Civil air defense door dynamic load simulation test equipment

By designing dynamic load simulation test equipment for civil air defense doors and utilizing a combination of lifting components and electromagnets, efficient dynamic load testing of civil air defense doors is achieved, solving the problems of inconvenient transportation and cumbersome testing, and improving test accuracy and efficiency.

CN120668403APending Publication Date: 2025-09-19HAINAN SAIF CIVIL DEFENSE ENGINEERING CO LTD
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Patent Information

Application Number
CN202510958774.3
Authority / Receiving Office
CN · China
Patent Type
Applications(China)
Current Assignee / Owner
Filing Date
2025-07-11
Publication Date
2025-09-19

AI Technical Summary

Technical Problem

Civil defense doors are inconvenient to carry and cumbersome to test during dynamic load testing, and existing equipment cannot efficiently simulate frontal and side impacts.

Method used

A dynamic load simulation test equipment for civil air defense doors was designed. Through the combination of lifting components, electromagnets and counterweights, frontal and side impacts on civil air defense doors were achieved. The switching connection state of the electromagnet was utilized to simplify the test process and improve work efficiency.

Benefits of technology

It realizes efficient testing of the dynamic load of civil air defense doors, simplifies the testing process, avoids multiple transfers, and improves testing accuracy and efficiency.

✦ Generated by Eureka AI based on patent content.

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Abstract

The invention discloses civil air defense door dynamic load simulation test equipment, and relates to the technical field of civil air defense door dynamic load test, the civil air defense door dynamic load simulation test equipment comprises a base, the top of the base is provided with a support frame, and the support frame is used for placing a civil air defense door; the two supporting assemblies are arranged on the two sides of the base; and the control assembly is arranged on the top of the base, and the control assembly is matched with the two supporting assemblies. Through work of the first electromagnet, the second electromagnet and the third electromagnet, switching of the connection state of the first balancing weight and the first connecting rope and the connection state of the first balancing weight and the second connecting rope can be achieved, and after the height of the first balancing weight is increased through the hoisting assembly, front-face impact work and side-face impact work are conducted; the civil air defense door dynamic load measuring device can measure the dynamic load of the civil air defense door, the functionality of the device is improved, the testing work of multiple devices is avoided, a large amount of transfer work of the civil air defense door in the testing process is also avoided, and the working efficiency is improved.
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Description

Technical Field

[0001] The present invention relates to the technical field of dynamic load testing of civil air defense doors, and in particular to a dynamic load simulation testing device for civil air defense doors. Background Art

[0002] The dynamic load of civil air defense doors refers to the load that the civil air defense doors bear during use, which changes rapidly with time. This test is used to identify the protective strength of civil air defense doors. For this purpose, a dynamic load simulation test equipment for civil air defense doors is proposed.

[0003] The dynamic loads of civil air defense doors are mainly divided into frontal impact and side impact. During this process, the civil air defense doors generally need to be placed on different types of test equipment. However, civil air defense doors are heavy, and there are many inconveniences during transportation, which makes the testing process more cumbersome. Summary of the Invention

[0004] The purpose of the present invention is to provide a dynamic load simulation test device for civil air defense doors to solve the technical problems in the prior art.

[0005] The present invention provides a dynamic load simulation test device for civil air defense doors, comprising: A base, wherein a support frame is provided on the top of the base, and the support frame is used to place the civil air defense door; Two support assemblies, the two support assemblies are arranged on both sides of the base; A control assembly is provided on the top of the base, adapted to the two support assemblies, and used to independently control the operation of the support assemblies; A support frame, the support frame being arranged on one side of the top of the base; A lifting assembly is rotatably mounted on top of the support frame; a first counterweight block, the first counterweight block being connected to the lifting assembly, the four side walls of the first counterweight block each having a rectangular hole, a counterweight assembly being disposed in each of the rectangular holes, and a strike plate being detachably fixed to the bottom of the first counterweight block; Two impact assemblies are arranged at both sides of the base, and both impact assemblies are adapted to the first counterweight.

[0006] Preferably, the support assembly includes: Two ear plates, each of which is fixed to one of the side walls of the support frame; a baffle, the baffle being rotatably disposed between the two lug plates; Two connecting rods, both of which are rotatably connected to the baffle; Two transmission assemblies are fixed on the top of the support frame, and the two transmission assemblies are respectively rotatably connected to the two connecting rods.

