CN109489478B - Aerial target display console - Google Patents
Aerial target display console Download PDFInfo
- Publication number
- CN109489478B CN109489478B CN201811617505.7A CN201811617505A CN109489478B CN 109489478 B CN109489478 B CN 109489478B CN 201811617505 A CN201811617505 A CN 201811617505A CN 109489478 B CN109489478 B CN 109489478B
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- lever
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- workbench
- resistance arm
- arm
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41A—FUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
- F41A33/00—Adaptations for training; Gun simulators
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
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- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Toys (AREA)
Abstract
The invention relates to the field of control consoles, in particular to an aerial target display control console, which comprises an airplane model, a workbench, a supporting frame, upright rods and a model base, wherein the workbench with a hollow cuboid structure is welded on the upper surface wall of the supporting frame, the model base is arranged on the upper surface wall of the workbench, the upright rods are fixed above the model base, the top of the upright rods is connected with the airplane model, the base is arranged on the upper surface wall of the bottom plate of the workbench through bolts, the upper surface wall of the base is connected with an electromagnet and a shaft bracket through bolts, and the shaft bracket is arranged on one side of the electromagnet.
Description
Technical Field
The invention relates to the field of aerial target display consoles, in particular to an aerial target display console.
Background
At present, the training of the air target recognition class of the air defense personnel main training is mainly finished by guaranteeing personnel to lift an airplane model, the problems of inconsistent target presentation time and angle, uneven height and the like exist in the way of lifting the airplane model, the lifting speed of training results is seriously influenced, and the personnel is especially used for guaranteeing that the assessment is quite objectively carried out.
Disclosure of Invention
The present invention is directed to an air target display console to solve the above-mentioned problems.
In order to achieve the above purpose, the present invention provides the following technical solutions:
the aerial target display control console comprises an airplane model, a workbench, a support frame, upright rods and a model base, wherein a workbench with a hollow cuboid structure is welded on the upper surface wall of the support frame, the model base is arranged on the upper surface wall of the workbench, the upright rods are fixed above the model base, the top of the upright rods is connected with the airplane model, the base is arranged on the upper surface wall of the bottom plate of the workbench through bolts, the upper surface wall of the base is connected with an electromagnet and a shaft bracket through bolts, the shaft bracket is arranged on one side of the electromagnet, two shaft brackets are arranged in total, a rotating shaft is connected between the two shaft brackets, a through square groove is transversely formed in the middle of the rotating shaft, a lever is inserted in the square groove and consists of a lever resistance arm and a lever power arm, the lever resistance arm is kept away from the one end welding of lever resistance arm and has been had the baffle, the fluting has all been seted up on roof and the back wall of workstation, and two flutings link up, the lever resistance arm is kept away from the one end welding of lever resistance arm has the handle, the handle extends to the outside of workstation by the fluting, the outside cover of handle is equipped with the rubber sleeve, the exterior wall of rubber sleeve evenly is provided with the lug, lug and rubber sleeve integrated into one piece, install AC circuit breaker, time relay and time delay relay through the bolt on the bottom horizontal pole of support frame, time relay is located one side of AC circuit breaker, time delay relay is located one side that AC circuit breaker was kept away from to time delay relay, electro-magnet, AC circuit breaker, time relay and time delay relay all are connected with 220V commercial power.
Further, the model base is of a cuboid structure with the length of 5cm multiplied by 2cm, and magnets are arranged at four corner positions at the bottom of the model base.
Further, a rubber cushion groove with an upward opening is formed in the bottom wall of the workbench, and a rubber cushion is embedded in the rubber cushion groove.
Further, when the lever resistance arm of the lever is lifted, the lever power arm of the lever is fixedly adsorbed with the electromagnet, the baffle is 20cm higher than the upper surface of the workbench, and when the lever resistance arm of the lever is lowered, the connection part of the lever resistance arm and the baffle is in contact with the rubber pad, and the baffle is 5cm higher than the upper surface of the workbench.
Further, the lever passes through the rotating shaft, one end of the lever forms a lever power arm, the other end of the lever forms a lever resistance arm, and the ratio of the lever power arm to the lever resistance arm is 1:10.
Further, the baffle plate and the lever resistance arm are integrally formed, and the baffle plate is perpendicular to the lever resistance arm.
