat (15), a pair of conducting sheets, a warning lamp and a storage battery are arranged on the circuit board, a wire is connected between the pair of conducting sheets, the warning lamp and the storage battery, and the wire is positioned in the circuit board.
6. The device for detecting the electric detonator of the aviation fire extinguishing bottle according to claim 1, wherein the supporting seat (3) is of a U-shaped structure.
CN202320179886.5U 2023-02-10 2023-02-10 Detection device of aviation fire-extinguishing bottle electric detonator Active CN219348995U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202320179886.5U CN219348995U (en) 2023-02-10 2023-02-10 Detection device of aviation fire-extinguishing bottle electric detonator

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202320179886.5U CN219348995U (en) 2023-02-10 2023-02-10 Detection device of aviation fire-extinguishing bottle electric detonator

Publications (1)

Publication Number Publication Date
CN219348995U true CN219348995U (en) 2023-07-14

Family

ID=87098357

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202320179886.5U Active CN219348995U (en) 2023-02-10 2023-02-10 Detection device of aviation fire-extinguishing bottle electric detonator

Country Status (1)

Country Link
CN (1) CN219348995U (en)

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