1. Novel people's air defense engineering protective apparatus and zinc impregnation technology thereof, including radar (1), its characterized in that: the radar is characterized in that galvanizing agent layers (25) are symmetrically and fixedly connected to the front side and the back side of the radar (1), galvanizing layers (26) are symmetrically and fixedly connected to the surfaces of the two galvanizing agent layers (25), first connecting columns (2) are arranged at the bottoms of the galvanizing layers (26), thread grooves (3) are formed in the bottoms of the first connecting columns (2), rotating shaft bodies (4) are arranged on the right sides of the thread grooves (3), mounting grooves (5) are formed in the centers of the tops of the rotating shaft bodies (4), first circular grooves (6) are formed in the right sides of the mounting grooves (5), fixing bolts (7) are arranged on the right sides of the first circular grooves (6), first supporting columns (8) are arranged at the bottoms of the fixing bolts (7), hole grooves (9) are arranged at the bottoms of the first supporting columns (8), bases (10) are arranged at the bottoms of the hole grooves (9), and limiting blocks (11) are arranged in inner cavities of the bases (10), lead to groove (12) has been seted up in the centre of stopper (11), the symmetry all around that leads to groove (12) is provided with second spliced pole (13), four the bottom symmetry of second spliced pole (13) is provided with second support column (14), controls two the relative lateral symmetry of second support column (14) is provided with gyro wheel (15), the centre fixedly connected with fixed axle (16) of gyro wheel (15), two the front and the symmetrical fixedly connected with third spliced pole (17) of back of the relative one side of fixed axle (16), the bottom of third spliced pole (17) is provided with lug (18), the bottom of lug (18) is provided with main tributary dagger (19), guide rail (20) have been seted up to the centre symmetry of main tributary dagger (19) inner chamber left and right sides, two the relative one side of guide rail (20) is provided with second circular slot (21), the front of second circular slot (21) is provided with recess (22), recess (22) inner chamber centre fixedly connected with axis of rotation (23), centre fixedly connected with gear (24) on axis of rotation (23) surface, the top of gear (24) is provided with mainboard (27), the output electricity of mainboard (27) is connected with control module (28), the output electricity of control module (28) is connected with anti-interference module (29), the output electricity of anti-interference module (29) is connected with signal investigation module (30), the output electricity of signal investigation module (30) is connected with signal conversion module (31), the output electricity of signal conversion module (31) is connected with notice display module (32).

2. The novel civil air defense engineering protection equipment and the zincification process thereof as claimed in claim 1, wherein: the top fixed connection of first spliced pole (2) is in the centre of radar (1) bottom, the size looks adaptation of first spliced pole (2) and mounting groove (5), the size looks adaptation of first circular slot (6) and thread groove (3), the left side and the thread groove (3) threaded connection of fixing bolt (7).

3. The novel civil air defense engineering protection equipment and the zincification process thereof as claimed in claim 2, wherein: the bottom of the rotating shaft body (4) is rotatably connected to the top of the first supporting column (8), the hole groove (9) is formed in the center of the top of the base (10), and the bottom of the first supporting column (8) penetrates through the hole groove (9) and is inserted into the inner cavity of the base (10).

4. The novel civil air defense engineering protection equipment and the zincification process thereof as claimed in claim 3, wherein: the bottom of each second connecting column (13) is symmetrically inserted in the center of the top of each second supporting column (14), the bottom of each second connecting column (13) is movably connected in the inner cavity of each second supporting column (14), and the bottoms of the four second supporting columns (14) are symmetrically and fixedly connected to the periphery of the bottom of the inner cavity of the base (10).

5. The novel civil air defense engineering protection equipment and the zincification process thereof as claimed in claim 4, wherein: the opposite side symmetry fixed connection of third spliced pole (17) is in the bottom of first spliced pole (8) left and right sides, the back fixed connection of lug (18) is in the centre of the positive bottom of first spliced pole (8).

6. The novel civil air defense engineering protection equipment and the zincification process thereof as claimed in claim 5, wherein: the centre at main tributary dagger (19) top is seted up in second circular slot (21), the size looks adaptation of first support column (8) and second circular slot (21), the size looks adaptation of guide rail (20) and gyro wheel (15), the inner chamber at main tributary dagger (19) is pegged graft through second circular slot (21) in the bottom of first support column (8), recess (22) are seted up in the positive centre of main tributary dagger (19), gear (24) and lug (18) mesh mutually.

