CN109911209B - Airborne anti-riot projectile emitter and unmanned aerial vehicle - Google Patents
Airborne anti-riot projectile emitter and unmanned aerial vehicle Download PDFInfo
- Publication number
- CN109911209B CN109911209B CN201910329433.4A CN201910329433A CN109911209B CN 109911209 B CN109911209 B CN 109911209B CN 201910329433 A CN201910329433 A CN 201910329433A CN 109911209 B CN109911209 B CN 109911209B
- Authority
- CN
- China
- Prior art keywords
- riot
- rotating wheel
- sleeve
- projectile launcher
- servo
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
- 238000010304 firing Methods 0.000 claims abstract description 49
- 230000007246 mechanism Effects 0.000 claims abstract description 47
- 230000008878 coupling Effects 0.000 claims description 16
- 238000010168 coupling process Methods 0.000 claims description 16
- 238000005859 coupling reaction Methods 0.000 claims description 16
- 238000003331 infrared imaging Methods 0.000 claims description 4
- 230000006835 compression Effects 0.000 claims description 3
- 238000007906 compression Methods 0.000 claims description 3
- 238000000034 method Methods 0.000 description 10
- 239000007789 gas Substances 0.000 description 3
- 230000008569 process Effects 0.000 description 3
- 230000009471 action Effects 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000004146 energy storage Methods 0.000 description 2
- 206010063385 Intellectualisation Diseases 0.000 description 1
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 1
- 238000010521 absorption reaction Methods 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 230000000903 blocking effect Effects 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 239000003814 drug Substances 0.000 description 1
- 238000004043 dyeing Methods 0.000 description 1
- 239000006260 foam Substances 0.000 description 1
- 230000010354 integration Effects 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- IMACFCSSMIZSPP-UHFFFAOYSA-N phenacyl chloride Chemical compound ClCC(=O)C1=CC=CC=C1 IMACFCSSMIZSPP-UHFFFAOYSA-N 0.000 description 1
- 230000002035 prolonged effect Effects 0.000 description 1
- 239000003380 propellant Substances 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
- 239000000741 silica gel Substances 0.000 description 1
- 229910002027 silica gel Inorganic materials 0.000 description 1
- 239000000779 smoke Substances 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- 230000008685 targeting Effects 0.000 description 1
- 239000003491 tear gas Substances 0.000 description 1
Landscapes
- Toys (AREA)
Abstract
The application discloses an airborne anti-riot projectile launcher and an unmanned aerial vehicle, wherein the airborne anti-riot projectile launcher comprises: the device comprises an emitter main body, a main controller, an emitting tube structure and a servo firing mechanism; the main controller, the transmitting tube structure and the servo firing mechanism are all arranged on the transmitter main body, and the transmitting tube mechanism is electrically connected with the main controller; the servo firing mechanism includes: the driving motor is connected with the electric contact through the first coupler, the electric contact is aligned to the bottom of the to-be-emitted anti-riot bullet in the emission tube structure, and the technical problems of high cost and poor reliability of the existing anti-riot bullet emitter are solved.
Description
Technical Field
The application belongs to the technical field of anti-riot bullet transmitters, and particularly relates to an airborne anti-riot bullet transmitter and an unmanned aerial vehicle.
Background
The multi-rotor unmanned aerial vehicle is particularly suitable for throwing rubber bullets, smoke bullets, dyeing bullets, acousto-optic bullets, tear-gas bullets and other anti-riot bullets to realize the integration of reconnaissance due to the advantages of hovering, high speed, wide reconnaissance range and intellectualization.
The current unmanned aerial vehicle airborne anti-riot projectile launcher is still in the stage of just starting, adopts mechanical impact to fire to the ignition of anti-riot projectile, when waiting to send the projectile medicine to rotate to the barrel and launch the department, servo toggle mechanism pulls the trigger and obtains the spring energy storage, and the rethread releases this spring energy storage drive hammer (or firing pin) striking and is waited to launch the striking primer of ammunition and fire. Thus, the spring and the hammer (or the firing pin) are worn, so that the anti-riot bullet cannot be fired, and the reliability is poor; and the servo toggle mechanism is also required to be designed, so that the cost is high.
Disclosure of Invention
In view of the above, the application provides an onboard anti-riot projectile launcher and an unmanned aerial vehicle, which solve the technical problems of higher cost and poor reliability of the existing anti-riot projectile launcher.
The first aspect of the application provides an airborne anti-riot projectile launcher comprising: the device comprises an emitter main body, a main controller, an emitting tube structure and a servo firing mechanism;
the main controller, the transmitting tube structure and the servo firing mechanism are all arranged on the transmitter main body, and the servo firing mechanism is electrically connected with the main controller;
the servo firing mechanism includes: the electric power device comprises a driving motor, a first coupler and an electric contact with positive and negative motors, wherein the driving motor is connected with the electric contact through the first coupler, and the electric contact is aligned to the bottom of an anti-riot bomb to be emitted in the launching tube structure.
