An intelligent civil air defense emergency control system

Abstract

The present invention relates to the field of civil air defense engineering technology, and in particular to an intelligent civil air defense emergency control system, comprising a support platform, and a monitor and a support frame arranged on the upper end surface of the support platform, wherein a first conducting mechanism and a second conducting mechanism are relatively arranged on the support frame, and the first conducting mechanism, the second conducting mechanism, the monitor and the backup power supply form a series circuit, and a blocking mechanism is also arranged on the support frame, and the blocking mechanism is arranged between the first conducting mechanism and the second conducting mechanism. An electromagnet mechanism is arranged on the upper end surface of the support platform, and the electromagnet mechanism is arranged directly below the blocking mechanism; the present invention improves the structure of the existing intelligent civil air defense control system, and the improved intelligent civil air defense emergency control system can intelligently start and stop working equipment in areas where local lines are damaged, thereby avoiding the occurrence of safety hazards.

Description

Technical Field

[0001] The present invention relates to the technical field of civil air defense engineering, and in particular to an intelligent civil air defense emergency control system. Background Art

[0002] Civil air defense projects are important national protection projects, which are composed of command projects, communication projects, personnel concealment projects, material concealment projects, etc. Among them, personnel shelter projects are mainly used for personnel shelter under air raid conditions during wartime. In order to have a basic environment suitable for the survival and living of sheltered personnel inside the project, ventilation inside and outside the project must be guaranteed in normal use. In the event of enemy nuclear attacks and biological and chemical attacks, the problem of air filtration and elimination of radioactive contamination should also be solved.

[0003] There are many ventilation equipment, air conditioning, air humidification and various environmental conditioning equipment installed in the civil air defense project. Various equipment are distributed. The larger the area of ​​the civil air defense project, the more equipment needs to be connected. Centralized control of the equipment will lead to confusion in the connection lines, which will cause local lines to be damaged. Repair and replacement are extremely inconvenient, which directly leads to the inability of equipment in the area where the local lines are damaged to work quickly, which will cause safety hazards due to the failure of the equipment to work normally. Therefore, there is an urgent need for an emergency control device that can quickly restart the equipment when the local lines are damaged. Summary of the invention

[0004] To achieve the above-mentioned objectives, the present invention provides an intelligent civil air defense emergency control system, comprising a support platform, and a monitor and a support frame arranged on the upper end surface of the support platform, wherein a first conduction mechanism and a second conduction mechanism are relatively arranged on the support frame, and the first conduction mechanism, the second conduction mechanism, the monitor and the backup power supply form a series circuit, and a blocking mechanism is also arranged on the support frame, and the blocking mechanism is arranged between the first conduction mechanism and the second conduction mechanism. An electromagnet mechanism is arranged on the upper end surface of the support platform, and the electromagnet mechanism is arranged directly below the blocking mechanism. During operation, when the monitor is powered off, the blocking mechanism moves upward, the first conduction mechanism and the second conduction mechanism move toward each other and contact, and the monitor is turned on again.

[0005] Optionally, the second conducting mechanism includes a first electrode contact, a first wire is arranged on the side wall of the first electrode contact, the first electrode contact is fixedly arranged on an L-shaped plate, a guide rod is fixedly connected to the side wall of the L-shaped plate, the guide rod is movably inserted into the side plate of the support frame, a support spring is wound around the outside of the guide rod, one end of the support spring is fixedly connected to the side wall of the L-shaped plate, and the other end of the support spring is fixedly connected to the side wall of the support frame, wherein the structure of the first conducting mechanism is consistent with that of the second conducting mechanism.

[0006] Optionally, the blocking mechanism includes a blocking ball assembly, a first guide assembly is connected to the upper end surface of the blocking ball assembly, the upper end of the first guide assembly is connected to the top plate of the support frame, the first guide assembly includes a first guide rod, a first guide cylinder and a first guide spring, the first guide rod is movably inserted in the first guide cylinder, the first guide spring is wound and arranged outside the first guide rod, the two ends of the first guide spring are respectively fixedly connected to the side wall of the first guide rod and the outer side wall of the first guide cylinder, the first guide rod is connected to the blocking ball assembly, and the first guide cylinder is connected to the support frame.

[0007] Optionally, the electromagnet mechanism includes an electromagnet body disposed directly below the blocking ball assembly, a second wire being connected to the side wall of the electromagnet body, a horizontal plate being fixedly connected to the side wall of the electromagnet body, a vertical plate being fixedly connected to the lower end surface of the horizontal plate, and a lower end of the vertical plate being fixedly connected to the upper end surface of the support platform.