[0007] Preferably, the transmission assembly includes: Two support blocks, both of which are fixed on the top of the support frame; A screw rod, the screw rod and the two support blocks are rotatably connected; A connecting block, the connecting block being slidably disposed on the top of the support frame and being rotatably connected to the connecting rod; A second bevel gear is fixed on one end portion of the screw rod.

[0008] Preferably, the control component includes: An electric push rod, the electric push rod is fixed to the bottom of the support frame, and a connecting plate is fixed to the telescopic end of the electric push rod; Two mounting plates, the two mounting plates being fixed to the two ends of the connecting plate, the top of the support frame being provided with two through holes, and the two mounting plates passing through the two through holes respectively; Two first motors, the two first motors are respectively fixed on two mounting plates; Two first bevel gears are rotatably arranged on two mounting plates respectively, and the two first bevel gears are fixed to the output ends of the two first motors respectively, and the first bevel gears are adapted to the second bevel gears.

[0009] Preferably, the impact assembly includes: A guide rail is provided on one side of the base; A transmission block is slidably arranged on the top of the guide rail and passes through the bottom of the guide rail; A fixed plate, the fixed plate being fixed on the top of the transmission block; A trolley is provided at one side of the base, and the trolley is fixed to the fixing plate; A plurality of impact blocks are detachably fixed on the side wall of the trolley.

[0010] Preferably, it also includes: A first support plate, the first support plate being fixed to the top of the base at one side of the support frame; a first pulley, the first pulley being rotatably disposed on top of the first support plate; A first connecting rope, one end of which is fixed to the transmission block, the other end of which is fixed to a first electromagnet, and the first connecting rope passes through a first pulley.

[0011] Preferably, it also includes: a second pulley, the second pulley being fixed to a side wall of the base; a second support plate, the second support plate being fixed to the top of the base; A second connecting rope, one end of the second connecting rope is fixed to the transmission block, the other end of the second connecting rope is fixed with a second electromagnet, and the second electromagnet is placed on the second support plate, and the second connecting rope passes through the second support plate and the second pulley.

[0012] Preferably, the lifting assembly comprises: A turntable rotatably arranged on top of the support frame; a second motor, wherein the second motor is fixed to the support frame, and an output shaft of the second motor is fixed to the turntable; a first support, the first support being fixed on the top of the turntable; a first hydraulic push rod, the first hydraulic push rod being rotatably connected to the first support; a hydraulic winch, the hydraulic winch being fixed to the telescopic end of the first hydraulic push rod; a steel cable, one end of which is fixed to the reel of the hydraulic winch, and the other end of which is fixed to a third electromagnet; A support base, the support base being fixed on the side wall of the turntable; a second support, the second support being fixed to the top of the support base; A second hydraulic push rod is rotatably connected to the second support, and a telescopic end of the second hydraulic push rod is rotatably connected to the first hydraulic push rod.

[0013] Preferably, the counterweight assembly includes: A second counterweight block, wherein a connecting seat is fixed to a side wall of the second counterweight block, and the connecting seat is adapted to the rectangular hole; a first magnet, wherein the first magnet is fixed on the top of the second counterweight; A card slot, the card slot being provided at the bottom of the connecting seat; a first groove, the first groove being formed in the first counterweight, the first groove being connected to the rectangular hole, and a second groove being formed at the bottom of the first groove; a second magnet, the second magnet being slidably disposed in the first groove, and a plurality of fixing rods being disposed at the bottom of the second magnet; A connecting frame is fixed to a plurality of fixing rods, and clamping blocks are fixed on four sides of the connecting frame, and the clamping blocks are adapted to the clamping slots.

[0014] Compared with the prior art, the present invention has the following beneficial effects: The present invention provides a lifting assembly, a first counterweight, a first electromagnet, a second electromagnet and a third electromagnet, which can realize the switching of the connection status between the first counterweight and the first connecting rope and the second connecting rope through the work between the first electromagnet, the second electromagnet and the third electromagnet. After the first counterweight is lifted to a higher height by the lifting assembly, it performs frontal impact and side impact respectively to realize the measurement of the dynamic load of the civil defense door, thereby improving the functionality of the device. By avoiding the testing work of multiple devices, a large amount of transportation work of the civil defense door during the testing process is also avoided, thereby improving work efficiency. BRIEF DESCRIPTION OF THE DRAWINGS

[0015] In order to more clearly illustrate the specific embodiments of the present invention or the technical solutions in the prior art, the following briefly introduces the drawings required for use in the specific embodiments or the description of the prior art. Obviously, the drawings described below are some embodiments of the present invention. For ordinary technicians in this field, other drawings can be obtained based on these drawings without paying any creative work.

