CN114027289A - Titanium radium bullet bird repellent device with compressed air as power - Google Patents
Titanium radium bullet bird repellent device with compressed air as power Download PDFInfo
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- CN114027289A CN114027289A CN202111312940.0A CN202111312940A CN114027289A CN 114027289 A CN114027289 A CN 114027289A CN 202111312940 A CN202111312940 A CN 202111312940A CN 114027289 A CN114027289 A CN 114027289A
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- bullet
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- clamping block
- support plate
- feeding
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- A—HUMAN NECESSITIES
- A01—AGRICULTURE; FORESTRY; ANIMAL HUSBANDRY; HUNTING; TRAPPING; FISHING
- A01M—CATCHING, TRAPPING OR SCARING OF ANIMALS; APPARATUS FOR THE DESTRUCTION OF NOXIOUS ANIMALS OR NOXIOUS PLANTS
- A01M29/00—Scaring or repelling devices, e.g. bird-scaring apparatus
- A01M29/16—Scaring or repelling devices, e.g. bird-scaring apparatus using sound waves
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41F—APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
- F41F1/00—Launching apparatus for projecting projectiles or missiles from barrels, e.g. cannons; Harpoon guns
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B30/00—Projectiles or missiles, not otherwise provided for, characterised by the ammunition class or type, e.g. by the launching apparatus or weapon used
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- Life Sciences & Earth Sciences (AREA)
- General Engineering & Computer Science (AREA)
- Birds (AREA)
- Insects & Arthropods (AREA)
- Pest Control & Pesticides (AREA)
- Wood Science & Technology (AREA)
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Abstract
The invention provides a titanium laser bomb bird repelling device which is convenient to charge and capable of improving the launching height and precision and takes compressed air as power, and relates to the technical field of bird repelling equipment. A titanium laser bomb bird repellent device taking compressed air as power comprises a launching tube, an air inlet pipe and a bomb pushing device arranged on the side face of the launching tube; the bullet pushing device comprises a bullet pushing linear driving mechanism, a bullet feeding barrel, a bullet feeding block and a clamping head for clamping a bullet; the front end of the bullet feeding cylinder is communicated with the bullet chamber, the bullet feeding block is arranged in the bullet feeding cylinder and is in sliding fit with the bullet feeding cylinder, a sealing ring is arranged between the bullet feeding block and the bullet feeding cylinder, and the bullet pushing linear driving mechanism is connected with the bullet feeding block so as to drive the bullet feeding block to slide back and forth along the bullet feeding cylinder; the clamping head is arranged at the front end of the bullet feeding block and comprises a left clamping block and a right clamping block. The device has high launching height and precision and good bird repelling effect.
Description
Technical Field
The invention relates to the technical field of bird repelling equipment, in particular to a titanium radium bomb bird repelling device with compressed air as power.
Background
A titanium laser bomb bird repelling device is a bird repelling device commonly used in airports and is used for repelling birds by emitting titanium laser bombs. The titanium laser bomb bird repelling device has the working characteristics of rapidness and controllability, the angle of the gun barrel of the titanium laser bomb bird repelling device can be adjusted rapidly according to the position of a bird group, the explosion point of the titanium laser bomb is close to the bird group, and therefore the bird repelling effect is good.
The existing titanium laser bomb bird repellent device mainly utilizes a large current to detonate an electronic detonator, the electronic detonator detonates propelling gunpowder of the titanium laser bomb while detonated, and the titanium laser bomb is emitted out of a gun barrel under the action of primary detonation generated by the propelling gunpowder. The launching mode needs the titanium radium bomb to be equipped with launching gunpowder, the bird repelling cost is high, and the problem of environmental pollution exists during launching.
Application number 200820089138.3 discloses a compressed air emitter, the device's emission mechanism comprises gas holder, ball valve, angle of elevation guiding mechanism, position adjustment structure etc. and the gas holder communicates with each other with the launching tube through the pipeline, and the ball valve setting is on the pipeline with control gas holder to the launching tube air feed. The launching device achieves the purposes of launching fireworks and fire extinguishing bombs by introducing compressed air into the launching tube, and solves the problem of launching pollution. When the device is used, the shell is loaded from the upper end of the launching tube, so that the loading is inconvenient, the constraint on the shell is poor (the shell and the launching tube are in clearance fit) during launching, the launching height and precision are greatly low, and the bird repelling effect is not ideal enough.
Disclosure of Invention
The invention aims to solve the technical problem of providing a titanium laser bomb bird repellent device which is convenient to charge and can improve the launching height and precision and takes compressed air as power.