7. The novel civil air defense engineering protection equipment and the zincification process thereof as claimed in claim 6, wherein: mainboard (27) fixed connection is in the inner chamber of radar (1), the output and the input electricity of control module (28) of rotation axis body (4), axis of rotation (23) and gyro wheel (15) are connected.

8. The novel civil air defense engineering protection equipment and the zincification process thereof as claimed in claim 7, wherein: the output end of the control module (28) is electrically connected with the input end of the anti-interference module (29), and the output end of the control module (28) is electrically connected with the input ends of the signal checking module (30), the signal conversion module (31) and the notification display module (32).

Background

Air defense engineering protective equipment is a kind of equipment that can carry out early warning to the danger that comes in advance, and the corrosion resisting property and the wear resistance of current air defense engineering protective equipment main part building materials are all relatively poor, and life is extremely low, cause the pollution easily when producing, cause the pollution to the environment easily, and the cost is expensive.

Therefore, it is necessary to provide a new civil air defense engineering protection device and a zincizing process thereof to solve the above problems.

Disclosure of Invention

The invention mainly aims to provide novel civil air defense engineering protection equipment and a zinc impregnation process thereof, which can effectively solve the problems in the background technology.

In order to achieve the purpose, the invention adopts the technical scheme that:

the novel civil air defense engineering protection equipment and the zinc impregnation process thereof comprise a radar, wherein the front and back surfaces of the radar are symmetrically and fixedly connected with a zinc plating agent layer, the surface of the two zinc plating agent layers is symmetrically and fixedly connected with a zinc plating layer, the bottom of the zinc plating layer is provided with a first connecting column, the bottom of the first connecting column is provided with a threaded groove, the right side of the threaded groove is provided with a rotating shaft body, the center of the top of the rotating shaft body is provided with a mounting groove, the right side of the mounting groove is provided with a first circular groove, the right side of the first circular groove is provided with a fixing bolt, the bottom of the fixing bolt is provided with a first supporting column, the bottom of the first supporting column is provided with a hole groove, the bottom of the hole groove is provided with a base, the inner cavity of the base is provided with a limiting block, the center of the limiting block is provided with a through groove, and the periphery of the through groove is symmetrically provided with a second connecting column, the bottom symmetry of four second spliced poles is provided with a second supporting column, the left and right sides of two opposite side symmetries of the second supporting column are provided with idler wheels, the center fixedly connected with fixed shaft of the idler wheel, the front and back sides of two opposite sides of the fixed shaft are fixedly connected with a third spliced pole symmetrically, the bottom of the third spliced pole is provided with a convex block, the bottom of the convex block is provided with a main support column, the center symmetrically arranged at the left and right sides of the inner cavity of the main support column is provided with guide rails, the two opposite sides of the guide rails are provided with second circular grooves, the front side of the second circular grooves is provided with grooves, the center fixedly connected with rotating shafts in the inner cavities of the grooves is provided with gears, the top of the gears is provided with a mainboard, the output end of the mainboard is electrically connected with a control module, the output end of the control module is electrically connected with an anti-interference module, the output end of the anti-interference module is electrically connected with a signal checking module, the output end of the signal checking module is electrically connected with a signal conversion module, and the output end of the signal conversion module is electrically connected with a notification display module.

Preferably, the top fixed connection of first spliced pole is in the centre of radar bottom, the size looks adaptation of first spliced pole and mounting groove, the size looks adaptation of first circular slot and thread groove, fixing bolt's left side and thread groove threaded connection.

Preferably, the bottom of the rotating shaft body is rotatably connected to the top of the first support column, the hole groove is formed in the center of the top of the base, and the bottom of the first support column penetrates through the hole groove and is inserted into the inner cavity of the base.

Preferably, the bottom of each second connecting column is symmetrically inserted into the center of the top of each second supporting column, the bottom of each second connecting column is movably connected into the inner cavity of each second supporting column, and the bottoms of the four second supporting columns are symmetrically and fixedly connected to the periphery of the bottom of the inner cavity of the base.