[0016] Figure 1 It is a schematic diagram of the three-dimensional structure of the present invention; Figure 2 The present invention Figure 1 A schematic diagram of the partially enlarged structure at center A; Figure 3 It is a schematic diagram of the first connecting rope, the second connecting rope and the guide rail structure of the present invention; Figure 4 The present invention Figure 3 A schematic diagram of the partially enlarged structure at point B in the middle; Figure 5 is a schematic structural diagram of the support frame and the second motor of the present invention; Figure 6 This is a schematic structural diagram of the electric push rod, connecting plate and mounting plate of the present invention; Figure 7 This is a schematic structural diagram of the first counterweight and the second counterweight of the present invention; Figure 8 This is a schematic diagram of the connecting seat and rectangular hole structure of the present invention; Figure 9 is a schematic cross-sectional structural diagram of a first counterweight block of the present invention; Figure 10 It is a schematic structural diagram of the first groove and the second groove of the present invention.

[0017] Reference numerals: 1. Base; 2. Support frame; 3. Ear plate; 4. Baffle; 5. Guide rail; 6. Support frame; 7. Turntable; 8. First support plate; 9. First pulley; 10. First electromagnet; 11. First connecting rope; 12. First support; 13. First hydraulic push rod; 14. Hydraulic winch; 15. Steel cable; 16. First counterweight; 17. Impact plate; 18. Support seat; 19. Second support; 20. Second hydraulic push rod; 21. Second connecting rope; 22. Second electromagnet; 23. Second support plate; 24. Second pulley; 25. Trolley; 26. Impact Block; 27, mounting plate; 28, first motor; 29, first bevel gear; 30, second bevel gear; 31, support block; 32, screw rod; 33, connecting block; 34, connecting rod; 35, fixing plate; 36, transmission block; 37, second motor; 38, electric push rod; 39, connecting plate; 40, third electromagnet; 41, second counterweight; 42, first magnet; 43, second magnet; 44, rectangular hole; 45, connecting seat; 46, clamping block; 47, connecting frame; 48, fixing rod; 49, clamping slot; 50, first groove; 51, second groove. DETAILED DESCRIPTION

[0018] The technical solution of the present invention will be clearly and completely described below with reference to the accompanying drawings. Obviously, the described embodiments are only part of the embodiments of the present invention, rather than all the embodiments.

[0019] The components of the embodiments of the present invention generally described and shown in the drawings herein may be arranged and designed in a variety of different configurations. Therefore, the following detailed description of the embodiments of the invention provided in the drawings is not intended to limit the scope of the claimed invention, but merely represents selected embodiments of the invention.

[0020] Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without making any creative work shall fall within the scope of protection of the present invention.

[0021] In the description of the present invention, it should be noted that the terms "center," "upper," "lower," "left," "right," "vertical," "horizontal," "inner," and "outer," etc., indicating orientations or positional relationships, are based on the orientations or positional relationships shown in the accompanying drawings and are intended solely to facilitate and simplify the description of the present invention. They are not intended to indicate or imply that the devices or components referred to must have, be constructed, or operate in a specific orientation, and therefore should not be construed as limitations on the present invention. Furthermore, the terms "first," "second," and "third" are used for descriptive purposes only and should not be construed as indicating or implying relative importance.

[0022] In the description of the present invention, it should be noted that, unless otherwise expressly specified or limited, the terms "mounted," "connected," and "connected" should be understood in a broad sense. For example, they may refer to fixed, detachable, or integral connections; mechanical or electrical connections; direct or indirect connections through an intermediate medium; and internal communication between two components. Those skilled in the art will understand the specific meanings of the above terms in the present invention based on the specific circumstances.