[0008] Optionally, the blocking ball assembly includes a rubber ball, which is provided with a first through hole and a second through hole, the first through hole and the second through hole are connected to each other, the cavity size of the first through hole is smaller than the cavity size of the second through hole, a magnet rod is movably inserted in the first through hole and the second through hole, a connecting spring is wrapped around the outside of the magnet rod, two ends of the connecting spring are respectively fixedly connected to the side wall of the magnet rod and the rubber ball, the upper end of the magnet rod is fixedly connected to the first connecting column, the upper end of the first connecting column is fixedly connected to the second connecting column, the second connecting column and the first connecting column are movably arranged in the second through hole, and the second connecting column is fixedly connected to the first guide rod.

[0009] Optionally, a locking mechanism is also included, which includes a movable plate, two locking rods are connected to the side wall of the movable plate, a locking groove matching the locking rod is provided on the first electrode contact piece, a push-pull rod is hinged on the side wall of the movable plate, the push-pull rod is movably arranged in a third through hole, the third through hole is provided on the rubber ball, and one end of the push-pull rod away from the movable plate is hinged on the side wall of the magnet rod.

[0010] Optionally, the locking mechanism also includes a second guide assembly, one end of the second guide assembly is connected to the movable plate, the other end of the second guide assembly is connected to the rubber ball, the second guide assembly includes a second guide rod, a second guide cylinder and a first guide spring, the second guide rod is movably inserted in the second guide cylinder, the first guide spring is wound and arranged outside the second guide rod, the two ends of the first guide spring are respectively fixedly connected to the side wall of the second guide rod and the outer side wall of the second guide cylinder, the second guide rod is fixedly connected to the movable plate, and the second guide cylinder is fixedly connected to the rubber ball.

[0011] Optionally, it also includes a fastening mechanism for connecting the locking rod and the movable plate, the fastening mechanism includes a threaded groove opened on the outside of the locking rod, the locking rod is threadedly inserted in the internal threaded coil through the threaded groove, the internal threaded coil is fixedly set on the rotating shaft, the rotating shaft is rotatably set on the sliding block, the sliding block is slidably set in the sliding groove, the sliding groove is opened on the movable plate, one end of the locking rod located in the internal threaded coil is fixedly connected to the first spring, the free end of the first spring is fixedly connected to the side wall of the sliding block, one end of the pulling wire is fixedly connected to the outer side wall of the internal threaded coil, the other end of the pulling wire is fixedly connected to the fixed block, and the fixed block is fixedly set on the side wall of the movable plate.

[0012] Optionally, the fastening mechanism also includes a third guide assembly, which includes a third guide rod, a third guide cylinder and a third guide spring. The third guide rod is movably inserted in the third guide cylinder, and the third guide spring is wound outside the third guide rod, and both ends of the third guide spring are respectively fixedly connected to the side wall of the third guide rod and the outer side wall of the third guide cylinder, the third guide rod is fixedly connected to the sliding block, and the third guide cylinder is fixedly connected to the side wall of the sliding groove.

[0013] Optionally, it also includes a third conduction mechanism, which includes a supporting tray that is arranged to be in contact with the magnet rod, a vertical rod is fixedly connected to the lower end surface of the supporting tray, the vertical rod is movably inserted in a fourth through hole, the fourth through hole is opened on the horizontal plate, a horizontal rod is fixedly connected to the side wall of the horizontal plate, the free end of the horizontal rod is fixedly connected to the side wall of the L-shaped plate, a rubber plug is provided on the outer fixed sleeve of the vertical rod, the rubber plug is a truncated cone structure, the rubber plug is movably inserted in the fourth through hole, a second electrode contact is provided on the outer fixed sleeve of the vertical rod, the lower end of the second electrode contact is in contact with a third electrode contact, and the third electrode contact is fixedly provided on the upper end surface of the horizontal plate.

[0014] The beneficial effects of the present invention are as follows: The present invention improves the structure of the existing intelligent civil air defense control system. The improved intelligent civil air defense emergency control system is provided with a combination structure of a first conducting mechanism, a second conducting mechanism, a blocking mechanism and a backup power supply. The setting of the combination structure can intelligently start and stop working equipment in areas where local lines are damaged, thereby avoiding the occurrence of safety hazards. BRIEF DESCRIPTION OF THE DRAWINGS