Further, the middle position of the upper surface wall of the model base and the middle position of the bottom of the airplane model are respectively provided with a round threaded hole with the diameter of 3.1mm, the vertical rod is of a cylindrical structure with the diameter of 3mm and the length of 14cm, the top end and the bottom end of the vertical rod are respectively provided with threads, the top end of the vertical rod stretches into the threaded hole formed in the bottom of the airplane model to be in threaded connection with the airplane model, and the bottom end of the vertical rod stretches into the threaded hole formed in the upper surface wall of the model base to be in threaded connection with the model base.
Compared with the prior art, the invention has the beneficial effects that:
when the electric power device is electrified and used, under the action of the time relay and the time delay relay, the electromagnet works for 5 seconds, the lever power arm of the adsorption lever and the lever resistance arm tilt upwards to drive the baffle plate connected with the electric power device to tilt upwards, the lever power arm is adsorbed by the electromagnet, when the baffle plate is attached to the workbench, the baffle plate is vertical to the upper surface of the workbench, at the moment, the baffle plate is 20cm higher than the upper surface of the workbench, the airplane model is shielded for 5 seconds, an airplane model target is shielded, a training person records the target, after 5 seconds, the alternating current circuit breaker works, the electromagnet is powered off, the electromagnetic force disappears, the baffle plate and the lever fall under the self gravity, the baffle plate is contacted with the rubber cushion until the target appears, the training person observes the identification target, the alternating current circuit breaker, the time delay relay, the electromagnet and the lever are matched for use, the effect of timing showing and hiding of the airplane model is achieved, the upper hand of the worker is liberated, the accuracy of training is improved, the four magnets are arranged on the upper surface of the workbench, the airplane model base can be adsorbed on the upper surface of the workbench, the electric power device is convenient to replace, the electric power device is convenient to hold the electric power device, and the electric power device is opened when the electric power device is in a power failure state, and the electric power device is opened to be opened to the electric power device is in a power failure state, and a user is normal, and a power failure device is held to be opened, and a power failure device is opened to the electric power device and is opened.
The aerial target display control console can show or shield an airplane model regularly, so that the problem that when a person needs to lift an airplane and check, the person lifts the airplane in inconsistent time and the check is not objective is solved, meanwhile, the design is light and attractive, the replacement of the airplane is stable and quick, the training is labor-saving and the check is fair is ensured, the control console effectively changes the training mode of the serious difficulty subjects of the air-defense personnel, and the control console has higher practical value.
Drawings
Figure 1 is a side cross-sectional view of the baffle of the present invention as it is raised.
Figure 2 is a front cross-sectional view of the baffle of the present invention as it is raised.
Figure 3 is a side cross-sectional view of the baffle of the present invention as it is lowered.
Fig. 4 is a front cross-sectional view of the baffle of the present invention as it is lowered.
Fig. 5 is a side view of the present invention.
Fig. 6 is a bottom view of the mold base of the present invention.
Fig. 7 is an enlarged schematic view of the area a in fig. 1 according to the present invention.
Fig. 8 is an enlarged schematic view of the area B of fig. 1 according to the present invention.
Fig. 9 is a circuit diagram of the present invention.
Fig. 10 is a rear view of the table of the present invention.
In the figure: 1. an aircraft model; 2. a baffle; 3. a lever; 301. lever resistance arm; 302. a lever power arm; 4. a work table; 5. a support frame; 6. an alternating current circuit breaker; 7. rubber cushion; 8. a rubber pad groove; 9. an electromagnet; 10. a magnet; 11. a shaft bracket; 12. a base; 13. a delay relay; 14. a time relay; 15. a vertical rod; 16. a model base; 17. a rotating shaft; 18. a rubber sleeve; 19. a handle; 20. slotting; 21. and a bump.
Detailed Description
The following description of the embodiments of the present invention will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present invention, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the invention without making any inventive effort, are intended to be within the scope of the invention.
In the description of the present invention, it should be noted that the terms "upper/lower", "inner", "outer", "front", "rear", "both ends", "one end", "the other end", etc. indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, are merely for convenience in describing the present invention and simplifying the description, and do not indicate or imply that the apparatus or elements referred to must have a specific orientation, be configured and operated in a specific orientation, and thus should not be construed as limiting the present invention. Furthermore, the terms "first," "second," and the like, are used for descriptive purposes only and are not to be construed as indicating or implying relative importance.
In the description of the present invention, it should be noted that, unless explicitly specified and limited otherwise, the terms "mounted," "configured/arranged," "coupled," "connected," and the like are to be construed broadly and include, for example, "connected," either fixedly, detachably, or integrally; can be mechanically or electrically connected; can be directly connected or indirectly connected through an intermediate medium, and can be communication between two elements. The specific meaning of the above terms in the present invention will be understood in specific cases by those of ordinary skill in the art.