Preferably, the method comprises the steps of,
The launch tube mechanism includes: a guide plate, a barrel and a muzzle brake;
the guide plate is mounted on the emitter body;
one end of the barrel is sleeved in a through hole formed in the guide plate, and the other end of the barrel is sleeved with the muzzle brake.
Preferably, the method comprises the steps of,
The side wall of the muzzle brake is provided with a plurality of round through holes.
Preferably, the method comprises the steps of,
The runner mechanism of the airborne anti-riot projectile launcher comprises: the device comprises a connecting rod, a rear baffle spring plate, a rotating wheel sleeve, a rotating wheel and a connecting plate;
The rotating wheel is provided with a plurality of bullet nests for placing anti-riot bullets, and the rotating wheel is sleeved with the rotating wheel sleeve;
The connecting rod and the connecting plate are symmetrically arranged at the edges of the rotating wheel sleeve and are perpendicular to the end face of the rotating wheel sleeve;
The non-end part of the connecting rod is connected with the rotating wheel sleeve, one end of the connecting rod is connected with the rear baffle spring plate, and the other end of the connecting rod is connected with the guide plate;
The non-end of the connecting plate is connected with the rotating wheel sleeve, the first end of the connecting plate is detachably connected with the rear baffle spring plate, and the second end of the connecting plate is connected with the guide plate.
Preferably, the method comprises the steps of,
The connecting plate is detachably connected with the rear baffle spring plate through a locking assembly;
The latch assembly includes: the locking device comprises a locking hook, a locking hook seat and a clamping groove, wherein the locking hook seat is arranged on the rear baffle spring plate, the locking hook seat is rotatably provided with the locking hook, and the connecting plate is provided with the clamping groove for the locking hook to be embedded and inserted.
Preferably, the method comprises the steps of,
The servo rotating mechanism of the airborne anti-riot projectile launcher comprises: steering engine, second coupling, sleeve, flange bearing, axle cap, key, rotation axis, spring;
The steering engine is arranged on the rear baffle spring plate;
The flange bearing is arranged in the central hole of the rear baffle spring plate and is in interference fit with the central hole of the rear baffle spring plate;
the first end of the sleeve is connected with the output shaft of the steering engine through the second coupling, the second end of the sleeve is sleeved in the flange bearing, the second end of the sleeve is sleeved with the shaft cap, and the sleeve is in interference fit with the flange bearing;
The lower half part of the key is positioned in a groove formed in the shaft cap, and the upper half part of the key is positioned in a key groove in the central hole of the rotating wheel;
the spring with preset compression amount is sleeved on the rotating shaft, one end of the rotating shaft is connected with the shaft cap, and the other end of the rotating shaft is connected with the guide plate.
Preferably, the method comprises the steps of,
The mounting assembly of the airborne anti-riot projectile launcher comprises: hooks, buffer pads and padlocks;
The emitter main body is of a cuboid structure;
the buffer pad is installed on the emitter main body, and the hook and the padlock are respectively installed on two opposite side walls of the emitter main body.
Preferably, the method comprises the steps of,
The aiming system of the airborne anti-riot projectile launcher comprises: the device comprises a laser sighting device, an infrared imaging instrument and a camera;
the laser sighting device and the infrared imaging device are both arranged on the emitter main body;
the camera is installed on the guide plate.
A second aspect of the application provides a unmanned aerial vehicle comprising an on-board anti-riot projectile launcher as described in the first aspect.
From the above technical scheme, the application has the following advantages:
The application provides an airborne anti-riot projectile launcher, comprising: the device comprises an emitter main body, a main controller, an emitting tube structure and a servo firing mechanism; the main controller, the transmitting tube structure and the servo firing mechanism are all arranged on the transmitter main body, and the transmitting tube mechanism is electrically connected with the main controller; the servo firing mechanism includes: the driving motor is connected with the electric contact through the first coupler, and the electric contact is aligned to the bottom of the to-be-shot antiriot bomb in the launching tube structure.
According to the application, the driving motor of the servo firing mechanism is connected with the electric contact through the first coupler, the electric contact is aligned with the bottom of the to-be-emitted anti-riot bullet in the transmitting tube structure, and when the electric contact is ignited, the driving motor rotates to drive the first coupler to move so as to drive the electric contact to move, the electric contact contacts the to-be-emitted anti-riot bullet to realize ignition, the to-be-emitted anti-riot bullet is ignited by triggering ignition, the reliability of the transmission is improved, and the ignition is realized by using the servo toggle mechanism, so that the technical problems of higher cost and poor reliability of the existing anti-riot bullet transmitter are solved.