The technical scheme adopted by the invention for solving the technical problems is as follows: a titanium laser bomb bird repellent device taking compressed air as power comprises a launching tube and an air inlet tube, wherein one end of the air inlet tube is communicated with the lower end of the launching tube, and a bomb chamber is arranged in the launching tube; the launching device is arranged on one side of the launching barrel;
the bullet pushing device comprises a bullet pushing linear driving mechanism, a bullet feeding barrel, a bullet feeding block and a clamping head for clamping a bullet; the front end of the bullet feeding cylinder is communicated with the bullet chamber, the bullet feeding block is arranged in the bullet feeding cylinder and is in sliding fit with the bullet feeding cylinder, a sealing ring is arranged between the bullet feeding block and the bullet feeding cylinder, and the bullet pushing linear driving mechanism is connected with the bullet feeding block so as to drive the bullet feeding block to slide back and forth along the bullet feeding cylinder; the clamping head is arranged at the front end of the bullet feeding block and comprises a left clamping block and a right clamping block, the left clamping block is connected with the bullet feeding block in a sliding mode along the sliding direction of the bullet feeding block, a bullet clamping spring enabling the left clamping block to be far away from the bullet feeding block is arranged between the left clamping block and the bullet feeding block, the right clamping block is arranged at the front end of the left clamping block and opposite to the left clamping block, the right clamping block and the left clamping block are matched to form a clamping cavity, the right clamping block is connected with the left clamping block in a sliding mode along the sliding direction of the bullet feeding block, a bullet loading spring enabling the right clamping block to be far away from the left clamping block is arranged between the right clamping block and the left clamping block, and a bullet loading hole for loading bullets to the clamping cavity is formed in the bullet feeding barrel;
the inside of the cartridge chamber is provided with a positioning plate which is matched with the right clamping block so that the clamping head clamps the shell.
Furthermore, a limiting table for limiting the advancing stroke of the bullet feeding block is arranged on the bullet feeding barrel.
Furthermore, one side of the positioning plate surface, which is provided with the right clamping block, is provided with a V-shaped groove, and one side of the right clamping block, which faces the positioning plate, is provided with a bulge matched with the V-shaped groove.
Further, still include gas holder and pulse valve, the gas holder is connected through the other end of pulse valve with the intake pipe.
Further, the launching tube comprises a launching tube section and a chamber seat section, the cartridge chamber is arranged in the chamber seat section, and the launching tube section is detachably connected with the chamber seat section.
The device further comprises a bullet storage device, wherein the bullet storage device comprises a motor, a rotary disc, a first bullet falling control mechanism and a plurality of bullet storage barrels; the carousel cover is established on the launching tube to with launching tube normal running fit, store up the bomb tube and be the annular around the rotation center of carousel and arrange on the carousel, the lower extreme of storing up the bomb tube is equipped with the first backup pad that can open and shut in order to be used for controlling to store up the bomb tube and fall the bullet, the motor is connected with the carousel transmission to the drive carousel rotates, will store up the bomb tube and remove to falling the bullet position, first fall bullet control mechanism and the cooperation of first backup pad for controlling opening and shutting of first backup pad.
Further, the first bullet dropping control mechanism comprises a first return spring and a stop dog; the first support plate is hinged with the bullet storage barrel through a hinge shaft, one end of the first reset spring is connected with the bullet storage barrel, and the other end of the first reset spring is connected with the first support plate, so that the first support plate is kept in a closed state; the dog passes through support and launch canister rigid coupling, when storage bomb moved to falling bullet position, dog and first backup pad cooperation make first backup pad rotate around the hinge to make first backup pad open.
The ignition device is connected with the sliding frame in a sliding manner along the radial direction of the bullet loading hole, a second return spring is arranged between the ignition device and the sliding frame, and an ignition head of the ignition device extends into the bullet loading hole;
the bullet storage device also comprises a bullet feeding linear driving mechanism, a second bullet dropping control mechanism and a bullet support for receiving bullets in the bullet storage barrel at the bullet loading position; the feeding linear driving mechanism is arranged on the support and connected with the bullet holder so as to move the bullet holder to the position above the bullet loading hole along the radial direction of the bullet loading hole, and the lower end of the bullet holder is also provided with a second supporting plate which can be opened and closed; the bullet holder is fixedly connected with a first reversing rod and a second reversing rod, the first reversing rod is provided with a guide groove, the sliding frame is fixedly provided with a pin which is in sliding fit with the guide groove, the guide groove comprises a straight section and an inclined section which enables the sliding frame to be far away from the bullet loading hole along the axis direction of the bullet loading hole, the straight section is arranged along the moving direction of the bullet holder, and the pin is inserted in the inclined section; the second reversing rod is provided with an inclined plane which is matched with the ignition device so as to enable the ignition device to be far away from the bullet loading hole along the radial direction of the bullet loading hole, and the position of the inclined plane corresponds to the position of the straight section; the second bullet falling control mechanism is matched with the second supporting plate and used for controlling the opening and closing of the second supporting plate.