Preferably, the opposite side of the third connecting column is symmetrically and fixedly connected to the bottoms of the left side and the right side of the first supporting column, and the back of the bump is fixedly connected to the center of the front bottom of the first supporting column.

Preferably, the second circular groove is formed in the center of the top of the main support column, the first support column is matched with the second circular groove in size, the guide rail is matched with the roller in size, the bottom of the first support column is inserted into the inner cavity of the main support column through the second circular groove, the groove is formed in the center of the front of the main support column, and the gear is meshed with the protruding block.

Preferably, the mainboard fixed connection is in the inner chamber of radar, the output and the control module's of the output of rotation axis body, axis of rotation and gyro wheel input electricity are connected.

Preferably, the output end of the control module is electrically connected with the input end of the anti-interference module, and the output end of the control module is electrically connected with the input ends of the signal checking module, the signal conversion module and the notification display module.

Advantageous effects

Compared with the prior art, the invention provides novel civil air defense engineering protection equipment and a zinc impregnation process thereof, and the novel civil air defense engineering protection equipment has the following beneficial effects:

1. the novel civil air defense engineering protection equipment and the zinc impregnation process thereof can send signals to the rotating shaft and the rotating shaft body by arranging the control module, thereby starting the rotating shaft and the rotating shaft body, when the rotating shaft rotates, the gear is driven to rotate, and through the arranged lug, the gear can be meshed with the rotating shaft body when rotating, so as to drive the first support column to move upwards in the inner cavity of the second circular groove, at the moment, the radar can be driven to move up and down, through the arranged first connecting column, the first connecting column can be inserted into the mounting groove arranged at the top of the rotating shaft body, through inserting the left side of the fixing bolt into the inner cavity of the first circular groove and being in threaded connection with the threaded groove, the bottom of the radar can be fixedly connected at the top of the rotating shaft body through the first connecting column, when the rotating shaft body is started, the radar can be driven to move in all directions, when civil air defense engineering is carried out, the height and angle of the radar can be freely adjusted, so that a large amount of information can be received and observed.

2. This novel people's air defense engineering protective apparatus and zinc impregnation technology thereof, through the surface of smearing the radar with the galvanizing agent layer uniformly, and heat it through heating device, make the inside active zinc atom of galvanizing agent in situ permeate to the inside of radar from the surface to the inside, thereby form the galvanizing coat and lay the surface at the radar, the corrosion resisting property and the wear resistance of multiplicable radar, make its life longer, the surface is harder, the production is pollution-free, the feature of environmental protection is excellent, do not influence the mechanical properties of radar.

3. This novel people's air defense engineering protective equipment and zinc impregnation technology thereof, mainboard through setting up, can control whole system, control module through setting up, the lift of steerable radar and the adjustment of angle, through the anti-interference module that sets up, can avoid other signals to cause the interference to the radar, signal investigation module through setting up, can investigate received information, thereby reject the information that does not need, through the signal conversion module that sets up, can convert received signal source, thereby convert required information and use, through the notice display module who sets up, can put in radar received information in the display screen.

Drawings

FIG. 1 is a schematic structural view of the front face of the present invention;

FIG. 2 is a schematic structural diagram of a limiting block according to the present invention;

FIG. 3 is a schematic diagram of the structure of the radar of the present invention;

FIG. 4 is a schematic structural view of the main support column and the first support column of the present invention;

FIG. 5 is an enlargement of FIG. 4 at A in accordance with the present invention;

fig. 6 is a system diagram of the present invention.

In the figure: 1. a radar; 2. a first connecting column; 3. a thread groove; 4. a rotation shaft body; 5. mounting grooves; 6. a first circular groove; 7. fixing the bolt; 8. a first support column; 9. a hole groove; 10. a base; 11. a limiting block; 12. a through groove; 13. a second connecting column; 14. a second support column; 15. a roller; 16. a fixed shaft; 17. a third connecting column; 18. a bump; 19. a main support column; 20. a guide rail; 21. a second circular groove; 22. a groove; 23. a rotating shaft; 24. a gear; 25. a zinc plating agent layer; 26. a zinc coating layer; 27. a main board; 28. a control module; 29. an anti-interference module; 30. a signal checking module; 31. a signal conversion module; 32. and a notification display module.