Drawings
Fig. 1 is a front view of an airborne anti-riot projectile launcher provided by an embodiment of the application;
FIG. 2 is a left side view of an airborne anti-riot projectile launcher according to an embodiment of the application;
FIG. 3 is a schematic view of the structure of the wheel and the rear fender according to the embodiment of the application;
FIG. 4 is a schematic view of the latch assembly according to the embodiment of the present application when opened;
FIG. 5 is an exploded view of a servo rotary mechanism according to an embodiment of the present application;
fig. 6 is a schematic structural diagram of an unmanned aerial vehicle according to an embodiment of the present application;
Wherein, the reference numerals are as follows:
P, a main controller; o, antiriot bullets; m, an emitter body; 1. a rotating wheel; 2. a guide plate; 3. a rotating wheel sleeve; 4. a rear spring blocking plate; 5. a connecting rod; 6. a connecting plate; 7. a driving motor; 8. a first coupling; 9. a barrel; 10. an electrical contact; 11. steering engine; 12. a second coupling; 13. a sleeve; 14. a flange bearing; 15. a shaft cap; 16. a key; 17. a rotation shaft; 18. a spring; 19. a locking hook; 20. a latch hook seat; 21. a clamping groove; 23. a muzzle brake; 24. a hook; 25. a padlock; 26. a laser sight; 27. an infrared imager; 28. a camera; 29. and a cushion pad.
Detailed Description
The embodiment of the application provides an airborne anti-riot projectile launcher and an unmanned aerial vehicle, which solve the technical problems of higher cost and poor reliability of the existing anti-riot projectile launcher.
The following description of the embodiments of the present application will be made in detail, but not necessarily all embodiments, with reference to the accompanying drawings. All other embodiments, which can be made by one of ordinary skill in the art without undue burden from the present disclosure, are within the scope of the embodiments of the present application.
In the description of the embodiments of the present application, it should be noted that the terms "center," "upper," "lower," "left," "right," "vertical," "horizontal," "inner," "outer," and the like indicate or are based on the orientation or positional relationship shown in the drawings, merely to facilitate description of the embodiments of the present application and to simplify the description, and do not indicate or imply that the devices 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 embodiments of the present application. Furthermore, the terms "", "second", "third" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance.
In describing embodiments of the present application, it should be noted that, unless explicitly stated and limited otherwise, the terms "mounted," "connected," and "connected" are to be construed broadly, and may be, for example, fixedly connected, interchangeably connected, integrally connected, mechanically connected, electrically connected, directly connected, indirectly connected through an intermediary, or in communication between two elements. The specific meaning of the above terms in embodiments of the present application will be understood in detail by those of ordinary skill in the art.
The present application provides an embodiment of an on-board riot projectile launcher, and particularly please refer to fig. 1 and 2.
The airborne anti-riot projectile launcher in this embodiment includes: the device comprises a transmitter main body M, a main controller P, a transmitting tube structure and a servo firing mechanism; the main controller P, the transmitting tube structure and the servo firing mechanism are all arranged on the transmitter main body M, and the transmitting tube structure is electrically connected with the main controller P; the servo firing mechanism includes: the driving motor 7, the first coupler 8 and the electrical contact 10 with positive and negative motors are connected, the driving motor 7 is connected with the electrical contact 10 through the first coupler 8, and the electrical contact 10 is aligned with the bottom of the to-be-shot anti-riot bomb O in the launching tube structure.
The driving motor 7 may be a linear motor, and the above design makes the driving motor 7, the coupling and the electrical contact 10 of the positive electrode form a mechanism that can move back and forth. When the linear motor rotates forward, the screw rod of the linear motor moves forward, the electric contact 10 is pushed to move forward through the coupler and contacts the anti-riot bullet O to be emitted, and otherwise, the electric contact 10 is pulled to retreat.
In this embodiment, the driving motor 7 of the servo firing mechanism is connected with the electrical contact 10 through the first coupling 8, and the electrical contact 10 is aligned to the bottom of the to-be-fired anti-riot bomb O in the launching tube structure, when in firing, the driving motor 7 rotates to drive the first coupling 8 to move, and then drives the electrical contact 10 to move, the electrical contact 10 contacts the to-be-fired anti-riot bomb O to realize firing, the to-be-fired anti-riot bomb O is fired through triggering the firing, the firing reliability is improved, and the same realization of firing is realized by using the servo toggle mechanism, so that the technical problems of higher firing cost and poor reliability in firing of the existing anti-riot bomb O are solved.
The foregoing is a first embodiment of an airborne anti-riot projectile launcher provided by an embodiment of the present application, and the following is a second embodiment of an airborne anti-riot projectile launcher provided by an embodiment of the present application.