Further, the second bullet dropping control mechanism comprises a third return spring and a stop pin; the second support plate is hinged with the elastic support, one end of the third reset spring is connected with the second support plate, and the other end of the third reset spring is connected with the elastic support, so that the second support plate is kept in a closed state; the stop pin is fixedly arranged on the bullet feeding barrel and is matched with the second supporting plate to open the second supporting plate.
The launching tube is hinged to the launching tube, and the cover body is connected with the cover body to control the opening and closing of the cover body.
The invention has the beneficial effects that: the device adopts and pushes away the bullet device and send into the shell chamber with the shell, and the loading is convenient, and pushes away the tight head of clamp of bullet device and can provide certain centre gripping pretightning force to the shell when the transmission, can realize the accurate coaxial positioning of shell and launching tube, and the transmission height and the precision of device drive the bird effect better.
Drawings
FIG. 1 is a schematic structural view of the present invention;
FIG. 2 is a top view of FIG. 1;
FIG. 3 is a schematic view of the mounting structure of the projectile apparatus;
FIG. 4 is a schematic structural view of a launch canister;
FIG. 5 is a cross-sectional view taken along A-A of FIG. 1;
FIG. 6 is an enlarged view at B in FIG. 5;
FIG. 7 is a cross-sectional view taken along E-E of FIG. 2;
FIG. 8 is a cross-sectional view taken along F-F of FIG. 7;
FIG. 9 is an enlarged view at D of FIG. 8;
FIG. 10 is a schematic view of the installation of the ignition device;
FIG. 11 is a schematic view of the structure of the first guide bar;
FIG. 12 is a schematic view of the mounting structure of the second support plate;
shown in the figure: the projectile firing device comprises a launching tube 1, an air inlet tube 2, a projectile pushing device 3, an ignition device 4, a projectile storage device 5, an air storage tank 6, a pulse valve 7, a projectile 8, a projectile chamber 11, a launching tube section 12, a chamber seat section 13, a taper hole flange 14, a support 15, an uncovering driving device 16, a cover 17, a projectile pushing linear driving mechanism 31, a projectile feeding tube 32, a projectile feeding block 33, a clamping head 34, a clamping cavity 35, a projectile clamping spring 36, a projectile loading spring 37, a sealing ring 38, a projectile loading hole 39, a sliding block 41, an ignition head 42, a collision tongue 43, a motor 51, a projectile storage tube 52, a rotating disc 53, a projectile feeding linear driving mechanism 54, a projectile holder 55, a sliding carriage 56, a first reversing rod 57, a second reversing rod 58, a second return spring 59, a positioning plate 111, a V-shaped groove 112, a limit table 331, a left clamping block 341, a right clamping block 342, a guide post 343, a guide rod 344, a first support plate 521, a first return spring stop block 523, a hinge shaft 524, a second support plate 551, a third return spring 552, a stop pin 553, a pin 561, a guide slot 571, a straight section 572, an inclined section 573, and a ramp 581.
Detailed Description
The invention is further illustrated with reference to the following figures and examples.
As shown in fig. 1 to 6, the titanium radium bomb bird repelling device using compressed air as power comprises a launching tube 1, an air inlet tube 2, a bomb chamber 11 and a bomb pushing device 3, wherein one end of the air inlet tube 2 is communicated with the lower end of the launching tube 1, and the bomb pushing device 3 is arranged on one side of the launching tube 1. The projectile apparatus 3 comprises a projectile linear drive mechanism 31, a feed barrel 32, a feed block 33 and a clamping head 34 for clamping the projectile. The front end of the bullet feeding barrel 32 is communicated with the bullet chamber 11, and the bullet feeding block 33 is arranged in the bullet feeding barrel 32 and is in sliding fit with the bullet feeding barrel 32, so that the bullet feeding block 33 can slide along the bullet feeding barrel 32. A seal 38 is provided between the projectile block 33 and the projectile barrel 32 to prevent leakage from a gap between the projectile block and the projectile barrel 32. The bullet pushing linear driving mechanism 31 is connected with the bullet feeding block 33 so as to drive the bullet feeding block 33 to slide back and forth along the bullet feeding barrel 32; the clamping head 34 is arranged at the front end of the bullet feeding block 33 (the direction close to the bullet chamber 11 is the front direction), and comprises a left clamping block 341 and a right clamping block 342, the left clamping block 341 is connected with the bullet feeding block 33 in a sliding manner along the sliding direction of the bullet feeding block 33 through a guide rod 344, a bullet clamping spring 36 enabling the left clamping block 341 to be far away from the bullet feeding block 33 is arranged between the left clamping block 341 and the bullet feeding block 33, the right clamping block 342 is arranged at the front end of the left clamping block 341 and is opposite to the left clamping block 341, the right clamping block 342 is matched with the left clamping block 341 to form a clamping cavity 35, the right clamping block 342 is connected with the left clamping block 341 in a sliding manner along the bullet feeding block 33 through a guide rod 343, and a bullet loading spring 37 enabling the right clamping block 342 to be far away from the left clamping block 341 is arranged between the right clamping block 342 and the left clamping block 341. The cartridge chamber 11 is provided with a positioning plate 111 which cooperates with the right clamping block 342 so that the clamping head 34 clamps the projectile, and the positioning plate 111 may be a wall of the cartridge chamber 11. The cartridge feed cylinder 32 is provided with a loading hole 39 for loading the cartridge into the holding chamber 35.