Detailed Description

In order to make the technical means, the creation characteristics, the achievement purposes and the effects of the invention easy to understand, the invention is further described with the specific embodiments.

As shown in fig. 1-6, the novel civil air defense engineering protection device and the zinc impregnation process thereof comprise a radar 1, wherein the front and back surfaces of the radar 1 are symmetrically and fixedly connected with a zinc plating agent layer 25, the surfaces of the two zinc plating agent layers 25 are symmetrically and fixedly connected with zinc plating layers 26, the bottom of each zinc plating layer 26 is provided with a first connecting column 2, the bottom of each first connecting column 2 is provided with a threaded groove 3, the right side of each threaded groove 3 is provided with a rotating shaft body 4, the center of the top of each rotating shaft body 4 is provided with a mounting groove 5, the right side of each mounting groove 5 is provided with a first round groove 6, the right side of each first round groove 6 is provided with a fixing bolt 7, the top of each first connecting column 2 is fixedly connected to the center of the bottom of the radar 1, the first connecting column 2 is matched with the size of the mounting groove 5, the first round groove 6 is matched with the size of the threaded groove 3, the left side of the fixing bolt 7 is in threaded connection with the threaded groove 3, the bottom of the fixing bolt 7 is provided with a first supporting column 8, the bottom of the first support column 8 is provided with a hole groove 9, the bottom of the hole groove 9 is provided with a base 10, the bottom of the rotating shaft body 4 is rotatably connected with the top of the first support column 8, the hole groove 9 is arranged in the center of the top of the base 10, the bottom of the first support column 8 penetrates through the hole groove 9 and is inserted into the inner cavity of the base 10, the inner cavity of the base 10 is provided with a limit block 11, the center of the limit block 11 is provided with a through groove 12, the periphery of the through groove 12 is symmetrically provided with second support columns 13, the bottoms of the four second support columns 13 are symmetrically provided with second support columns 14, the bottom of each second support column 13 is symmetrically inserted into the center of the top of each second support column 14, the bottom of each second support column 13 is movably connected into the inner cavity of the second support column 14, the bottoms of the four second support columns 14 are symmetrically and fixedly connected around the bottom of the inner cavity of the base 10, and one opposite sides of the left and right second support columns 14 are symmetrically provided with rollers 15, a fixed shaft 16 is fixedly connected in the center of the roller 15, a third connecting column 17 is symmetrically and fixedly connected on the front surface and the back surface of the opposite side of the two fixed shafts 16, a convex block 18 is arranged at the bottom of the third connecting column 17, one side of the opposite side of the third connecting column 17 is symmetrically and fixedly connected at the bottom of the left side and the right side of the first supporting column 8, the back surface of the convex block 18 is fixedly connected in the center of the bottom of the front surface of the first supporting column 8, a main supporting column 19 is arranged at the bottom of the convex block 18, guide rails 20 are symmetrically arranged in the center of the left side and the right side of the inner cavity of the main supporting column 19, a second circular groove 21 is arranged at the opposite side of the two guide rails 20, a groove 22 is arranged on the front surface of the second circular groove 21, a rotating shaft 23 is fixedly connected in the center of the inner cavity of the groove 22, a gear 24 is fixedly connected in the center of the surface of the rotating shaft 23, the second circular groove 21 is arranged in the center of the top of the main supporting column 19, and the first supporting column 8 is matched with the size of the second circular groove 21, the guide rail 20 is matched with the roller 15 in size, the bottom of the first support column 8 is inserted into the inner cavity of the main support column 19 through the second circular groove 21, the groove 22 is arranged in the center of the front surface of the main support column 19, the gear 24 is meshed with the bump 18, the top of the gear 24 is provided with a main board 27, the output end of the main board 27 is electrically connected with a control module 28, the output end of the control module 28 is electrically connected with an anti-interference module 29, the output end of the anti-interference module 29 is electrically connected with a signal checking module 30, the output end of the signal checking module 30 is electrically connected with a signal conversion module 31, the output end of the signal conversion module 31 is electrically connected with a notification display module 32, the main board 27 is fixedly connected with the inner cavity of the radar 1, the output ends of the rotating shaft 4, the rotating shaft 23 and the roller 15 are electrically connected with the input end of the control module 28, the output end of the control module 28 is electrically connected with the input end of the anti-interference module 29, the output end of the control module 28 is electrically connected with the input end of the signal checking module 30, the signal conversion module 31 is electrically connected with the input end of the notification display module 32, the control module 28 is arranged to send signals to the rotating shaft 23 and the rotating shaft 4, thereby starting the rotating shaft 23 and the rotating shaft 4, when the rotating shaft 23 rotates, the gear 24 is driven to rotate, through the arranged lug 18, the gear 24 can be meshed with the first support column 8 when rotating, thereby driving the first support column 8 to move upwards in the inner cavity of the second circular groove 21, at the moment, the radar 1 can be driven to move up and down, through the arranged first connecting column 2, the first connecting column 2 can be inserted into the mounting groove 5 arranged at the top of the rotating shaft 4, through inserting the left side of the fixing bolt 7 into the inner cavity of the first circular groove 6 and being in threaded connection with the threaded groove 3, the bottom of the radar 1 can be fixedly connected at the top of the rotating shaft 4 through the first connecting column 2, when the rotating shaft body 4 is started, the radar 1 can be driven to move in all directions, when people's air defense engineering is carried out, the height and the angle of the radar 1 can be freely adjusted, so that a large amount of information can be received and observed, the galvanized agent layer 25 is uniformly coated on the surface of the radar 1 and is heated by the heating device, active zinc atoms in the galvanized agent layer 25 penetrate into the radar 1 from the surface to the inside, so that the galvanized layer 26 is formed and is laid on the surface of the radar 1, the corrosion resistance and the wear resistance of the radar 1 can be improved, the service life of the radar 1 is longer, the outer surface is harder, pollution-free production is realized, the environmental protection performance is excellent, the mechanical performance of the radar 1 is not influenced, the whole system can be controlled by the arranged main board 27, the lifting and the angle adjustment of the radar 1 can be controlled by the arranged control module 28, and the anti-interference module 29 is arranged, can avoid other signals to cause the interference to radar 1, through the signal investigation module 30 that sets up, can investigate received information to reject the information that does not need, through the signal conversion module 31 that sets up, can convert the signal source that receives, thereby convert required information and use, through the notice display module 32 that sets up, can put in the display screen with radar 1 received information.