The present application provides a second embodiment of an on-board riot projectile launcher, referring specifically to fig. 1 to 5, comprising: the device comprises a transmitter main body M, a main controller P, a transmitting tube structure and a servo firing mechanism; the main controller P, the transmitting tube structure and the servo firing mechanism are all arranged on the transmitter main body M, and the transmitting tube structure is electrically connected with the main controller P; the servo firing mechanism includes: the driving motor 7, the first coupler 8 and the electrical contact 10 with positive and negative motors are connected, the driving motor 7 is connected with the electrical contact 10 through the first coupler 8, and the electrical contact 10 is aligned with the bottom of the to-be-shot anti-riot bomb O in the launching tube structure.
It should be noted that, after the anti-riot bullet O is initially installed, the rear baffle plate 4 is attached to the rotating wheel 1 through the latch assembly. At this time, the backward stroke of the electrical contact 10 is short, the electrical contact 10 is contracted in the rear baffle spring plate 4 under the pressure of the spring 18, the contact does not contact with the bottom of the anti-riot spring O or the rear end face of the rotating wheel 1, and the contact does not hinder the rotating wheel 1. When the wheel 1 is turned to the correct position, the centre of the electric primer to be launched with the anti-riot bomb O is just aligned with the positive pole of the electric contact 10. The linear motor rotates positively, and the screw rod pushes the positive thimble to overcome the pressure of the spring 18 through the coupler so as to press the whole electrical contact 10 backwards on the low end face of the projectile. At this time, the positive electrode of the electrical contact 10 is conducted with the positive electrode in the middle of the electric primer of the anti-riot bomb to be shot, the negative electrode of the electrical contact 10 is conducted with the negative electrode at the outer end of the electric primer, and as long as the electrical contact 10 is electrified, the electric primer fires under the action of current to shot.
The launching tube mechanism in this embodiment includes: the guide plate 2, the barrel 9 and the muzzle brake guide plate 2 are arranged on the launcher main body M; one end of the barrel 9 is sleeved in a through hole formed in the guide plate 2, and the other end of the barrel is sleeved with a muzzle brake 23.
The muzzle brake 23 mounted on the barrel 9 reduces the impulse of the propellant gas to the recoil portion.
Further, a plurality of circular through holes are provided on the side wall of the muzzle brake 23. Designing a muzzle brake 23 of this type has the following advantages: 1) The appearance is beautiful; 2) The circular through hole is easy to process; 3) The round through hole is smaller, so that when the projectile runs rapidly in the round through hole, the projectile can not collide with the muzzle brake 23 even if nutation occurs, and the projectile can not be driven out even if the projectile is blocked from decelerating, but the nutation is reduced; 4) The many small holes form a number of transverse cross-sections through which the rear high pressure gas will impinge upon as a result of the pressure differential as the projectile tail passes, after which a side-to-rear refracted gas flow is formed, which impact will hinder the squat of barrel 9. Because of the plurality of holes, each hole can form a reverse squat impact, so the braking efficiency is effectively improved.
As shown in fig. 2 and 3, the wheel 1 mechanism of the on-board riot projectile launcher in the present embodiment includes: the connecting rod 5, the rear baffle spring plate 4, the rotating wheel sleeve 3, the rotating wheel 1 and the connecting plate 6; a plurality of bullet nests for placing anti-riot bullets O are arranged on the rotating wheel 1, and a rotating wheel sleeve 3 is sleeved on the rotating wheel 1; the connecting rod 5 and the connecting plate 6 are symmetrically arranged at the edge of the rotating wheel sleeve 3 and are perpendicular to the end face of the rotating wheel sleeve 3; the non-end part of the connecting rod 5 is connected with the rotating wheel sleeve 3, one end is connected with the rear baffle spring plate 4, and the other end is connected with the guide plate 2; the non-end of the connecting plate 6 is connected with the rotating wheel sleeve 3, the first end is detachably connected with the rear baffle spring plate 4, and the second end is connected with the guide plate 2.
In this embodiment, the rotating wheel 1 is sleeved with the rotating wheel sleeve 3 to prevent the rotating wheel 1 from moving radially and moving axially forward, and the rear elastic baffle 4 is arranged behind the rotating wheel 1 to press the anti-riot elastic O and the rotating wheel 1 to prevent the two from moving backward.
As shown in fig. 4, the connecting plate 6 in the present embodiment is detachably connected with the rear baffle plate 4 through a latch assembly; the latch assembly includes: the locking device comprises a locking hook 19, a locking hook seat 20 and a clamping groove 21, wherein the locking hook seat 20 is arranged on the rear baffle spring plate 4, the locking hook 19 is rotatably arranged on the locking hook seat 20, and the clamping groove 21 for embedding and inserting the locking hook 19 is formed in the connecting plate 6.