When the device is used, the other end of the air inlet pipe 2 is communicated with an air storage tank, and shells 8 (titanium laser shells) are loaded into the clamping cavity 35 of the clamping head 34 from the loading hole 39 during loading. Because the loading spring 37 which enables the right clamping block 342 to be far away from the left clamping block 341 is arranged between the right clamping block 342 and the left clamping block 341, the clamping head 34 can keep an opening state under the action of the loading spring 37, and the inner diameter of the clamping cavity 35 is larger than the outer diameter of the shell at the moment, so that the shell can be conveniently loaded. When the shell is loaded into the clamping cavity 35, the projectile pushing linear driving mechanism 31 pushes the projectile feeding block 33 to slide forwards (close to the chamber 11) along the projectile feeding barrel 32, and the clamping head 34 pushed by the projectile feeding block 33 moves, so that the shell 8 is fed into the chamber 11. During the process of feeding the shell into the shell chamber 11, the clamping head 34 gradually enters the shell chamber 11, and along with the continuous movement of the shell feeding block, the positioning plate 111 is matched with the right clamping block 342 to limit the movement of the right clamping block 342, so that the right clamping block 342 and the left clamping block 341 are pressed together to close the clamping cavity 35, and the clamping head 34 provides a certain clamping pretightening force for the shell. When the clamping cavity 35 is closed, the bullet pushing linear driving mechanism 31 stops pushing the bullet feeding block 33. During the transmission, let in compressed gas from the lower extreme of launching tube 1, the propelling force of compressed gas promotes the shell and removes after being greater than the frictional force between shell and the compact heap to launch the shell. The left clamping block 341 is connected with the bullet feeding block 33 in a sliding manner along the sliding direction of the bullet feeding block 33, and a bullet clamping spring 36 for enabling the left clamping block 341 to be far away from the bullet feeding block 33 is arranged between the left clamping block 341 and the bullet feeding block 33, so that the phenomenon that the cannonball is clamped can be avoided, and the clamping pretightening force of the cannonball can be adjusted by replacing the bullet clamping spring 36 or adjusting the length of the bullet clamping spring 36. The device adopts and pushes away bullet device 3 and sends into cartridge chamber 11 with the shell, and the loading is convenient, and pushes away the tight head 34 of clamp of bullet device 3 and can provide certain centre gripping pretightning force to the shell when the transmission, through above-mentioned structure pretension centre gripping, can realize the accurate coaxial positioning of shell and launching tube, can show hoisting device's transmission height and precision, and is better to high altitude bird's dispersing effect.
The launch canister 1 may be of unitary construction but is not so convenient to manufacture and machine. As shown in figure 4, for the convenience of manufacturing and processing, the launching tube 1 comprises a launching tube section 12 and a chamber seat section 13, a cartridge chamber 11 is arranged in the chamber seat section 13, and the launching tube section 12 is detachably connected with the chamber seat section 13. The above structure can also be replaced after the barrel section 12 is worn, since the barrel section 12 is worn. Specifically, the lower end of the launching tube section 12 is inserted into the bore seat section 13, the conical hole flange 14 is sleeved on the launching tube section 12, the launching tube section 12 is in press connection with the bore seat section 13 through the matching of the conical hole of the launching tube section 12, and the conical hole flange 14 is in bolt connection with the launching tube section 12. Of course, the barrel section 12 may also be bolted or screwed directly to the bore seat section 13.
The advancing stroke of the bullet feeding block can be realized by controlling the bullet pushing linear driving mechanism 31, and the bullet feeding barrel 32 is provided with a limit table 331 for limiting the advancing stroke of the bullet feeding block 33. Therefore, when the bullet feeding block moves forwards to the limiting table 331, the bullet feeding block stops automatically, positioning is more accurate, and the clamping pretightening force of each shooting can be guaranteed to be the same.