[0015] Figure 1 This is a schematic diagram of the structure of an embodiment of the intelligent civil air defense emergency control system of the present invention; Figure 2 The intelligent civil air defense emergency control system of the present invention Figure 1 A schematic diagram of the enlarged structure in the middle; Figure 3 This is a structural schematic diagram of a blocking component of an intelligent civil air defense emergency control system of the present invention; Figure 4 It is a structural schematic diagram of the locking mechanism in the intelligent civil air defense emergency control system of the present invention; Figure 5 The intelligent civil air defense emergency control system of the present invention Figure 4 The first partial cross-sectional structure schematic diagram is shown in the middle left view; Figure 6 The intelligent civil air defense emergency control system of the present invention Figure 4 The second partial cross-sectional structure schematic diagram is shown in the middle left view; Figure 7 The intelligent civil air defense emergency control system of the present invention Figure 6 Middle B is an enlarged schematic diagram of the structure; Figure 8 It is a structural schematic diagram of the third conduction mechanism in the intelligent civil air defense emergency control system of the present invention; Fig. 9 The intelligent civil air defense emergency control system of the present invention Figure 8 Enlarged schematic diagram of the C structure in the middle.

[0016] Description of Reference Numerals Support table 1, monitor 2, support frame 3, first conduction mechanism 4, second conduction mechanism 5, first electrode contact sheet 51, first wire 52, L-shaped plate 53, guide rod 54, support spring 55, blocking mechanism 6, blocking ball assembly 61, rubber ball 611, first through hole 612, second through hole 613, magnet rod 614, connecting spring 615, first connecting column 616, second connecting column 617, first guide assembly 62, first guide rod 621, first guide cylinder 622, first guide spring 623, electromagnet mechanism 7, electromagnet body 71, second wire 72, horizontal plate 73, vertical plate 74, locking mechanism 8, moving plate 81, locking rod 82, locking groove 83, second guide assembly 84, second guide rod 841, second guide cylinder 842, first guide spring 843, push-pull rod 85, third through hole 86, fastening mechanism 9, threaded groove 91, internal threaded spiral tube 92, rotating shaft 93, sliding block 94, first spring 95, sliding groove 96, pulling wire 97, fixing block 98, third guide assembly 99, third guide rod 991, third guide cylinder 992, third guide spring 993, third conduction mechanism 10, supporting tray 101, vertical rod 102, fourth through hole 103, rubber plug 104, second electrode contact piece 105, third electrode contact piece 106, horizontal plate 107, horizontal rod 108. DETAILED DESCRIPTION

[0017] In order to make the purpose, technical solutions and advantages of the present invention clearer, the technical solutions in the embodiments of the present invention will be clearly and completely described below in conjunction with the drawings of the present invention. Obviously, the described embodiments are part of the embodiments of the present invention, rather than all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the present invention. Unless otherwise defined, the technical terms or scientific terms used herein should be understood by people with general skills in the field to which the present invention belongs. "Including" and similar words used in this article mean that the elements or objects appearing before the word include the elements or objects listed after the word and their equivalents, without excluding other elements or objects.

[0018] In view of the problems existing in the prior art, the embodiments of the present invention provide an intelligent civil air defense emergency control system, such as Figure 1As shown, the intelligent civil air defense emergency control system includes a support platform 1, and a monitor 2 and a support frame 3 arranged on the upper end surface of the support platform 1. The monitor 2 is used to monitor the area in real time. When a line fails, the monitor 2 will be powered off and stop working, and the area cannot be monitored at this time. The support frame 3 is relatively provided with a first conduction mechanism 4 and a second conduction mechanism 5. The first conduction mechanism 4, the second conduction mechanism 5, the monitor 2 and the backup power supply form a series circuit. The support frame 3 is also provided with a blocking mechanism 6, and the blocking mechanism 6 is arranged between the first conduction mechanism 4 and the second conduction mechanism 5. The upper end surface of the support platform 1 is provided with an electromagnet mechanism 7, and the electromagnet mechanism 7 is arranged directly below the blocking mechanism 6. When working, when the monitor 2 is powered off, the blocking mechanism 6 moves upward, the first conduction mechanism 4 and the second conduction mechanism 5 move toward each other and contact, and the monitor 2 is turned on again.

[0019] It should be understood that when there is no fault in the line, the blocking mechanism 6 will exist between the first conducting mechanism 4 and the second conducting mechanism 5, so that the series circuit composed of the first conducting mechanism 4, the second conducting mechanism 5, the monitor 2 and the backup power supply is in a disconnected state, and the monitor 2 stops working; when a fault occurs in the line, the blocking mechanism 6 moves upward and loses the blocking of the first conducting mechanism 4 and the second conducting mechanism 5. At this time, the first conducting mechanism 4 and the second conducting mechanism 5 are in contact, and the series circuit composed of the first conducting mechanism 4, the second conducting mechanism 5, the monitor 2 and the backup power supply is in a connected state, and the monitor 2 restarts to work.