As shown in figures 1-10, an aerial target display control console comprises an airplane model 1, a workbench 4, a support frame 5, a vertical rod 15 and a model base 16, wherein the workbench 4 with a hollow cuboid structure is welded on the upper surface wall of the support frame 5 and is used for placing the airplane model 1, the model base 16 is arranged on the upper surface wall of the workbench 4, the vertical rod 15 is fixedly arranged above the model base 16, the top of the vertical rod 15 is connected with the airplane model 1, round threaded holes with the diameter of 3.1mm are drilled in the middle position of the upper surface wall of the model base 16 and the middle position of the bottom of the airplane model 1, the vertical rod 15 is of a cylindrical structure with the diameter of 3mm, threads are formed in the top end and bottom surface wall of the vertical rod 15, the top end of the vertical rod 15 stretches into the threaded holes formed in the bottom of the airplane model 1 and is in threaded connection with the airplane model base 16, in use, the top end of the vertical rod 15 stretches into the threaded holes formed in the bottom of the model base 16 and is in threaded connection with the model base 16, the top of the vertical rod 15 stretches into the bottom of the vertical rod 1, the top of the vertical rod 15 stretches into the threaded holes formed in the bottom of the model base 1, the magnet 15 is in the position of the bottom of the model base 16 is equal to be in the shape of the diameter of 3 cm, the diameter of the cylindrical structure is equal to be 3, the diameter of the cylindrical structure is equal to 3mm, the cylindrical structure is equal to the diameter of the vertical rod 15, the top of the bottom of the model 1 is equal to the model 1, the bottom of the model base is equal to the model base is 5cm, and the bottom 5cm is equal to the bottom 5, and the bottom 5cm is opposite to the bottom 5, and the bottom 5 is 5cm is 5 and the bottom 5.
The base 12 is arranged on the upper surface wall of the bottom plate of the workbench 4 through bolts, the electromagnet 9 and the shaft bracket 11 are connected on the upper surface wall of the base 12 through bolts, the shaft bracket 11 is positioned on one side of the electromagnet 9, the type of the electromagnet 9 is ELE-P30/22 24V, two shaft brackets 11 are arranged in total, a rotating shaft 17 is connected between the two shaft brackets 11, a through square groove is transversely arranged in the middle of the rotating shaft 17, the size of the square groove is matched with the vertical section size of the lever 3, the lever 3 is convenient to detach, a lever 3 is inserted in the square groove, the lever 3 consists of a lever resistance arm 301 and a lever power arm 302, one end of the lever resistance arm 301 far away from the lever power arm 302 is welded with a baffle plate 2, an alternating current circuit breaker 6, an alternating current relay 14 and a time delay relay 13 are arranged on the bottom cross rod of the support 5 through bolts, the model of the alternating current breaker 6 is PMB9-63, the time relay 14 is DH48S-S, the model of the time delay relay 13 is JSZ3, the time relay 14 is positioned on one side of the alternating current breaker 6, the time delay relay 13 is positioned on one side of the time relay 14 far away from the alternating current breaker 6, the electromagnet 9, the alternating current breaker 6, the time relay 14 and the time delay relay 13 are all connected with 220V mains supply, the lever 3 passes through the rotating shaft 17, one end of the lever 3 forms a lever power arm 302, the other end forms a lever resistance arm 301, the ratio of the lever power arm 302 to the lever resistance arm 301 is 1:10, the baffle 2 and the lever resistance arm 301 are integrally formed, and the baffle 2 is perpendicular to the lever resistance arm 301, when the electric power is electrified and in use, the electromagnet 9 is enabled to work for 5 seconds under the action of the time relay 14 and the time delay relay 13, the lever arm 302 of the lever 3 is adsorbed, the lever resistance arm 301 is lifted upwards to drive the baffle plate 2 connected with the lever resistance arm 301 to lift upwards, the lever power arm 302 is adsorbed by the electromagnet 9, when the lever power arm 302 is attached to the lever resistance arm, the baffle plate 2 is perpendicular to the upper surface of the workbench 4, at the moment, the baffle plate 2 is 20cm higher than the upper surface of the workbench 4, the airplane model 1 is shielded for 5 seconds, the airplane model target is shielded, a training person records the target, after 5 seconds, the alternating current circuit breaker 6 works, the electromagnet 9 is powered off, the electromagnetic force disappears, the baffle plate 2 and the lever 3 descend under the self gravity, the connecting part of the baffle plate 2 and the lever resistance arm 301 is lowered to be contacted with the rubber pad 7, the target appears, and the training person observes and identifies the target.