In the invention, a V-shaped groove 112 is formed on one side of the positioning plate 111 facing the right clamping block 342, and a protrusion matched with the V-shaped groove 112 is formed on one side of the right clamping block 342 facing the positioning plate 111. Therefore, in the loading process of the cannonball, the V-shaped groove 112 is matched with the protrusion of the right clamping block 342, the movement of the right clamping block 342 is limited, and meanwhile, the V-shaped groove 112 also plays a centering role in the clamping head 34, so that the eccentricity caused by gaps between the clamping blocks and the cannonball feeding blocks can be eliminated, and the coaxiality of the cannonball and the cannonball can be further improved.
The ejection linear driving mechanism 31 may be a linear motor, a hydraulic cylinder, an air cylinder, etc., and the ejection linear driving mechanism 31 in the embodiment of the present invention employs an air cylinder.
The launching device also comprises an air storage tank 6 and a pulse valve 7, wherein the air storage tank 6 is connected with the other end of the air inlet pipe 2 through the pulse valve 7.
The launching device can be provided with an elevation angle adjusting mechanism and an azimuth adjusting mechanism according to the requirement.
The invention further comprises a cartridge magazine 5, as shown in fig. 7, the cartridge magazine 5 comprises a motor 51, a turntable 53, a first cartridge drop control mechanism and a plurality of cartridge storage barrels 52. The turntable 53 is sleeved on the launching tube 1 and is in running fit with the launching tube 1 to reduce the occupied space of the launching device. The magazine 52 is arranged on the turntable 53 in a ring around the center of rotation of the turntable 53, preferably in a uniform manner. The lower end of the bullet storage cylinder 52 is provided with a first supporting plate 521 which can be opened and closed and is used for controlling the bullet falling of the bullet storage cylinder 52, and the motor 51 is in transmission connection with the rotating disc 53 through a gear so as to drive the rotating disc 53 to rotate and move the bullet storage cylinder 52 to the bullet falling position. The bullet dropping position can be any orientation of the rotating disc. Chain and belt transmission can also be adopted between the motor 51 and the turntable 53. The first bullet dropping control mechanism is matched with the first support plate 521 and used for controlling the opening and closing of the first support plate 521. The first support plate 521 is supported at the lower end of the storage barrel 52 in a normal state to prevent the shells in the storage barrel from falling, when the motor 51 moves the storage barrel 52 to the shell falling position, the first shell falling control mechanism opens the first support plate 521, the shells stored in the storage barrel 52 lose support and fall under the action of gravity, and therefore the shells can be fed into the loading hole 39. After adopting above-mentioned structure, the dress bullet is convenient.
The first supporting plate 521 can be inserted, hinged, etc. at the lower end of the cartridge 52 to be openable. The first bullet falling control mechanism can be a motor, an air cylinder, a hydraulic cylinder and the like which are matched with the first supporting plate. As shown in fig. 8 and 9, specifically, the first drop control mechanism includes a first return spring 523 and a stopper 524; the first support plate 521 is hinged to the cartridge 52 by a hinge shaft 525. The first return spring 523 has one end connected to the cartridge 52 and the other end connected to the first support plate 521 so as to keep the first support plate 521 in a closed state. The stopper 524 is fixedly connected with the launching tube 1 through the bracket 15, and when the bullet storage tube 52 moves to the bullet falling position, the stopper 524 is matched with the first support plate 521, so that the first support plate 521 rotates around the hinge shaft 525, and the first support plate 521 is opened. When the launch barrel 1 leaves the bullet dropping position, the stop block 524 is separated from the first support plate 521, and the first support plate 521 is reset (in a closed state) under the action of the first reset spring 523. The structure can realize the automatic bullet falling control of the bullet storage barrel 52, and the mode has the advantages of simple and reliable work, small occupied space, no need of a complex electromechanical control system and low manufacturing cost.