In order to enable stable rotation of the storm ball O during continuous firing, as shown in fig. 5, the servo rotation mechanism of the on-board storm ball launcher in the present embodiment includes: steering engine 11, second coupling 12, sleeve 13, flange bearing 14, shaft cap 15, key 16, rotation axis 17, spring 18; the steering engine 11 is arranged on the rear baffle spring plate 4; the flange bearing 14 is arranged in the central hole of the rear baffle spring plate 4 and is in interference fit with the central hole of the rear baffle spring plate 4; the first end of the sleeve 13 is connected with the output shaft of the steering engine 11 through a second coupling 12, the second end is sleeved in a flange bearing 14, a shaft cap 15 is sleeved in the second end, and the sleeve 13 is in interference fit with the flange bearing 14; the lower half part of the key 16 is positioned in a groove formed on the shaft cap 15, and the upper half part is positioned in a key 16 groove in the central hole of the rotating wheel 1; the rotating shaft 17 is sleeved with a spring 18 with a preset compression amount, one end of the rotating shaft 17 is connected with the shaft cap 15, and the other end of the rotating shaft is connected with the guide plate 2.
It will be appreciated that the socket 13 may be selected as desired, and is not particularly limited herein, and in this embodiment, a socket head cap is selected.
Meanwhile, as the front end of the rotating shaft 17 is inserted into the shaft cap 15, the rear end of the rotating shaft is fixed on the guide plate 2, and the spring 18 is sleeved on the rotating shaft, when the shaft cap 15 rotates, the shaft cap 15 can ensure that a part of the front end of the shaft cap 15 protrudes out of the front end surface of the rotating wheel 1 under the forward pre-pressure of the spring 18 when the shaft cap 15 does not have backward external pressure, and when the rotating wheel 1 is buckled with ammunition, the sleeve 13 in the rear baffle spring plate 4 can be in collision fit with the protruding shaft cap 15 when the rear baffle spring plate 4 is buckled with ammunition. If the two are positioned exactly, the front end and the rear end of the shaft cap 15 are inserted into the sleeve 13, and if the positions deviate, the sleeve 13 can apply external pressure to the shaft cap 15, and the external pressure can lead the shaft cap 15 to actuate backwards and compress the spring 18 (the rotating wheel 1 is not moved in the process and can be attached to the rear baffle plate 4). At this time, only by slightly rotating the rotating wheel 1, the rotating wheel 1 drives the shaft cap 15 to rotate through the key 16, so that when the shaft cap 15 rotates to be at the same angle as the sleeve 13, the shaft cap 15 is clamped into the sleeve 13 under the forward pressure of the spring 18. This forms a rotational path formed by a steering engine 11, coupling, sleeve 13, shaft cap 15 and rotational shaft 17. The channel can enable the rotation of the output shaft of the steering engine 11 to drive the rotating wheel 1 to synchronously rotate, so that continuous emission of the riot grenade is realized. Wherein smooth rotation and low friction are ensured by means of flange bearings 14.
In order to make the connection stable when emitter and unmanned aerial vehicle connect, the mounting subassembly of on-board anti-riot bullet transmitter includes in this embodiment: hook 24, cushion 29 and hook 25; the emitter main body M is of a cuboid structure; the cushion is mounted on the emitter body M, and hooks 24 and 25 are respectively mounted on two opposite sidewalls of the emitter body M.
It should be noted that the cushion pad 29 may play a role of shock absorption, and it is understood that the material of the cushion pad 29 may be foam silica gel or the like, which is not particularly limited herein.
In order to make the target more accurate and widely used in the process of launching the riot bomb O, the aiming system of the airborne riot bomb launcher in the present embodiment includes: a laser sight 26, an infrared imager 27 and a camera 28; the laser sight 26 and the infrared imager 27 are both mounted on the emitter body M; the camera 28 is mounted on the guide plate 2. It will be appreciated that the camera 28 is mainly used for daytime camera reconnaissance and shooting effect viewing, and the laser sight 26 is mainly used for aiming (when aiming directly) at a shooting target; the infrared imager 27 is primarily used for night target reconnaissance and post-shooting effect viewing.
When the airborne anti-riot projectile launcher in the embodiment is used, firstly, the rear baffle spring plate 4 is opened to install the anti-riot projectile O in the rotating wheel 1, after loading is completed, the rear baffle spring plate 4 is locked with the connecting plate 6 by means of the locking assembly, then the direction and the angle of the unmanned aerial vehicle are adjusted by means of target information detected by the camera 28 or the laser sighting device 26, the electric contact 10 is electrified, so that the electric primer of the anti-riot projectile O fires, the launching action of the first anti-riot projectile O is completed, after the first anti-riot projectile O is launched, the electric contact 10 is pulled by means of the linear motor, and then the servo rotating mechanism is controlled to drive the rotating wheel 1 to rotate by a certain angle, so that the next anti-riot projectile O in the projectile nest of the rotating wheel 1 is aligned with the projectile chamber of the transmitting tube, and then the contact is pressed by the linear motor, and the launching of the next anti-riot projectile O can be carried out.
Compared with the prior art, the airborne anti-riot O transmitter provided by the embodiment of the application has the following advantages:
1) The hooks 24 and 25 are adopted to be fastened and mounted with the unmanned aerial vehicle, so that the structure is stable, the stress is greatly reduced, and the service life of extra-high parts is prolonged.