[0023] The following combination Figures 1 to 10 As shown, an embodiment of the present invention provides a dynamic load simulation test device for civil air defense doors, comprising: Base 1, a support frame 2 is provided on the top of the base 1, and the support frame 2 is used to place the civil air defense door; Two support assemblies, the two support assemblies are arranged on both sides of the base 1; A control component is provided on the top of the base 1 and is adapted to the two support components. The control component is used to independently control the operation of the support components. Support frame 6, support frame 6 is arranged on one side of the top of the base 1; A lifting assembly is rotatably mounted on top of the support frame 6; The first counterweight 16 is connected to the lifting assembly. The four side walls of the first counterweight 16 are provided with rectangular holes 44. Each rectangular hole 44 is provided with a counterweight assembly. The bottom of the first counterweight 16 is detachably fixed with a strike plate 17. Two impact assemblies are provided at both sides of the base 1 , and both impact assemblies are adapted to the first counterweight 16 .

[0024] Furthermore, the support assembly includes: Two ear plates 3, both of which are fixed on one of the side walls of the support frame 2; The baffle 4 is rotatably arranged between the two ear plates 3; Two connecting rods 34, both connecting rods 34 are rotatably connected to the baffle 4; Two transmission assemblies, both of which are fixed on the top of the support frame 2, and are rotatably connected to the two connecting rods 34 respectively.

[0025] Furthermore, the transmission assembly includes: Two support blocks 31, both of which are fixed on the top of the support frame 2; The screw rod 32 is rotatably connected to the two support blocks 31; The connecting block 33 is slidably arranged on the top of the support frame 2, and the connecting block 33 is rotatably connected to the connecting rod 34; The second bevel gear 30 is fixed on one end of the screw rod 32 .

[0026] Furthermore, the control component includes: The electric push rod 38 is fixed to the bottom of the support frame 2, and a connecting plate 39 is fixed to the telescopic end of the electric push rod 38; Two mounting plates 27 are fixed to the two ends of the connecting plate 39. Two through holes are provided on the top of the support frame 2, and the two mounting plates 27 pass through the two through holes respectively. Two first motors 28, the two first motors 28 are respectively fixed on the two mounting plates 27; Two first bevel gears 29 are rotatably mounted on the two mounting plates 27 , and the two first bevel gears 29 are fixed to the output ends of the two first motors 28 , respectively. The first bevel gears 29 are adapted to the second bevel gears 30 .

[0027] The position of the connecting plate 39 is adjusted by the electric push rod 38, and then the position of the first bevel gear 29 is changed by the mounting plate 27 on the connecting plate 39 and the first motor 28, so that the first bevel gear 29 is engaged with the corresponding second bevel gear 30, and through the operation of the first motor 28, in cooperation with the screw rod 32, the connecting block 33 and the connecting rod 34, the baffle 4 on the side of the door frame that is hit is rotated to an inclined state to prevent the trolley 25 from hitting the baffle 4, and the baffle 4 on the other side in a vertical state can provide support for the civil defense door, thereby avoiding energy loss caused by displacement of the civil defense door after being hit, so as to ensure test accuracy.

[0028] Furthermore, the impact assembly includes: A guide rail 5 is provided on one side of the base 1; The transmission block 36 is slidably disposed on the top of the guide rail 5 and passes through the bottom of the guide rail 5; Fixed plate 35, fixed on the top of transmission block 36; The trolley 25 is provided at one side of the base 1 and is fixed to the fixing plate 35; A plurality of impact blocks 26 are detachably fixed to the side wall of the trolley 25 .

[0029] Furthermore, it also includes: A first support plate 8 is fixed to the top of the base 1 on one side of the support frame 6; A first pulley 9, which is rotatably arranged on the top of the first support plate 8; The first connecting rope 11 has one end fixed to the transmission block 36 , and the other end of the first connecting rope 11 is fixed to the first electromagnet 10 , and the first connecting rope 11 passes through the first pulley 9 .

[0030] Furthermore, it also includes: A second pulley 24, the second pulley 24 is fixed to the side wall of the base 1; A second support plate 23, the second support plate 23 is fixed to the top of the base 1; The second connecting rope 21 has one end fixed to the transmission block 36 , and the other end of the second connecting rope 21 is fixed with a second electromagnet 22 , and the second electromagnet 22 is placed on the second support plate 23 , and the second connecting rope 21 passes through the second support plate 23 and the second pulley 24 .