For the convenience of ignition, the launching device of the present invention further comprises an ignition device 4, wherein a carriage 56 is provided on the support 15, and the carriage 56 is slidably connected with the support 15 along the axial direction of the loading hole 39, so that the carriage 56 can be far away from the loading hole 39 along the axial direction of the loading hole 39. The ignition device 4 is slidably connected to the carriage 56 by the slider 41 in the radial direction of the loading hole 39, so that the ignition device 4 can be moved away from the loading hole 39 in the radial direction of the loading hole 39. The ignition head 42 of the ignition device 4 extends into the loading hole 39, and a second return spring 59 is arranged between the ignition device 4 and the carriage 56. The storage device 5 further comprises a feeding linear driving mechanism 54, a second drop control mechanism and a support 55 for receiving the shell in the storage barrel 52 at the loading position. The feeding linear driving mechanism 54 is mounted on the frame 15 and connected to the magazine 55 to move the magazine 55 in the radial direction of the loading hole 39 to above the loading hole 39, and the lower end of the magazine 55 is also provided with a second support plate 551 which can be opened and closed. The second support plate 551 serves to control the dropping of the projectile from the sabot 55. The elastic support 55 is fixedly connected with a first reversing rod 57 and a second reversing rod 58, the first reversing rod 57 is provided with a guide groove 571, the carriage 56 is fixedly provided with a pin 561 in sliding fit with the guide groove 571, the guide groove 571 comprises a straight section 572 and an inclined section 573 capable of enabling the carriage 56 to be far away from the elastic loading hole 39 along the axial direction of the elastic loading hole 39, the straight section 572 is arranged along the moving direction of the elastic support 55, the inclined section 573 and the straight section 572 form a certain included angle, and the pin 561 is inserted into the inclined section 573; the second reversing lever 58 is provided with an inclined plane 581 which is matched with the ignition device 4 so as to lead the ignition device 4 to be far away from the loading hole 39 along the radial direction of the loading hole 39, and the position of the inclined plane 581 corresponds to the position of the straight section 572; the second bullet dropping control mechanism is matched with the second support plate 551 and is used for controlling the opening and closing of the second support plate 551.
When the shell in the storage barrel 52 in the loading position drops into the sabot, the sabot 55 is driven by the feed linear drive mechanism 54 to move, and the sabot 55 is moved above the loading hole 39. The bullet holder 55 drives the first reversing rod 57 and the second reversing rod 58 to move together during the movement, and during the movement of the first reversing rod 57, the inclined section 573 is engaged with the pin 561, so that the carriage 56 is gradually separated from the bullet loading hole 39 along the axial direction of the bullet loading hole 39, and further, the ignition device 4 on the carriage 56 is separated along the axial direction of the bullet loading hole 39, so that the ignition head 42 of the ignition device 4 can be removed from the bullet loading hole 39. When the ignition head 42 of the ignition device 4 is removed from the loading hole 39, the pin 561 slides to the straight section 572, and the pin 561 moves along the straight section 572, while the position of the carriage 56 in the axial direction of the loading hole 39 remains unchanged. Since the inclined plane 581 is located corresponding to the straight section 572, when the pin 561 slides to the straight section 572, the inclined plane 581 is engaged with the ignition device 4 (in the figure, the inclined plane 581 is engaged with the ignition device 4 through the striking tongue 43 fixed to the slider 41), the inclined plane 581 generates a component force on the ignition device 4, which makes the ignition device 4 radially outward along the loading hole 39, and as the sabot 55 continues to move, the inclined plane 581 pushes the ignition device 4 radially outward along the loading hole 39 away from the loading hole 39, so that the firing head of the ignition device 4 does not interfere with the loading, and the shell of the sabot 55 is conveniently dropped into the loading hole 39. When the support 55 moves above the loading hole 39, the second drop control mechanism opens the second support plate 551, the shell drops into the loading hole 39, and the feeding linear driving mechanism 54 drives the support 55 to return. During the return of the sabot 55, the inclined plane 581 is not engaged with the ignition device 4, the ignition device 4 is reset in the radial direction of the loading hole 39 by the second return spring 59, the pin 561 moves along the inclined section 573 as the sabot 55 is returned, the ignition device 4 is reset in the axial direction of the loading hole 39, and the ignition head of the ignition device 4 is extended into the loading hole 39 again to ignite the shell. The fired shell is pushed into the firing chamber by the shell pushing device to be fired. The automatic withdrawing and returning function of the ignition head realized by the mechanical linkage does not need an electrical control system, and has the advantages of simple structure, low manufacturing cost and high reliability.
The second support plate 551 may be inserted, hinged, etc. at the lower end of the elastic support 55 to be openable. The second bullet dropping control mechanism can also adopt a motor, a hydraulic cylinder, an air cylinder and the like to be matched with the second support plate 551. The second drop control mechanism of the present invention includes a third return spring 552 and a stopper pin 553; the second support plate 551 is hinge-connected to the elastic support 55, and the third return spring 552 has one end connected to the second support plate 551 and the other end connected to the elastic support 55 so that the second support plate 551 maintains a closed state. The stop pin 553 is fixedly disposed on the feeding cylinder 32 and cooperates with the second support plate 551 to open the second support plate 551. When the magazine 55 moves to the loading hole 39, the stopper pin 553 engages with the second support plate 551, and as the magazine 55 continues to move, the stopper pin 553 pushes the second support plate 551 to rotate, thereby opening the second support plate 551. When the magazine 55 returns, the second support plate 551 returns by the third return spring 552 to be closed for the next loading. The mode has simple and reliable operation, small occupied space, no need of a complex electromechanical control system and low manufacturing cost.