2) The barrel 9 is far away from the mass center, the structure is compact, and the stress of the mounting plate and the impact of shooting squatting on the unmanned aerial vehicle are reduced.
3) The locking mechanism is adopted to realize the rapid and convenient locking or unlocking.
4) The scheme of utilizing the linear motor, the electric contact 10 and the electric primer replaces the mechanical triggering mechanism of the hand-held anti-riot bomb O emitter, simplifies the structure, lightens the weight and is convenient for the aircraft to realize ignition and emission.
5) A unique servo rotation mechanism is used to achieve accurate rotation and servo movement of the rotor 1.
6) The muzzle brake 23 is additionally arranged, so that recoil impulse during firing is reduced;
7) The infrared imager 27 is added to facilitate the use of a particular environment, particularly for night-time targeting.
In this embodiment, the driving motor 7 of the servo firing mechanism is connected with the electrical contact 10 through the first coupling 8, and the electrical contact 10 is aligned to the bottom of the to-be-fired anti-riot bomb O in the launching tube structure, when in firing, the driving motor 7 rotates to drive the first coupling 8 to move, and then drives the electrical contact 10 to move, the electrical contact 10 contacts the to-be-fired anti-riot bomb O to realize firing, the to-be-fired anti-riot bomb O is fired through triggering the firing, the firing reliability is improved, and the same realization of firing is realized by using the servo toggle mechanism, so that the technical problems of higher firing cost and poor reliability in firing of the existing anti-riot bomb O are solved.
The foregoing is a second embodiment of an airborne anti-riot projectile launcher provided by the embodiment of the application, and the following is an embodiment of an unmanned aerial vehicle provided by the embodiment of the application.
As shown in fig. 6, the unmanned aerial vehicle in this embodiment includes the on-board riot projectile launcher of any one of the embodiments described above. It can be appreciated that the unmanned aerial vehicle in this embodiment mounts the anti-riot projectile launcher on the unmanned aerial vehicle through the mounting assembly of the anti-riot projectile launcher in the foregoing embodiment.
In this embodiment, the driving motor 7 of the servo firing mechanism is connected with the electrical contact 10 through the first coupling 8, and the electrical contact 10 is aligned to the bottom of the to-be-fired anti-riot bomb O in the launching tube structure, when in firing, the driving motor 7 rotates to drive the first coupling 8 to move, and then drives the electrical contact 10 to move, the electrical contact 10 contacts the to-be-fired anti-riot bomb O to realize firing, the to-be-fired anti-riot bomb O is fired through triggering the firing, the firing reliability is improved, and the same realization of firing is realized by using the servo toggle mechanism, so that the technical problems of higher firing cost and poor reliability in firing of the existing anti-riot bomb O are solved.
The above embodiments are only for illustrating the technical solution of the present application, and not for limiting the same; although the application has been described in detail with reference to the foregoing embodiments, it will be understood by those of ordinary skill in the art that: the technical scheme described in the foregoing embodiments can be modified or some technical features thereof can be replaced by equivalents; such modifications and substitutions do not depart from the spirit and scope of the technical solutions of the embodiments of the present application.
Claims (6)
1. An airborne anti-riot projectile launcher comprising: the device comprises an emitter main body, a main controller, an emitting tube structure and a servo firing mechanism;
the main controller, the transmitting tube structure and the servo firing mechanism are all arranged on the transmitter main body, and the servo firing mechanism is electrically connected with the main controller;
The servo firing mechanism includes: the driving motor is connected with the electric contact through the first coupler, and the electric contact is aligned to the bottom of the to-be-shot antiriot bomb in the launching tube structure;
the launch tube mechanism includes: a guide plate, a barrel and a muzzle brake;
the guide plate is mounted on the emitter body;
One end of the barrel is sleeved in a through hole formed in the guide plate, and the other end of the barrel is sleeved with the muzzle brake;
a plurality of circular through holes are formed in the side wall of the muzzle brake;
The runner mechanism of the airborne anti-riot projectile launcher comprises: the device comprises a connecting rod, a rear baffle spring plate, a rotating wheel sleeve, a rotating wheel and a connecting plate;
The rotating wheel is provided with a plurality of bullet nests for placing anti-riot bullets, and the rotating wheel is sleeved with the rotating wheel sleeve;
The connecting rod and the connecting plate are symmetrically arranged at the edges of the rotating wheel sleeve and are perpendicular to the end face of the rotating wheel sleeve;
The non-end part of the connecting rod is connected with the rotating wheel sleeve, one end of the connecting rod is connected with the rear baffle spring plate, and the other end of the connecting rod is connected with the guide plate;
The non-end of the connecting plate is connected with the rotating wheel sleeve, the first end of the connecting plate is detachably connected with the rear baffle spring plate, and the second end of the connecting plate is connected with the guide plate.