The bottom wall of the workbench 4 is provided with a rubber cushion groove 8 with an upward opening, a rubber cushion 7 is embedded in the rubber cushion groove 8, when the baffle 2 is in a falling state, the joint of the baffle 2 and the lever resistance arm 301 is connected with the rubber cushion 7, and as the baffle 2 repeatedly ascends and descends, the buffer effect can be achieved through the arranged rubber cushion 7, the problems that the collision sound of the baffle 2 and the workbench 4 is overlarge and the abrasion is overlarge are avoided, when the lever resistance arm 301 of the lever 3 is lifted, the lever power arm 302 of the lever 3 is fixedly adsorbed by the electromagnet 9, the baffle 2 is 20cm higher than the upper surface of the workbench 4, when the lever resistance arm 301 of the lever 3 is descended, the joint of the lever resistance arm 301 and the baffle 2 is in contact with the rubber cushion 7, and the baffle 2 is 5cm higher than the upper surface of the workbench 4 for shielding other airplane models 1 laid on the upper surface of the workbench 4.
The top wall and the rear wall of the workbench 4 are provided with grooves 20, the two grooves 20 are communicated, one end of the lever power arm 302, far away from the lever resistance arm 301, is welded with a handle 19, the handle 19 extends to the outside of the workbench 4 from the grooves 20, a rubber sleeve 18 is sleeved on the outside of the handle 19, a lug 21 is uniformly arranged on the outer surface wall of the rubber sleeve 18, and the lug 21 and the rubber sleeve 18 are integrally formed.
Working principle: when in use, the electromagnet 9, the alternating current breaker 6, the time relay 14 and the time relay 13 are all connected with a 220V power supply, the top end of the upright 15 stretches into a threaded hole formed in the bottom of the airplane model 1, the airplane model 1 is rotated relative to the upright 15, the airplane model 1 is fixed with the upright 15, the bottom of the upright 15 stretches into a threaded hole formed in the middle position of the model base 16, the upright 15 is rotated relative to the model base 16, the upright 15 is fixed with the model base 16, the electromagnet 9 is not fixed with the lever power arm 302 under the condition of no power supply, the connecting part of the baffle 2 and the lever resistance arm 301 is contacted with the rubber pad 7 under the gravity action of the baffle 2 and the lever 3, when in power supply, the electromagnet 9 is enabled to work for 5 seconds under the action of the time relay 14 and the time relay 13, the lever power arm 302 of the lever 3 is adsorbed, the lever resistance arm 301 is lifted upwards to drive the baffle plate 2 connected with the lever resistance arm 301 to lift upwards, the lever power arm 302 is absorbed by the electromagnet 9, when the lever power arm 302 is attached to the lever resistance arm, the baffle plate 2 is vertical to the upper surface of the workbench 4, at the moment, the baffle plate 2 is 20cm higher than the upper surface of the workbench 4, the airplane model 1 is shielded for 5 seconds, the airplane model target is shielded, a training person records the target, after 5 seconds, the alternating current circuit breaker 6 works, the electromagnet 9 is powered off, the electromagnetic force disappears, the baffle plate 2 and the lever 3 descend under the self gravity, the connecting part of the baffle plate 2 and the lever resistance arm 301 is lowered to be contacted with the rubber pad 7, the target appears, the training person observes and identifies the target, the baffle plate 2 is 5cm higher than the upper surface of the workbench 4, and is used for shielding other airplane models 1 laid on the upper surface of the workbench 4, if the power is cut off or the alternating current circuit breaker 6, the electromagnet 9, the delay relay 13, when the module used by the time relay 14 after any power connection fails and the device cannot be used normally, a worker can hold the handle 19 and push down to enable the lever power arm 302 to act downwards and enable the lever resistance arm 301 to tilt upwards, so that the baffle plate 2 is driven to tilt upwards to shield the airplane model 1, and normal use of the device is ensured.