The bullet feeding linear driving mechanism adopts an air cylinder, and a hydraulic cylinder, a linear motor and the like can be adopted.
The launching device adopts the structure and is matched with a corresponding control system, so that automatic loading, ignition and launching can be realized.
In order to prevent rainwater from entering the launching tube, the invention is provided with an uncovering driving device 16 on one side of the launching tube 1, the upper end of the launching tube 1 is provided with an openable cover 17, the cover body 17 is hinged with the launching tube 1, and the uncovering driving device 16 is connected with the cover body 17 to control the opening and closing of the cover body 16. The cover opening driving device can be an air cylinder, a motor, a hydraulic cylinder and the like.
Claims (10)
1. A titanium laser bomb bird repellent device taking compressed air as power comprises a launching tube (1) and an air inlet tube (2), wherein one end of the air inlet tube (2) is communicated with the lower end of the launching tube (1), and a bomb chamber (11) is arranged in the launching tube (1); the method is characterized in that: the launching device also comprises a bullet pushing device (3) arranged on one side of the launching tube (1);
the projectile pushing device (3) comprises a projectile pushing linear driving mechanism (31), a projectile feeding barrel (32), a projectile feeding block (33) and a clamping head (34) for clamping a projectile; the front end of the bullet feeding cylinder (32) is communicated with the bullet chamber (11), the bullet feeding block (33) is arranged in the bullet feeding cylinder (32) and is in sliding fit with the bullet feeding cylinder (32), a sealing ring (38) is arranged between the bullet feeding block (33) and the bullet feeding cylinder (32), and the bullet pushing linear driving mechanism (31) is connected with the bullet feeding block (33) so as to drive the bullet feeding block (33) to slide back and forth along the bullet feeding cylinder (32); the clamping head (34) is arranged at the front end of the bullet feeding block (33) and comprises a left clamping block (341) and a right clamping block (342), the left clamping block (341) is in sliding connection with the bullet feeding block (33) along the sliding direction of the bullet feeding block (33), a bullet clamping spring (36) enabling the left clamping block (341) to be far away from the bullet feeding block (33) is arranged between the left clamping block (341) and the bullet feeding block (33), the right clamping block (342) is arranged at the front end of the left clamping block (341) and is opposite to the left clamping block (341), the right clamping block (342) and the left clamping block (341) are matched to form a clamping cavity (35), the right clamping block (342) is in sliding connection with the left clamping block (341) along the sliding direction of the bullet feeding block (33), and a bullet loading spring (37) enabling the right clamping block (342) to be far away from the left clamping block (341) is arranged between the right clamping block (342) and the left clamping block (341), the bullet feeding cylinder (32) is provided with a bullet loading hole (39) for loading bullets to the clamping cavity (35);
the cartridge chamber (11) is internally provided with a positioning plate (111) which is matched with the right clamping block (342) so that the clamping head (34) clamps the cannonball.
2. The titanium laser bomb bird repelling device powered by compressed air as claimed in claim 1, wherein: the bullet feeding cylinder (32) is provided with a limit table (331) for limiting the advancing stroke of the bullet feeding block (33).
3. The titanium laser bomb bird repelling device powered by compressed air as claimed in claim 1, wherein: one side of the positioning plate (111) facing the right clamping block (342) is provided with a V-shaped groove (112), and one side of the right clamping block (342) facing the positioning plate (111) is provided with a bulge matched with the V-shaped groove (112).
4. The titanium laser bomb bird repelling device powered by compressed air as claimed in claim 1, wherein: still include gas holder (6) and pulse valve (7), gas holder (6) are connected through pulse valve (7) and the other end of intake pipe (2).
5. The titanium laser bomb bird repelling device powered by compressed air as claimed in claim 1, wherein: the launching tube (1) comprises a launching tube section (12) and a chamber seat section (13), the cartridge chamber (11) is arranged in the chamber seat section (13), and the launching tube section (12) is detachably connected with the chamber seat section (13).
6. The titanium laser bomb bird repelling device powered by compressed air as claimed in claim 1, wherein: the automatic bullet falling device is characterized by further comprising a bullet storage device (5), wherein the bullet storage device (5) comprises a motor (51), a rotating disc (53), a first bullet falling control mechanism and a plurality of bullet storage barrels (52); carousel (53) cover is established on launching tube (1) to with launching tube (1) normal running fit, storage cylinder (52) are the annular around the rotation center of carousel (53) and arrange on carousel (53), the lower extreme of storage cylinder (52) is equipped with the first backup pad (521) that can open and shut in order to be used for controlling storage cylinder (52) to fall the bullet, motor (51) are connected with carousel (53) transmission to drive carousel (53) and rotate, will store up cylinder (52) and move to falling the bullet position, first bullet control mechanism and first backup pad (521) cooperation of falling is used for controlling opening and shutting of first backup pad (521).