It should be noted that the invention is a new civil air defense engineering protection device and its zinc impregnation process, when in use, the galvanizing agent layer 25 is uniformly laid on the surface of the radar 1, the radar is heated by the heating device, after the heating is finished, the galvanizing layer 26 is formed and laid on the surface of the radar 1, at this time, the bottom of the first connecting column 2 is inserted into the inner cavity of the mounting groove 5, the right side of the fixing bolt 7 is inserted into the inner cavity of the first circular groove 6 and is in threaded connection with the threaded groove 3, at this time, the bottom of the radar 1 is fixedly connected to the bottom of the rotating shaft body 4 through the first connecting column 2, the main board 27 is started, the control module 28 is sent a signal, the control module 28 sends a signal to the rotating shaft 23 to drive the rotating shaft 23 to rotate, the rotating shaft 23 drives the gear 24 to rotate, when the gear 24 rotates, the gear 24 is meshed with the bump 18 to drive the first supporting column 8 to move upwards, when the first supporting column 8 moves upwards, the rollers 15 on the left and right sides are driven to slide in the inner cavity of the guide rail 20, simultaneously first support column 8 drives stopper 11 and moves upwards, and when stopper 11 moves upwards, drives second connection column 13 and moves to the top of 14 inner chambers of second support column, and radar 1 can move upwards this moment, through control module 28 signals to rotation axis body 4 for rotation axis body 4 can drive radar 1 and rotate.

The foregoing shows and describes the general principles and broad features of the present invention and advantages thereof. It will be understood by those skilled in the art that the present invention is not limited to the embodiments described above, which are described in the specification and illustrated only to illustrate the principle of the present invention, but that various changes and modifications may be made therein without departing from the spirit and scope of the present invention, which fall within the scope of the invention as claimed. The scope of the invention is defined by the appended claims and equivalents thereof.