[0031] When the lifting assembly is working, it drives the first counterweight 16 to rise. During this process, the first counterweight 16 drives the second connecting rope 21 to move through the second electromagnet 22, and the second connecting rope 21 drives the fixed plate 35 to move along the guide rail 5 through the transmission block 36, so that the trolley 25 can move to the end of the guide rail 5, and then disconnect the switch of the second electromagnet 22, and control the first counterweight 16 to continue to rise until the first counterweight 16 moves to the first electromagnet 10, and then turn on the switch of the first electromagnet 10. When the first electromagnet 10 is working, it is adsorbed on the first counterweight 16, and then the switch of the third electromagnet 40 is disconnected to make the first counterweight 16 drop vertically, and the first connecting rope 11 is driven to move by the action of the first electromagnet 10, and through the action of each auxiliary pulley, the first connecting rope 11 can drive the trolley 25 to move along the guide rail 5 through the transmission block 36 and the fixed plate 35, and hit the door frame of the civil defense door.

[0032] Furthermore, the lifting assembly includes: A turntable 7 is rotatably mounted on top of the support frame 6; The second motor 37 is fixed to the support frame 6, and the output shaft of the second motor 37 is fixed to the turntable 7; A first support 12, the first support 12 is fixed on the top of the turntable 7; A first hydraulic push rod 13, the first hydraulic push rod 13 is rotatably connected to the first support 12; A hydraulic winch 14 is fixed to the telescopic end of the first hydraulic push rod 13; A steel cable 15, one end of which is fixed to the reel of the hydraulic winch 14, and the other end of which is fixed to a third electromagnet 40; Support base 18, support base 18 is fixed on the side wall of turntable 7; A second support 19, the second support 19 is fixed on the top of the support base 18; The second hydraulic push rod 20 is rotatably connected to the second support 19 , and the telescopic end of the second hydraulic push rod 20 is rotatably connected to the first hydraulic push rod 13 .

[0033] The turntable 7 is driven to rotate by the second motor 37 to adjust the horizontal position of the hydraulic winch 14 at the end of the first hydraulic push rod 13. The second hydraulic push rod 20 cooperates with the rotation of the two second supports 19 to adjust the inclination angle of the first hydraulic push rod 13 to achieve height adjustment of the hydraulic winch 14. The hydraulic winch 14 works and the switch of the third electromagnet 40 is turned on to achieve the rise of the first counterweight 16. When the first counterweight 16 rises to the hydraulic winch 14, the switch of the third electromagnet 40 is turned off to achieve the release of the first counterweight 16. The first counterweight 16 is used to impact the door panel of the civil defense door to perform dynamic load testing of the door panel of the civil defense door.

[0034] Furthermore, the counterweight assembly includes: A second counterweight 41 is provided with a connecting seat 45 fixed to the side wall of the second counterweight 41 , and the connecting seat 45 is adapted to fit in the rectangular hole 44 ; A first magnet 42 is fixed on the top of the second counterweight 41; The card slot 49 is provided at the bottom of the connecting seat 45; A first groove 50 is provided in the first counterweight 16 , the first groove 50 is connected to the rectangular hole 44 , and a second groove 51 is provided at the bottom of the first groove 50 ; The second magnet 43 is slidably disposed in the first groove 50 , and a plurality of fixing rods 48 are disposed at the bottom of the second magnet 43 ; The connecting frame 47 is fixed to a plurality of fixing rods 48 , and a clamping block 46 is fixed on each of the four sides of the connecting frame 47 , and the clamping block 46 is adapted to the clamping slot 49 .

[0035] When the first counterweight 16 reaches its highest point and still cannot perform an effective impact test, the second counterweight 41 can be lifted by the action of the third electromagnet 40 and the first magnet 42, and the connecting seat 45 on the second counterweight 41 is inserted into the corresponding rectangular hole 44 on the first counterweight 16. Then, the third electromagnet 40 and the first magnet 42 are released. Thereafter, the first counterweight 16 and the second counterweight 41 are temporarily fixed together under the action of the connecting seat 45 and the rectangular hole 44. After an appropriate number of second counterweights 41 and the first counterweight 16 are preliminarily fixed, the third electromagnet 40 is moved to the top of the first counterweight 16, and the switch of the third electromagnet 40 is turned on. When the third electromagnet 40 is working, it attracts the second magnet 43. During the rising process of the second magnet 43, the connecting frame 47 is driven to rise through the fixing rod 48, and then all the blocks 46 are driven to rise. When the blocks 46 enter the card slots 49, the final fixation between the connecting seat 45 and the first counterweight 16 can be achieved, and then the overall weight of the first counterweight 16 is increased by adding the second counterweight 41, thereby increasing the impact force.