7. The titanium laser bomb bird repelling device powered by compressed air as claimed in claim 6, wherein: the first bullet dropping control mechanism comprises a first return spring (523) and a stop block (524); the first support plate (521) is hinged with the bullet storage barrel (52) through a hinge shaft (525), one end of the first return spring (523) is connected with the bullet storage barrel (52), and the other end of the first return spring is connected with the first support plate (521), so that the first support plate (521) is kept in a closed state; the stop block (524) is fixedly connected with the launching tube (1) through the bracket (15), and when the bullet storage tube (52) moves to the bullet falling position, the stop block (524) is matched with the first support plate (521), so that the first support plate (521) rotates around the hinge shaft (525), and the first support plate (521) is opened.
8. The titanium laser bomb bird repelling device powered by compressed air as claimed in claim 7, wherein: the ignition device is characterized by further comprising an ignition device (4), a sliding frame (56) is arranged on the support (15), the sliding frame (56) is connected with the support (15) in a sliding mode along the axial direction of the bullet loading hole (39), the ignition device (4) is connected with the sliding frame (56) in a sliding mode along the radial direction of the bullet loading hole (39), a second return spring (59) is arranged between the ignition device (4) and the sliding frame (56), and an ignition head of the ignition device (4) extends into the bullet loading hole (39);
the bullet storage device (5) further comprises a bullet feeding linear driving mechanism (54), a second bullet dropping control mechanism and a bullet support (55) for receiving bullets in the bullet storage barrel (52) at the bullet loading position; the feeding linear driving mechanism (54) is installed on the support (15) and connected with the bullet holder (55) so as to move the bullet holder (55) to the position above the bullet loading hole (39) along the radial direction of the bullet loading hole (39), and the lower end of the bullet holder (55) is also provided with a second support plate (551) capable of being opened and closed; the bullet holder (55) is fixedly connected with a first reversing rod (57) and a second reversing rod (58), the first reversing rod (57) is provided with a guide groove (571), the sliding frame (56) is fixedly provided with a pin (561) in sliding fit with the guide groove (571), the guide groove (571) comprises a straight section (572) and an inclined section (573) capable of enabling the sliding frame (56) to be far away from the bullet loading hole (39) along the axial direction of the bullet loading hole (39), the straight section (572) is arranged along the moving direction of the bullet holder (55), and the pin (561) is inserted into the inclined section (573); the second reversing rod (58) is provided with a bevel (581) which is matched with the ignition device (4) so as to enable the ignition device (4) to be far away from the bullet loading hole (39) along the radial direction of the bullet loading hole (39), and the position of the bevel (581) corresponds to the position of the straight section (572); the second bullet falling control mechanism is matched with the second support plate (551) and used for controlling the opening and closing of the second support plate (551).
9. The titanium laser bomb bird repelling device powered by compressed air as claimed in claim 8, wherein: the second bullet dropping control mechanism comprises a third return spring (552) and a stop pin (553); the second support plate (551) is hinged with the elastic support (55), one end of the third return spring (552) is connected with the second support plate (551), and the other end of the third return spring is connected with the elastic support (55) so as to keep the second support plate (551) in a closed state; the stop pin (553) is fixedly arranged on the bullet feeding barrel (32) and is matched with the second support plate (551) to open the second support plate (551).
10. The titanium laser bomb bird repelling device powered by compressed air as claimed in claim 1, wherein: the launching tube is characterized by further comprising a cover opening driving device (16) arranged on one side of the launching tube (1), a cover body (17) capable of being opened and closed is arranged at the upper end of the launching tube (1), the cover body (17) is hinged to the launching tube (1), and the cover opening driving device (16) is connected with the cover body (17) to control the opening and closing of the cover body (17).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202111312940.0A CN114027289B (en) | 2021-11-08 | 2021-11-08 | Titanium radium bullet bird repellent device with compressed air as power |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202111312940.0A CN114027289B (en) | 2021-11-08 | 2021-11-08 | Titanium radium bullet bird repellent device with compressed air as power |
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| CN114027289A true CN114027289A (en) | 2022-02-11 |
| CN114027289B CN114027289B (en) | 2023-01-20 |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115156990A (en) * | 2022-08-10 | 2022-10-11 | 吴廷山 | Digit control machine tool with function of putting out a fire |
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| CN115156990A (en) * | 2022-08-10 | 2022-10-11 | 吴廷山 | Digit control machine tool with function of putting out a fire |
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|---|---|
| CN114027289B (en) | 2023-01-20 |
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