[0020] In one embodiment, Figure 2 As shown, the second conducting mechanism 5 includes a first electrode contact sheet 51, a first wire 52 is arranged on the side wall (which can be understood as the rear side wall) of the first electrode contact sheet 51, the first electrode contact sheet 51 is fixedly arranged on an L-shaped plate 53, a guide rod 54 is fixedly connected to the side wall (which can be understood as the right side wall) of the L-shaped plate 53, the guide rod 54 is movably plugged into the side plate of the support frame 3, a support spring 55 is wound around the guide rod 54, one end (which can be understood as the left end) of the support spring 55 is fixedly connected to the side wall (which can be understood as the right side wall) of the L-shaped plate 53, and the other end (which can be understood as the right end) of the support spring 55 is fixedly connected to the side wall of the support frame 3, wherein the first conducting mechanism 4 has the same structure as the second conducting mechanism 5. In the present invention, only the structure of the second conducting mechanism 5 is described in detail, and the detailed structure of the first conducting mechanism 4 is not repeated.

[0021] During operation, when the circuit is not damaged, the blocking mechanism 6 is arranged between the two first electrode contact pieces 51, and the blocking mechanism 6 will form a resistance to the first electrode contact piece 51. At this time, the support spring 55 is in a compressed state. When the circuit is damaged, the blocking mechanism 6 moves upward to disengage from the first electrode contact piece 51. At this time, under the push of the support spring 55, the first conduction mechanism 4 and the second conduction mechanism 5 move toward each other. At this time, the two first electrode contact pieces 51 will contact, so that the series circuit composed of the first conduction mechanism 4, the second conduction mechanism 5, the monitor 2 and the backup power supply is in a connected state, and the monitor 2 restarts to work.

[0022] In one embodiment, Figure 2 As shown, the blocking mechanism 6 includes a blocking ball assembly 61. A first guide assembly 62 is connected to the upper end surface of the blocking ball assembly 61, and the upper end of the first guide assembly 62 is connected to the top plate of the support frame 3. In this example, the blocking ball assembly 61 is arranged between the two first electrode contact sheets 51, and the first guide assembly 62 is arranged above the two first electrode contact sheets 51. The arrangement of the first guide assembly 62 can enable the blocking ball assembly 61 to move upward or downward in the vertical direction. The first guide assembly 62 includes a first guide rod 621, a first guide cylinder 622 and a first guide spring 623. The first guide rod 621 is movably inserted in the first guide cylinder 622, and the first guide spring 623 is wound and arranged outside the first guide rod 621. The two ends of the first guide spring 623 are respectively fixedly connected to the side wall of the first guide rod 621 and the outer side wall of the first guide cylinder 622. The first guide rod 621 is connected to the blocking ball assembly 61, and the first guide cylinder 622 is connected to the support frame 3.

[0023] In one embodiment, Figure 3 As shown, the blocking ball assembly 61 includes a rubber ball 611, and the rubber ball 611 is provided with a first through hole 612 and a second through hole 613. The first through hole 612 and the second through hole 613 are arranged in communication with each other, and the cavity size of the first through hole 612 (which can be understood as the aperture of the cavity) is smaller than the cavity size of the second through hole 613. The first through hole 612 is arranged below the second through hole 613. Figure 3In the example, a step is formed at the connection between the first through hole 612 and the second through hole 613. Preferably, the first through hole 612 and the second through hole 613 are vertically arranged. A magnet rod 614 is movably inserted in the first through hole 612 and the second through hole 613. A connecting spring 615 is wound around the outside of the magnet rod 614. The two ends of the connecting spring 615 are respectively fixedly connected to the side wall of the magnet rod 614 and the rubber ball 611. The upper end of the magnet rod 614 is fixedly connected to a first connecting column 616. The diameter of the first connecting column 616 is larger than the aperture of the first through hole 612. The upper end of the first connecting column 616 is fixedly connected to a second connecting column 617. The second connecting column 617 and the first connecting column 616 are movably arranged in the second through hole 613. The second connecting column 617 is fixedly connected to the first guide rod 621.

[0024] The arrangement of this embodiment can protect the first electrode contact piece 51 through the buffering effect. Specifically, when the rubber ball 611 moves downward and contacts the two first electrode contact pieces 51 to move away from each other, the rubber ball 611 will collide with the first electrode contact piece 51 at the moment of contact. The existence of this impact force will cause the first electrode contact piece 51 to be damaged. The arrangement of the blocking ball assembly 61 in the present invention can effectively buffer the impact force. Specifically, when the rubber ball 611 hits the first electrode contact piece 51, the magnet rod 614 will move downward relative to the rubber ball 611. At this time, the connecting spring 615 is stretched. During the stretching process, the connecting spring 615 avoids the rigid collision between the rubber ball 611 and the first electrode contact piece 51. By having a certain buffer distance, the first electrode contact piece 51 is protected.