[0036] The specific working method is: first, the auxiliary pulley needs to be installed, and the installation position of the auxiliary pulley needs to be determined according to the position of the guide rail 5, and then the first connecting rope 11 and the second connecting rope 21 are tensioned and adjusted in direction through the action of the auxiliary pulley; During the frontal impact test, the turntable 7 is driven to rotate by the second motor 37 to adjust the horizontal position of the hydraulic winch 14 at the end of the first hydraulic push rod 13. The second hydraulic push rod 20 cooperates with the rotation of the two second supports 19 to adjust the inclination angle of the first hydraulic push rod 13 to achieve height adjustment of the hydraulic winch 14. The hydraulic winch 14 works to turn on the switch of the third electromagnet 40 to achieve the rise of the first counterweight 16. When the first counterweight 16 rises to the hydraulic winch 14, the switch of the third electromagnet 40 is turned off to release the first counterweight 16. The first counterweight 16 is used to impact the door panel of the civil air defense door to perform the dynamic load test of the door panel of the civil air defense door. During this process, the position adjustment of the two mounting plates 27 is achieved through the operation of the electric push rod 38 in cooperation with the connecting plate 39, so that the first motor 28 on the mounting plate 27 drives the first bevel gear 29 to engage with the two second bevel gears 30 respectively. The operation of the first motor 28 cooperates with the action of the first motor 28 and the second bevel gear 30 to drive the corresponding screw rod 32 to rotate, thereby driving the connecting block 33 to move. The baffle 4 is able to rotate around the ear plate 3 through the action of the connecting rod 34. Through the above operation, the two baffles 4 are adjusted to a vertical state, so that the door panel of the civil air defense door remains stable during the dynamic load test. In addition, according to actual conditions, the impact plates 17 and the first counterweight 16 with different surface areas can be fixed to achieve dynamic load testing under different contact areas; When performing the door frame impact test, the second motor 37 drives the turntable 7 to rotate so that the first counterweight 16 is located at one side of the support frame 6, and the steel cable 15 is released by the hydraulic winch 14 to make the first counterweight 16 at the lowest position, and the switch of the second electromagnet 22 is turned on so that the second electromagnet 22 can be adsorbed on the first counterweight 16, and then the first counterweight 16 is driven to rise by the operation of the hydraulic winch 14. In this process, the first counterweight 16 drives the second connecting rope 21 to move through the second electromagnet 22, and the second connecting rope 21 drives the fixed plate 35 to move along the guide rail 5 through the transmission block 36, so that the trolley 25 can move to the end of the guide rail 5, then turn off the switch of the second electromagnet 22, and control the first counterweight 16 to continue to rise until the first counterweight 16 moves to the first electromagnet 10, then turn on the switch of the first electromagnet 10, and the first electromagnet 10 is adsorbed on the first counterweight 16 when working, and then turn off the switch of the third electromagnet 40 to make the first counterweight 16 vertically descend, and the first electromagnet 10 drives the first connecting rope 11 to move, and through the action of each auxiliary pulley, the first connecting rope 11 can drive the trolley 25 to move along the guide rail 5 through the transmission block 36 and the fixed plate 35, and hit the door frame of the civil air defense door; Before the above test, the position of the first bevel gear 29 should be adjusted so that the first bevel gear 29 is meshed with the corresponding second bevel gear 30, and the baffle 4 on the side of the door frame that is hit is rotated to an inclined state through the operation of the first motor 28 in cooperation with the screw rod 32, the connecting block 33 and the connecting rod 34 to prevent the trolley 25 from hitting the baffle 4. The baffle 4 on the other side in the vertical state can provide support for the civil air defense door, thereby avoiding energy loss caused by displacement of the civil air defense door after being hit, so as to ensure the test accuracy; In addition, during the impact process, by removing or increasing the number of impact blocks 26, testing work with different contact areas and different contact positions can be achieved; When the first counterweight 16 reaches its highest point and still cannot perform an effective impact test, the second counterweight 41 can be lifted by the action of the third electromagnet 40 and the first magnet 42, and the connecting seat 45 on the second counterweight 41 is inserted into the corresponding rectangular hole 44 on the first counterweight 16. Then, the third electromagnet 40 and the first magnet 42 are released. Thereafter, the first counterweight 16 and the second counterweight 41 are temporarily fixed together under the action of the connecting seat 45 and the rectangular hole 44. After an appropriate number of second counterweights 41 and the first counterweight 16 are preliminarily fixed, the third electromagnet 40 is moved to the top of the first counterweight 16, and the switch of the third electromagnet 40 is turned on. When the third electromagnet 40 is working, it attracts the second magnet 43. During the rising process of the second magnet 43, the connecting frame 47 is driven to rise through the fixing rod 48, and then all the blocks 46 are driven to rise. When the blocks 46 enter the card slots 49, the final fixation between the connecting seat 45 and the first counterweight 16 can be achieved, and then the overall weight of the first counterweight 16 is increased by adding the second counterweight 41, thereby increasing the impact force.