2. The on-board riot projectile launcher of claim 1, wherein the attachment plate is detachably connected to the backstop spring plate by a latch assembly;
The latch assembly includes: the locking device comprises a locking hook, a locking hook seat and a clamping groove, wherein the locking hook seat is arranged on the rear baffle spring plate, the locking hook seat is rotatably provided with the locking hook, and the connecting plate is provided with the clamping groove for the locking hook to be embedded and inserted.
3. The on-board riot projectile launcher according to claim 1, wherein the servo rotation mechanism of the on-board riot projectile launcher comprises: steering engine, second coupling, sleeve, flange bearing, axle cap, key, rotation axis, spring;
The steering engine is arranged on the rear baffle spring plate;
The flange bearing is arranged in the central hole of the rear baffle spring plate and is in interference fit with the central hole of the rear baffle spring plate;
the first end of the sleeve is connected with the output shaft of the steering engine through the second coupling, the second end of the sleeve is sleeved in the flange bearing, the second end of the sleeve is sleeved with the shaft cap, and the sleeve is in interference fit with the flange bearing;
The lower half part of the key is positioned in a groove formed in the shaft cap, and the upper half part of the key is positioned in a key groove in the central hole of the rotating wheel;
the spring with preset compression amount is sleeved on the rotating shaft, one end of the rotating shaft is connected with the shaft cap, and the other end of the rotating shaft is connected with the guide plate.
4. The on-board riot projectile launcher according to claim 1, wherein the mounting assembly of the on-board riot projectile launcher comprises: hooks, buffer pads and padlocks;
The emitter main body is of a cuboid structure;
the buffer pad is installed on the emitter main body, and the hook and the padlock are respectively installed on two opposite side walls of the emitter main body.
5. The on-board riot projectile launcher according to claim 1, wherein the sighting system of the on-board riot projectile launcher comprises: the device comprises a laser sighting device, an infrared imaging instrument and a camera;
the laser sighting device and the infrared imaging device are both arranged on the emitter main body;
the camera is installed on the guide plate.
6. A drone comprising an on-board riot projectile launcher as claimed in any one of claims 1 to 5.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910329433.4A CN109911209B (en) | 2019-04-23 | 2019-04-23 | Airborne anti-riot projectile emitter and unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910329433.4A CN109911209B (en) | 2019-04-23 | 2019-04-23 | Airborne anti-riot projectile emitter and unmanned aerial vehicle |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN109911209A CN109911209A (en) | 2019-06-21 |
| CN109911209B true CN109911209B (en) | 2024-05-31 |
Family
ID=66978283
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910329433.4A Active CN109911209B (en) | 2019-04-23 | 2019-04-23 | Airborne anti-riot projectile emitter and unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109911209B (en) |
Families Citing this family (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110395392B (en) * | 2019-07-29 | 2021-02-19 | 北京无线电测量研究所 | Lower-throwing type sonde ejection cylinder, ejection device and automatic throwing equipment |
| CN111141174A (en) * | 2020-01-07 | 2020-05-12 | 吉林省翼启飞科技有限公司 | Eight-hole smoke bomb launching device for unmanned aerial vehicle |
| CN111824421B (en) * | 2020-06-15 | 2022-12-13 | 成都大学 | A anti-riot bullet shooting mechanism and bullet shooting device for unmanned aerial vehicle |
| CN111811338B (en) * | 2020-08-13 | 2023-08-11 | 吉林省翼启飞科技有限公司 | Mechanical excitation type smoke bomb device and remote emission method thereof |
| CN112229267B (en) * | 2020-11-03 | 2022-07-26 | 长沙金信诺防务技术有限公司 | Automatic grenade launcher |
| CN113184191A (en) * | 2021-03-31 | 2021-07-30 | 成都飞机工业（集团）有限责任公司 | Mandrel operation mechanism for high-altitude release of meteorological sonde |
| CN113086205B (en) * | 2021-05-13 | 2022-07-22 | 山东理工大学 | Rotating wheel type seeding unmanned aerial vehicle |
| CN113086204B (en) * | 2021-05-13 | 2022-07-29 | 山东理工大学 | Projection type mangrove hypocotyl sowing unmanned aerial vehicle |
| CN113485415B (en) * | 2021-06-28 | 2024-06-18 | 中交遥感载荷(江苏)科技有限公司 | Rescue and relief method based on unmanned aerial vehicle system and unmanned aerial vehicle system thereof |