[0025] In one embodiment, Figure 2 As shown, the electromagnet mechanism 7 includes an electromagnet body 71 arranged directly below the blocking ball assembly 61, a second wire 72 is connected to the side wall of the electromagnet body 71, a horizontal plate 73 is fixedly connected to the side wall of the electromagnet body 71, a vertical plate 74 is fixedly connected to the lower end surface of the horizontal plate 73, and the lower end of the vertical plate 74 is fixedly connected to the upper end surface of the support platform 1.

[0026] During operation, when the circuit is not damaged, the electromagnet body 71 is powered on to generate magnetism. Under the action of magnetic attraction, the magnet rod 614 will be attracted to move the rubber ball 611 downward, so that the rubber ball 611 moves between the two first electrode contacts 51, which is used to isolate the contact between the two first electrode contacts 51, so that the series circuit is not connected. When the circuit is damaged, the electromagnet body 71 is powered off and loses its magnetism. At this time, under the pulling of the first guide component 62, the rubber ball 611 moves upward to reset, so that the rubber ball 611 moves above the two first electrode contacts 51. At this time, the first electrode contacts 51 lose the resistance of the rubber ball 611, and the support spring 55 pushes the two first electrode contacts 51 to move toward each other through the L-shaped plate 53. When the two first electrode contacts 51 are in contact, the series circuit is connected, and the monitor 2 restarts.

[0027] When the rubber ball 611 is placed between the two first electrode contact sheets 51, in order to prevent the two first electrode contact sheets 51 from moving relative to the rubber ball 611, in one embodiment, as shown in FIG. Figure 4 and Figure 5 As shown, the intelligent civil air defense emergency control system also includes a locking mechanism 8, which includes a movable plate 81, and two locking rods 82 are connected to the side wall (which can be understood as the rear side wall) of the movable plate 81. A locking groove 83 matching the locking rod 82 is provided on the first electrode contact sheet 51, and a push-pull rod 85 is hinged on the side wall of the movable plate 81. The push-pull rod 85 is movably arranged in a third through hole 86, and the third through hole 86 is provided on the rubber ball 611. The end of the push-pull rod 85 away from the movable plate 81 is hinged (which can be understood as the lower end) on the side wall of the magnet rod 614.

[0028] During operation, when the rubber ball 611 is suspended between the two first electrode contact pieces 51, with the magnetic adsorption of the electromagnet body 71, the magnet rod 614 will continue to move downward relative to the rubber ball 611. At this time, the downward movement of the magnet rod 614 will pull the movable plate 81 toward the rubber ball 611 through the push-pull rod 85. The movement of the movable plate 81 will bring the locking rod 82 into the locking groove 83. It should be noted that the number of locking rods 82 is set to two, and the two locking rods 82 are respectively inserted into the locking grooves 83 set on the two first electrode contact pieces 51. At this time, the locking effect of the two locking rods 82 will lock the rubber ball 611 between the two first electrode contact pieces 51 to prevent the two first electrode contact pieces 51 from moving relative to the rubber ball 611.

[0029] In one embodiment, Figure 5As shown, the locking mechanism 8 also includes a second guide assembly 84, one end of which is connected to the moving plate 81, and the other end of which is connected to the rubber ball 611. The second guide assembly 84 includes a second guide rod 841, a second guide cylinder 842 and a first guide spring 843. The second guide rod 841 is movably inserted in the second guide cylinder 842, and the first guide spring 843 is wound and arranged outside the second guide rod 841. The two ends of the first guide spring 843 are respectively fixedly connected to the side wall of the second guide rod 841 and the outer side wall of the second guide cylinder 842. The second guide rod 841 is fixedly connected to the moving plate 81, and the second guide cylinder 842 is fixedly connected to the rubber ball 611. The setting of the second guide assembly 84 in this embodiment can not only play the role of guiding support for the movement of the moving plate 81, so that the moving plate 81 can only move closer to or away from the rubber ball 611, but also provide a reset force for the reset process of the moving plate 81 when the moving plate 81 is reset.

[0030] In order to allow the locking rod 82 to be inserted into the locking groove 83, the diameter of the locking rod 82 is set to be smaller than the groove cavity diameter of the locking groove 83. In this way, after the locking rod 82 is inserted into the locking groove 83, there is still a gap, which causes the two first electrode contact sheets 51 to still shake slightly relative to the rubber ball 611. In order to solve the above problem, in one embodiment, as shown in FIG. Figure 6 and Figure 7 As shown, the intelligent civil air defense emergency control system also includes a fastening mechanism 9 for connecting the locking rod 82 and the movable plate 81, and the fastening mechanism 9 is used to pull the two locking rods 82 to move closer to each other, so that the locking rod 82 and the locking groove 83 fit more closely, and at the same time, through the clamping of the two locking rods 82, the two first electrode contact sheets 51 and the rubber ball 611 remain stationary. The fastening mechanism 9 includes a threaded groove 91 opened on the outside of the locking rod 82, and the locking rod 82 is threadedly inserted in the internal threaded coil 92 through the threaded groove 91. The internal threaded coil 92 is fixedly set on a rotating shaft 93, and the rotating shaft 93 is rotatably set on a sliding block 94. The sliding block 94 is slidably set in a sliding groove 96, and the sliding groove 96 is opened on the movable plate 81. One end of the locking rod 82 located in the internal threaded coil 92 is fixedly connected to a first spring 95, and the free end of the first spring 95 is fixedly connected to the side wall of the sliding block 94. One end of a pulling wire 97 is fixedly connected to the outer side wall of the internal threaded coil 92, and the other end of the pulling wire 97 is fixedly connected to a fixed block 98, and the fixed block 98 is fixedly set on the side wall of the movable plate 81.

[0031] During operation, after the locking rod 82 hits the right side wall of the locking groove 83, as the moving plate 81 continues to move to the right, the internal threaded coil 92 will move to the right relative to the locking rod 82. Due to the limitation of the first spring 95, the locking rod 82 can only move in the horizontal direction and cannot rotate. Since the locking rod 82 is threadedly inserted in the internal threaded coil 92, the internal threaded coil 92 will rotate relative to the locking rod 82 during the movement to the right. The rotation of the internal threaded coil 92 will cause the pulling wire 97 to be entangled. In this winding process, the two locking rods 82 will move closer to each other through the combined structure of the internal threaded coil 92, the rotating shaft 93 and the sliding block 94, so that the locking rod 82 and the wall of the locking groove 83 are more closely fitted, so that the two first electrode contacts 51 clamp the rubber ball 611 more firmly.

[0032] In one embodiment, Figure 7 As shown, the fastening mechanism 9 also includes a third guide assembly 99, which includes a third guide rod 991, a third guide cylinder 992 and a third guide spring 993. The third guide rod 991 is movably inserted in the third guide cylinder 992, and the third guide spring 993 is wound outside the third guide rod 991, and the two ends of the third guide spring 993 are respectively fixedly connected to the side wall of the third guide rod 991 and the outer side wall of the third guide cylinder 992, the third guide rod 991 is fixedly connected to the sliding block 94, and the third guide cylinder 992 is fixedly connected to the side wall of the sliding groove 96. The setting of the third guide assembly 99 in this embodiment can not only play a role of guiding support for the movement of the sliding block 94, but also provide a reset force for the reset process of the sliding block 94.

[0033] In one embodiment, Figure 8 and Fig. 9 As shown, the intelligent civil air defense emergency control system also includes a third conduction mechanism 10. The third conducting mechanism 10 includes a supporting tray 101 which is arranged to be in contact with the magnet rod 614, a vertical rod 102 is fixedly connected to the lower end surface of the supporting tray 101, the vertical rod 102 is movably inserted in the fourth through hole 103, the fourth through hole 103 is provided on the horizontal plate 107, a horizontal rod 108 is fixedly connected to the side wall of the horizontal plate 107, the free end of the horizontal rod 108 is fixedly connected to the side wall of the L-shaped plate 53, a rubber plug 104 is fixedly sleeved outside the vertical rod 102, the rubber plug 104 is a truncated cone structure, the rubber plug 104 is movably inserted in the fourth through hole 103, a second electrode contact 105 is fixedly sleeved outside the vertical rod 102, the lower end of the second electrode contact 105 is in contact with the third electrode contact 106, and the third electrode contact 106 is fixedly arranged on the upper end surface of the horizontal plate 107.

[0034] The third conduction mechanism 10 is provided for further intelligent control of the circuit. Specifically, the second electrode contact piece 105, the third electrode contact piece 106, the two first electrode contact pieces 51, the monitor 2 and the backup power supply form a series circuit. The third conduction mechanism 10 is specifically provided to prevent the monitor 2 from being connected to the backup power supply when the two first electrode contact pieces 51 are in contact when the electromagnet body 71 is not powered on in the initial stage of installation. Specifically, during installation, the second electrode contact 105 and the third electrode contact 106 are not in contact. Even if the two first electrode contacts 51 are in contact, the monitor 2 will still not be connected to the backup power supply. As the electromagnet body 71 is powered on, the magnetic attraction generated during the downward movement of the magnet rod 614 will resist the downward movement of the supporting tray 101. The downward movement of the supporting tray 101 will carry the second electrode contact 105 downward through the vertical rod 102 and resist the third electrode contact 106. At this time, when the circuit is damaged, the electromagnet body 71 is powered off, the rubber ball 611 moves upward, and the two first electrode contacts 51 will contact each other. At this time, the series circuit composed of the two first electrode contacts 51, the monitor 2, the second electrode contact 105, the third electrode contact 106 and the monitor 2 is connected, and the monitor 2 restarts and starts working.

[0035] In this embodiment, the provision of the rubber plug 104 can lock the contact state of the second electrode contact 105 and the third electrode contact 106 so that the second electrode contact 105 and the third electrode contact 106 will not be separated. Specifically, when the second electrode contact 105 and the third electrode contact 106 are in contact with each other, the rubber plug 104 is firmly plugged in the fourth through hole 103.

[0036] Although the embodiments of the present invention are described in detail above, it is obvious to those skilled in the art that various modifications and variations can be made to these embodiments. However, it should be understood that such modifications and variations are within the scope and spirit of the present invention. Moreover, the present invention described herein may have other embodiments and may be implemented or realized in a variety of ways.

Claims

1. An intelligent civil air defense emergency control system, characterized in that: The invention comprises a support platform (1), a monitor (2) and a support frame (3) arranged on the upper end surface of the support platform (1); a first conduction mechanism (4) and a second conduction mechanism (5) are arranged on the support frame (3) in a relative manner; the first conduction mechanism (4), the second conduction mechanism (5), the monitor (2) and a backup power supply form a series circuit; a blocking mechanism (6) is also arranged on the support frame (3); the blocking mechanism (6) is arranged between the first conduction mechanism (4) and the second conduction mechanism (5); an electromagnet mechanism (7) is arranged on the upper end surface of the support platform (1); the electromagnet mechanism (7) is arranged directly below the blocking mechanism (6); when the monitor (2) is powered off during operation, the blocking mechanism (6) moves upward, the first conduction mechanism (4) and the second conduction mechanism (5) move toward each other and contact each other, and the monitor (2) is turned on again.

2. The intelligent civil air defense emergency control system according to claim 1 is characterized in that: The second conducting mechanism (5) comprises a first electrode contact sheet (51), a first wire (52) is arranged on the side wall of the first electrode contact sheet (51), the first electrode contact sheet (51) is fixedly arranged on an L-shaped plate (53), a guide rod (54) is fixedly connected to the side wall of the L-shaped plate (53), the guide rod (54) is movably plugged into the side plate of the support frame (3), a support spring (55) is wound around the outside of the guide rod (54), one end of the support spring (55) is fixedly connected to the side wall of the L-shaped plate (53), and the other end of the support spring (55) is fixedly connected to the side wall of the support frame (3), wherein the first conducting mechanism (4) has the same structure as the second conducting mechanism (5).

3. The intelligent civil air defense emergency control system according to claim 2 is characterized in that: The blocking mechanism (6) comprises a blocking ball assembly (61), the upper end surface of the blocking ball assembly (61) is connected to a first guide assembly (62), the upper end of the first guide assembly (62) is connected to the top plate of the support frame (3), the first guide assembly (62) comprises a first guide rod (621), a first guide cylinder (622) and a first guide spring (623), the first guide rod (621) is movably inserted in the first guide cylinder (622), the first guide spring (623) is wound and arranged outside the first guide rod (621), the two ends of the first guide spring (623) are respectively fixedly connected to the side wall of the first guide rod (621) and the outer side wall of the first guide cylinder (622), the first guide rod (621) is connected to the blocking ball assembly (61), and the first guide cylinder (622) is connected to the support frame (3).

4. The intelligent civil air defense emergency control system according to claim 3 is characterized in that: The electromagnet mechanism (7) comprises an electromagnet body (71) arranged directly below the blocking ball assembly (61), a second wire (72) being connected to a side wall of the electromagnet body (71), a transverse plate (73) being fixedly connected to the side wall of the electromagnet body (71), a vertical plate (74) being fixedly connected to the lower end surface of the transverse plate (73), and a lower end of the vertical plate (74) being fixedly connected to the upper end surface of the support platform (1).

5. The intelligent civil air defense emergency control system according to claim 3 is characterized in that: The blocking ball assembly (61) comprises a rubber ball (611), the rubber ball (611) is provided with a first through hole (612) and a second through hole (613), the first through hole (612) and the second through hole (613) are arranged in communication, the hole size of the first through hole (612) is smaller than the hole size of the second through hole (613), a magnet rod (614) is movably inserted in the first through hole (612) and the second through hole (613), and a connecting spring (615) is wound around the outside of the magnet rod (614), The two ends of the connecting spring (615) are respectively fixedly connected to the side wall of the magnet rod (614) and the rubber ball (611); the upper end of the magnet rod (614) is fixedly connected to a first connecting column (616); the upper end of the first connecting column (616) is fixedly connected to a second connecting column (617); the second connecting column (617) and the first connecting column (616) are movably arranged in the second through hole (613); and the second connecting column (617) is fixedly connected to the first guide rod (621).

6. The intelligent civil air defense emergency control system according to claim 5 is characterized in that: The invention also comprises a locking mechanism (8), the locking mechanism (8) comprising a movable plate (81), two locking rods (82) being connected to the side wall of the movable plate (81), a locking groove (83) matching the locking rods (82) being provided on the first electrode contact sheet (51), a push-pull rod (85) being hinged on the side wall of the movable plate (81), the push-pull rod (85) being movably arranged in a third through hole (86), the third through hole (86) being provided on the rubber ball (611), and one end of the push-pull rod (85) away from the movable plate (81) being hinged on the side wall of the magnet rod (614).

7. The intelligent civil air defense emergency control system according to claim 6 is characterized in that: The locking mechanism (8) further comprises a second guide assembly (84), one end of the second guide assembly (84) being connected to the movable plate (81), and the other end of the second guide assembly (84) being connected to the rubber ball (611). The second guide assembly (84) comprises a second guide rod (841), a second guide cylinder (842) and a first guide spring (843). The second guide rod (841) is movably inserted into the second guide cylinder (842), the first guide spring (843) is wound around the outside of the second guide rod (841), and the two ends of the first guide spring (843) are respectively fixedly connected to the side wall of the second guide rod (841) and the outer side wall of the second guide cylinder (842). The second guide rod (841) is fixedly connected to the movable plate (81), and the second guide cylinder (842) is fixedly connected to the rubber ball (611).

8. The intelligent civil air defense emergency control system according to claim 6 is characterized in that: The locking rod (82) is connected to the movable plate (81) by a fastening mechanism (9), wherein the fastening mechanism (9) comprises a thread groove (91) formed on the outside of the locking rod (82), the locking rod (82) is threadedly inserted into an internally threaded spiral tube (92) through the thread groove (91), the internally threaded spiral tube (92) is fixedly arranged on a rotating shaft (93), the rotating shaft (93) is rotatably arranged on a sliding block (94), the sliding block (94) is slidably arranged in a sliding groove (96), and the sliding A groove (96) is formed on the movable plate (81); one end of the locking rod (82) located inside the internally threaded spiral tube (92) is fixedly connected to a first spring (95); a free end of the first spring (95) is fixedly connected to a side wall of the sliding block (94); one end of a pulling wire (97) is fixedly connected to an outer side wall of the internally threaded spiral tube (92); the other end of the pulling wire (97) is fixedly connected to a fixed block (98); and the fixed block (98) is fixedly arranged on the side wall of the movable plate (81).

9. The intelligent civil air defense emergency control system according to claim 8, characterized in that: The fastening mechanism (9) further comprises a third guide assembly (99), the third guide assembly (99) comprising a third guide rod (991), a third guide cylinder (992) and a third guide spring (993), the third guide rod (991) being movably inserted in the third guide cylinder (992), the third guide spring (993) being wound and arranged outside the third guide rod (991), and the two ends of the third guide spring (993) being respectively fixedly connected to the side wall of the third guide rod (991) and the outer side wall of the third guide cylinder (992), the third guide rod (991) being fixedly connected to the sliding block (94), and the third guide cylinder (992) being fixedly connected to the side wall of the sliding groove (96).

10. The intelligent civil air defense emergency control system according to claim 5, characterized in that: The device further comprises a third conduction mechanism (10), the third conduction mechanism (10) comprising a support tray (101) disposed in mutual abutment with the magnet rod (614), a vertical rod (102) being fixedly connected to the lower end surface of the support tray (101), the vertical rod (102) being movably inserted into a fourth through hole (103), the fourth through hole (103) being provided on the horizontal plate (107), a horizontal rod (108) being fixedly connected to the side wall of the horizontal plate (107), and a free end of the horizontal rod (108) being fixedly connected to the vertical rod (103). Connected to the side wall of the L-shaped plate (53), the outer fixed sleeve of the vertical rod (102) is provided with a rubber plug (104), the rubber plug (104) is in a truncated cone structure, the rubber plug (104) is movably inserted into the fourth through hole (103), the outer fixed sleeve of the vertical rod (102) is provided with a second electrode contact piece (105), the lower end of the second electrode contact piece (105) is abutted against a third electrode contact piece (106), and the third electrode contact piece (106) is fixedly arranged on the upper end surface of the horizontal plate (107).

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