[0037] It is worth mentioning that the auxiliary pulley mentioned in the present application is mainly used to adjust the direction of the first connecting rope 11 and the second connecting rope 21 to ensure that the force applied to the trolley 25 is parallel to the guide rail 5.

[0038] Finally, it should be noted that the above embodiments are only used to illustrate the technical solutions of the present invention, rather than to limit it. Although the present invention has been described in detail with reference to the above embodiments, those skilled in the art should understand that they can still modify the technical solutions described in the above embodiments, or replace some or all of the technical features therein with equivalents. However, these modifications or replacements do not cause the essence of the corresponding technical solutions to deviate from the scope of the technical solutions of the embodiments of the present invention.

Claims

1. A dynamic load simulation test equipment for civil air defense doors, characterized in that: include: A base (1), wherein a support frame (2) is provided on the top of the base (1), and the support frame (2) is used to place the civil air defense door; Two support assemblies, the two support assemblies being arranged on both sides of the base (1); A control component, the control component being arranged on the top of the base (1), the control component being adapted to the two support components, and the control component being used to independently control the operation of the support components; A support frame (6), the support frame (6) being arranged on one side of the top of the base (1); A lifting assembly, the lifting assembly being rotatably mounted on the top of the support frame (6); A first counterweight (16), the first counterweight (16) being connected to the lifting assembly, the four side walls of the first counterweight (16) being provided with rectangular holes (44), each of the rectangular holes (44) being provided with a counterweight assembly, and a strike plate (17) being detachably fixed to the bottom of the first counterweight (16); Two impact assemblies are provided, both of which are arranged at both sides of the base (1), and both of which are adapted to the first counterweight (16).

2. The dynamic load simulation test equipment for civil air defense doors according to claim 1 is characterized in that: The support assembly comprises: Two ear plates (3), both of the ear plates (3) are fixed on one of the side walls of the support frame (2); a baffle (4), the baffle (4) being rotatably arranged between the two ear plates (3); Two connecting rods (34), both of the connecting rods (34) are rotatably connected to the baffle (4); Two transmission assemblies are fixed on the top of the support frame (2), and the two transmission assemblies are rotationally connected to two connecting rods (34) respectively.

3. The dynamic load simulation test equipment for civil air defense doors according to claim 2, characterized in that: The transmission assembly comprises: Two support blocks (31), both of which are fixed on the top of the support frame (2); A screw rod (32), wherein the screw rod (32) is rotatably connected to the two support blocks (31); A connecting block (33), wherein the connecting block (33) is slidably arranged on the top of the support frame (2), and the connecting block (33) and the connecting rod (34) are rotatably connected; A second bevel gear (30) is fixed on one end of the screw rod (32).

4. The dynamic load simulation test equipment for civil air defense doors according to claim 3 is characterized in that: The control component includes: An electric push rod (38), the electric push rod (38) is fixed to the bottom of the support frame (2), and a connecting plate (39) is fixed to the telescopic end of the electric push rod (38); Two mounting plates (27), the two mounting plates (27) are fixed on two ends of the connecting plate (39), the top of the support frame (2) is provided with two through holes, and the two mounting plates (27) pass through the two through holes respectively; Two first motors (28), the two first motors (28) being fixed on two mounting plates (27) respectively; Two first bevel gears (29) are rotatably mounted on two mounting plates (27) and are fixed to output ends of two first motors (28) respectively. The first bevel gears (29) are adapted to the second bevel gear (30).

5. The dynamic load simulation test equipment for civil air defense doors according to claim 1, characterized in that: The impact assembly comprises: A guide rail (5), wherein the guide rail (5) is arranged on one side of the base (1); A transmission block (36), wherein the transmission block (36) is slidably arranged on the top of the guide rail (5), and the transmission block (36) passes through the bottom of the guide rail (5); A fixed plate (35), wherein the fixed plate (35) is fixed on the top of the transmission block (36); A trolley (25), wherein the trolley (25) is arranged at one side of the base (1), and the trolley (25) and the fixing plate (35) are fixed; A plurality of impact blocks (26) are detachably fixed on the side wall of the trolley (25).

6. The dynamic load simulation test equipment for civil air defense doors according to claim 5, characterized in that: Also includes: A first support plate (8), the first support plate (8) being fixed to the top of the base (1) on one side of the support frame (6); a first pulley (9) rotatably disposed on the top of the first support plate (8); A first connecting rope (11), one end of the first connecting rope (11) is fixed to the transmission block (36), the other end of the first connecting rope (11) is fixed with a first electromagnet (10), and the first connecting rope (11) passes through a first pulley (9).

7. The dynamic load simulation test equipment for civil air defense doors according to claim 6, characterized in that: Also includes: a second pulley (24), the second pulley (24) being fixed on a side wall of the base (1); a second support plate (23), the second support plate (23) being fixed to the top of the base (1); A second connecting rope (21), one end of the second connecting rope (21) is fixed to the transmission block (36), the other end of the second connecting rope (21) is fixed with a second electromagnet (22), and the second electromagnet (22) is placed on the second support plate (23), and the second connecting rope (21) passes through the second support plate (23) and the second pulley (24).

8. The dynamic load simulation test equipment for civil air defense doors according to claim 1, characterized in that: The lifting assembly comprises: A turntable (7), the turntable (7) being rotatably arranged on the top of the support frame (6); A second motor (37), wherein the second motor (37) and the support frame (6) are fixed, and an output shaft of the second motor (37) and the turntable (7) are fixed; A first support (12), wherein the first support (12) is fixed on the top of the turntable (7); a first hydraulic push rod (13), wherein the first hydraulic push rod (13) is rotatably connected to the first support (12); A hydraulic winch (14), wherein the hydraulic winch (14) is fixed to the telescopic end of the first hydraulic push rod (13); A steel cable (15), one end of the steel cable (15) is fixed to the reel of the hydraulic winch (14), and the other end of the steel cable (15) is fixed to a third electromagnet (40); A support seat (18), wherein the support seat (18) is fixed on the side wall of the turntable (7); A second support (19), the second support (19) being fixed on the top of the support base (18); A second hydraulic push rod (20) is rotatably connected to the second support (19), and a telescopic end of the second hydraulic push rod (20) is rotatably connected to the first hydraulic push rod (13).

9. The dynamic load simulation test equipment for civil air defense doors according to claim 1, characterized in that: The counterweight assembly comprises: A second counterweight (41), wherein a connecting seat (45) is fixed to a side wall of the second counterweight (41), and the connecting seat (45) is adapted to fit the rectangular hole (44); a first magnet (42), wherein the first magnet (42) is fixed on the top of the second counterweight (41); A card slot (49), wherein the card slot (49) is provided at the bottom of the connecting seat (45); A first groove (50), the first groove (50) is provided in the first counterweight (16), the first groove (50) is communicated with the rectangular hole (44), and a second groove (51) is provided at the bottom of the first groove (50); A second magnet (43), the second magnet (43) being slidably disposed in the first groove (50), and a plurality of fixing rods (48) being disposed at the bottom of the second magnet (43); A connecting frame (47) is fixed to a plurality of fixing rods (48), and four sides of the connecting frame (47) are fixed with clamping blocks (46), and the clamping blocks (46) are adapted to the clamping slots (49).