Although embodiments of the present invention have been shown and described, it will be understood by those skilled in the art that various changes, modifications, substitutions and alterations can be made therein without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
Claims (7)
1. Aerial target shows control cabinet, including aircraft model (1), workstation (4), support frame (5), pole setting (15) and model base (16), table wall welding has workstation (4) for cavity cuboid structure on support frame (5), the last table wall of workstation (4) is provided with model base (16), the top of model base (16) is fixed with pole setting (15), the top of pole setting (15) is connected with aircraft model (1), its characterized in that: the base (12) is arranged on the upper surface wall of the bottom plate of the workbench (4) through bolts, the electromagnet (9) and the shaft bracket (11) are connected to the upper surface wall of the base (12) through bolts, the shaft bracket (11) is positioned on one side of the electromagnet (9), two shaft brackets (11) are arranged in total, a rotating shaft (17) is connected between the two shaft brackets (11), a through square groove is transversely formed in the middle of the rotating shaft (17), a lever (3) is inserted in the square groove, the lever (3) is composed of a lever resistance arm (301) and a lever power arm (302), one end of the lever resistance arm (301) far away from the lever power arm (302) is welded with a baffle plate (2), grooves (20) are formed in the top wall and the rear wall of the workbench (4), one end of the lever power arm (302) far away from the lever resistance arm (301) is welded with a handle (19), the handle (19) extends from the grooves (20) to the outside of the workbench (4), the rubber sleeve (18) is uniformly sleeved on the outer surface of the rubber sleeve (18), the alternating current circuit breaker is characterized in that an alternating current circuit breaker (6), a time relay (14) and a time delay relay (13) are mounted on a bottom cross rod of the supporting frame (5) through bolts, the time relay (14) is located on one side of the alternating current circuit breaker (6), the time delay relay (13) is located on one side, far away from the alternating current circuit breaker (6), of the time relay (14), and the electromagnet (9), the alternating current circuit breaker (6), the time relay (14) and the time delay relay (13) are all connected with 220V mains supply.
2. An airborne target display console as in claim 1, wherein: the model base (16) is of a cuboid structure with the length of 5cm multiplied by 2cm, and magnets (10) are arranged at four corner positions at the bottom of the model base (16).
3. An airborne target display console as in claim 1, wherein: the bottom wall of the workbench (4) is provided with a rubber cushion groove (8) with an upward opening, and a rubber cushion (7) is embedded in the rubber cushion groove (8).
4. An airborne target display console as in claim 1, wherein: when the lever resistance arm (301) of the lever (3) is lifted, the lever power arm (302) of the lever (3) is fixedly adsorbed with the electromagnet (9), the baffle (2) is higher than the upper surface of the workbench (4) by 20cm, and when the lever resistance arm (301) of the lever (3) is lowered, the connecting part of the lever resistance arm (301) and the baffle (2) is contacted with the rubber pad (7), and the baffle (2) is higher than the upper surface of the workbench (4) by 5cm.
5. An airborne target display console as in claim 1, wherein: the lever (3) passes through the rotating shaft (17), one end of the lever (3) forms a lever power arm (302), the other end of the lever forms a lever resistance arm (301), and the ratio of the lever power arm (302) to the lever resistance arm (301) is 1:10.
6. An airborne target display console as in claim 1, wherein: the baffle (2) and the lever resistance arm (301) are integrally formed, and the baffle (2) is perpendicular to the lever resistance arm (301).
7. An airborne target display console as in claim 1, wherein: the utility model is characterized in that the middle position of the upper surface wall of the model base (16) and the middle position of the bottom of the airplane model (1) are respectively provided with a round threaded hole with the diameter of 3.1mm, the vertical rod (15) is of a cylindrical structure with the diameter of 3mm and the length of 14cm, the top end and the bottom end of the vertical rod (15) are respectively provided with threads, the top end of the vertical rod (15) stretches into the threaded hole formed in the bottom of the airplane model (1) to be in threaded connection with the airplane model (1), and the bottom end of the vertical rod (15) stretches into the threaded hole formed in the upper surface wall of the model base (16) to be in threaded connection with the model base (16).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811617505.7A CN109489478B (en) | 2018-12-28 | 2018-12-28 | Aerial target display console |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811617505.7A CN109489478B (en) | 2018-12-28 | 2018-12-28 | Aerial target display console |
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| CN109489478A CN109489478A (en) | 2019-03-19 |
| CN109489478B true CN109489478B (en) | 2023-09-01 |
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| CN201811617505.7A Active CN109489478B (en) | 2018-12-28 | 2018-12-28 | Aerial target display console |
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| CN109489478A (en) | 2019-03-19 |
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