| CN113788130B (en) * | 2021-08-17 | 2022-09-06 | 河北汉光重工有限责任公司 | Underwater vehicle launching device of imitation revolver |
| CN114379782B (en) * | 2021-12-30 | 2023-06-06 | 哈瓦国际航空技术（深圳）有限公司 | Material throwing device and unmanned aerial vehicle |
| CN114877759B (en) * | 2022-03-31 | 2024-02-13 | 无锡海纳光电子信息技术有限公司 | Gunpowder power non-standard bullet detection device |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6422120B1 (en) * | 1999-08-03 | 2002-07-23 | General Dynamics Armament Systems, Inc. | Firing mechanism for a rotary machine gun |
| CN1372123A (en) * | 2002-04-12 | 2002-10-02 | 张宝林 | Military current firing type ultrahigh speed shooting gun and cannon |
| RU2373477C1 (en) * | 2008-06-10 | 2009-11-20 | Открытое акционерное общество "Тулаточмаш" | Manual hand grenade launcher complex |
| CN203394472U (en) * | 2013-08-23 | 2014-01-15 | 中国石油天然气集团公司 | Time-sharing perforation selective shooting device |
| CN104748619A (en) * | 2015-04-23 | 2015-07-01 | 成都恒安警用装备制造有限公司 | Multi-running-fire anti-riot gun |
| CN208707206U (en) * | 2018-08-28 | 2019-04-05 | 湖北电鹰科技有限公司 | A kind of electric stringing auxiliary catapult-launching gear based on unmanned aerial vehicle platform |
| CN209889117U (en) * | 2019-04-23 | 2020-01-03 | 广州鼎飞航空科技有限公司 | Airborne anti-riot bullet emitter and unmanned aerial vehicle |
-
2019
- 2019-04-23 CN CN201910329433.4A patent/CN109911209B/en active Active
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6422120B1 (en) * | 1999-08-03 | 2002-07-23 | General Dynamics Armament Systems, Inc. | Firing mechanism for a rotary machine gun |
| CN1372123A (en) * | 2002-04-12 | 2002-10-02 | 张宝林 | Military current firing type ultrahigh speed shooting gun and cannon |
| RU2373477C1 (en) * | 2008-06-10 | 2009-11-20 | Открытое акционерное общество "Тулаточмаш" | Manual hand grenade launcher complex |
| CN203394472U (en) * | 2013-08-23 | 2014-01-15 | 中国石油天然气集团公司 | Time-sharing perforation selective shooting device |
| CN104748619A (en) * | 2015-04-23 | 2015-07-01 | 成都恒安警用装备制造有限公司 | Multi-running-fire anti-riot gun |
| CN208707206U (en) * | 2018-08-28 | 2019-04-05 | 湖北电鹰科技有限公司 | A kind of electric stringing auxiliary catapult-launching gear based on unmanned aerial vehicle platform |
| CN209889117U (en) * | 2019-04-23 | 2020-01-03 | 广州鼎飞航空科技有限公司 | Airborne anti-riot bullet emitter and unmanned aerial vehicle |
Also Published As
| Publication number | Publication date |
|---|---|
| CN109911209A (en) | 2019-06-21 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN109911209B (en) | Airborne anti-riot projectile emitter and unmanned aerial vehicle | |
| CN106924962B (en) | Shooting game device | |
| US7631601B2 (en) | Surveillance projectile | |
| CN113218251B (en) | Air flying net capturing bomb and working method thereof | |
| US20060196383A1 (en) | Target assignment projectile | |
| CN209889117U (en) | Airborne anti-riot bullet emitter and unmanned aerial vehicle | |
| CN108327897A (en) | Equip with arms unmanned helicopter | |
| CN208216982U (en) | Equip with arms unmanned helicopter | |
| CN210400162U (en) | Electromagnetic weapon for gunship helicopter | |
| CN111372665B (en) | Transmitting device, transmitting assembly and remote control car | |
| KR101343393B1 (en) | Shooting training module combined with weapon and Shooting training system using the same | |
| US20220381533A1 (en) | Bullet rotatably shooting apparatus in a toy gun | |
| CN215337998U (en) | Small-caliber rocket bomb | |
| CN112129179B (en) | Laser beam driving guided missile emitted by 40mm rocket tube | |
| CN211863818U (en) | Silencer formula radium war box | |
| CN210212783U (en) | Nonmetal bullet continuous launching device of unmanned aerial vehicle airborne platform | |
| CN210952527U (en) | Wireless instruction guidance rocket projectile and controlled infrared beacon for 40mm rocket launcher | |
| CN209752182U (en) | Transmitting device, transmitting assembly and remote control car | |
| CN111981917B (en) | Wireless instruction guided rocket projectile for 40mm rocket tube | |
| CN209820260U (en) | Cluster type automatic signal bullet emitter based on electromagnetic percussion | |
| CN220959818U (en) | Movable combat platform carrying clustered rocket projectile | |
| CN220959817U (en) | Rocket projectile bundling and transmitting device | |
| CN217585507U (en) | Emitter and small-size ground robot | |
| CN217929978U (en) | Launching mechanism of full-automatic fire extinguishing rocket projectile launching device | |
| CN108759555A (en) | A kind of true rifle of simulation |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant |