CN114061373A - Unmanned aerial vehicle carries ammunition launching platform - Google Patents
Unmanned aerial vehicle carries ammunition launching platform Download PDFInfo
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- CN114061373A CN114061373A CN202111563854.7A CN202111563854A CN114061373A CN 114061373 A CN114061373 A CN 114061373A CN 202111563854 A CN202111563854 A CN 202111563854A CN 114061373 A CN114061373 A CN 114061373A
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- aerial vehicle
- unmanned aerial
- ammunition
- unmanned
- launching
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- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims description 18
- 230000003287 optical effect Effects 0.000 claims description 15
- 238000010304 firing Methods 0.000 claims description 10
- 229910052742 iron Inorganic materials 0.000 claims description 9
- 238000005474 detonation Methods 0.000 abstract description 3
- 239000000779 smoke Substances 0.000 abstract description 2
- 230000001276 controlling effect Effects 0.000 description 7
- 230000005540 biological transmission Effects 0.000 description 6
- 238000010586 diagram Methods 0.000 description 4
- 230000009286 beneficial effect Effects 0.000 description 3
- 238000000034 method Methods 0.000 description 3
- 238000005516 engineering process Methods 0.000 description 2
- 230000001105 regulatory effect Effects 0.000 description 2
- 230000008054 signal transmission Effects 0.000 description 2
- 206010015856 Extrasystoles Diseases 0.000 description 1
- 238000010521 absorption reaction Methods 0.000 description 1
- 238000012790 confirmation Methods 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
- 238000001179 sorption measurement Methods 0.000 description 1
- 239000003491 tear gas Substances 0.000 description 1
Images
Classifications
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D1/00—Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight
- B64D1/02—Dropping, ejecting, or releasing articles
- B64D1/04—Dropping, ejecting, or releasing articles the articles being explosive, e.g. bombs
- B64D1/06—Bomb releasing; Bombs doors
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Abstract
The invention provides an unmanned airborne ammunition launching platform. The unmanned airborne ammunition launching platform comprises: an unmanned aerial vehicle; the cloud platform, the cloud platform is fixed in unmanned aerial vehicle's bottom, the cloud platform is including rotating movable support, last driving motor and the drive control module of being provided with of rotating movable support to one side fixedly connected with of rotating movable support is used for the cooperation drive control module is right the rotating movable support turned angle carries out the angle sensor who controls. The unmanned aerial vehicle-mounted ammunition launching platform provided by the invention is provided with an ammunition launcher which can launch tear shells, detonation shells, smoke shells and the like, the ammunition launcher is installed on the unmanned aerial vehicle, the unmanned aerial vehicle is taken as a flight platform, the unmanned aerial vehicle enters a battlefield through ground remote control, the aiming assembly is used for searching and locking and tracking the target, and the triple launching cylinders are used for respectively striking the target, so that the target can be struck quickly and accurately, and the designated task can be finished quickly and accurately.
Description
Technical Field
The invention relates to the technical field of fire control of unmanned aerial vehicles, in particular to an unmanned aerial vehicle-mounted ammunition launching platform.
Background
An unmanned aircraft, abbreviated as "drone", and abbreviated in english as "UAV", is an unmanned aircraft that is operated by a radio remote control device and a self-contained program control device, or is operated autonomously, either completely or intermittently, by an onboard computer.
In prior art, although unmanned aerial vehicle flight application technique, ammunition firing technology are mature, nevertheless make up unmanned aerial vehicle and ammunition firing technology, strike the operation of system very complicated, inconvenient quick locking and accomplish the strike to the target, inconvenient completion appointed striking task rapidly.
Therefore, there is a need to provide an unmanned airborne ammunition launching platform that solves the above technical problems.
Disclosure of Invention
The invention provides an unmanned airborne ammunition launching platform, which solves the problem that the unmanned airborne ammunition launching platform is inconvenient to rapidly complete a specified striking task.
In order to solve the technical problem, the invention provides an unmanned airborne ammunition launching platform which comprises: an unmanned aerial vehicle;
the cloud platform is fixed at the bottom of the unmanned aerial vehicle and comprises a rotating support, a driving motor and a driving control module are arranged on the rotating support, and an angle sensor used for being matched with the driving control module to control the rotating angle of the rotating support is fixedly connected to one side of the rotating support;
the ammunition launcher is fixedly arranged on the cradle head and comprises a triple launching barrel, and a locking device for aiming and locking and a trigger generator for controlling the triple launching barrel are arranged on the triple launching barrel;
the aiming assembly is fixedly installed on the holder, and comprises a camera and optical equipment used for controlling the camera.
Preferably, the triple launching tube is provided with a mounting bracket for mounting the triple launching tube on the holder.
Preferably, the rotating support is fixed to the bottom of the unmanned aerial vehicle, the output end of the driving motor is fixedly connected with the mounting support and is used for driving the mounting support to rotate.
Preferably, the camera is fixed on the mounting bracket and is positioned below the triple launching tube.
Preferably, unmanned aerial vehicle's inside is provided with information transmission receiving element, information transmission receiving element includes airborne receiver and video transmitter, airborne receiver with video transmitter electric connection.
Preferably, host system is used for right unmanned aerial vehicle's control, and host system with airborne receiver with the equal electric connection of video transmitter.
Preferably, the main control module is electrically connected to the driving control module, and the video transmitter is electrically connected to the optical device.
Preferably, the unmanned aerial vehicle further comprises a ground handheld transceiver for controlling the unmanned aerial vehicle matched with the main control module, the ground handheld transceiver comprises a shell, and a control panel with a plurality of control switches is arranged on the outer surface of the shell;
the telescopic display screen comprises a telescopic assembly, wherein the telescopic assembly is arranged in the shell and comprises a telescopic groove, the inner part of the telescopic groove is movably connected with a telescopic display screen, a wire is arranged at the bottom of the telescopic display screen, wear-resistant rubber pads are fixedly connected to the two sides of the telescopic display screen, and one side of the telescopic display screen is fixedly connected with a handle which is used for pulling the telescopic display screen out of the telescopic groove.
Preferably, the flexible groove set up in unmanned aerial vehicle's inside, the one end of wire is passed unmanned aerial vehicle and with control panel fixed connection.
Preferably, limiting grooves are formed in two sides of the inner wall of the telescopic groove, limiting iron blocks are fixedly connected to two sides of the telescopic display screen, the limiting grooves are in sliding connection with the limiting iron blocks, and adsorption magnetic blocks are fixedly connected to two sides of the inner wall of the limiting groove.
Compared with the related art, the unmanned airborne ammunition launching platform provided by the invention has the following beneficial effects:
the invention provides an unmanned aerial vehicle-mounted ammunition launching platform, wherein an ammunition launcher can launch tear shells, detonation shells, smoke shells and the like, the ammunition launcher is installed on an unmanned aerial vehicle, the unmanned aerial vehicle is taken as a flight platform and enters a battlefield through ground remote control, a target is prevented from being searched, locked and tracked through a sighting assembly, and then the target is struck through a triple launching cylinder respectively, so that the target can be struck quickly and accurately, designated tasks can be quickly and accurately completed, and quick transmission of signals and quick return of target information images are realized through a vehicle-mounted receiver and a video transmitter which are installed inside the unmanned aerial vehicle, so that the real-time performance and the high efficiency of unmanned aerial vehicle striking are ensured.
Drawings
FIG. 1 is a schematic structural view of a first embodiment of an unmanned airborne ammunition firing platform provided by the present invention;
fig. 2 is a schematic structural diagram of a side view portion of the drone shown in fig. 1;
fig. 3 is a schematic structural view of an internal part of the drone shown in fig. 1;
FIG. 4 is a system diagram of a controlled launch ensemble of an unmanned on-board ammunition launch platform provided by the present invention;
FIG. 5 is a schematic structural view of a second embodiment of an unmanned airborne ammunition firing platform provided by the present invention;
fig. 6 is a schematic structural view of an inner portion of the housing shown in fig. 5.
Reference numbers in the figures:
1. an unmanned aerial vehicle;
2. the device comprises a holder 21, a rotating bracket 22, a driving motor 23, a driving control module 24 and an angle sensor;
3. ammunition launcher, 31, triple launch canister, 32, locking device, 33, and trigger generator;
4. aiming assembly, 41, camera, 42, optical device;
5. an optical device;
6. receiving component, 61, onboard receiver, 62, video transmitter;
7. a main control module;
8. a ground handheld transceiver 81, a shell 82 and a panel;
9. the telescopic display screen comprises a telescopic assembly 91, a telescopic groove 92, a telescopic display screen 93, a telescopic display screen 94, a wear-resistant rubber pad 95 and a handle;
10. spacing recess, 11, spacing iron plate, 12, absorption magnetic path.
Detailed Description
The invention is further described with reference to the following figures and embodiments.
First embodiment
Referring to fig. 1, 2, 3 and 4, fig. 1 is a schematic structural view of a first embodiment of an unmanned airborne ammunition launching platform provided by the present invention; fig. 2 is a schematic structural diagram of a side view portion of the drone shown in fig. 1; fig. 3 is a schematic structural view of an internal part of the drone shown in fig. 1; fig. 4 is a system diagram of the control launching integrity of the unmanned airborne ammunition launching platform provided by the invention. Unmanned airborne ammunition launching platform includes: an unmanned aerial vehicle 1;
the cloud platform 2 is fixed at the bottom of the unmanned aerial vehicle 1, the cloud platform 2 comprises a rotating support 21, a driving motor 22 and a driving control module 23 are arranged on the rotating support 21, and an angle sensor 24 used for being matched with the driving control module 23 to control the rotating angle of the rotating support 21 is fixedly connected to one side of the rotating support 21;
the ammunition launcher 3 is fixedly arranged on the cradle head 2, the ammunition launcher 3 comprises a triple launching cylinder 31, and a locking device 32 for aiming and locking and a striking generator 33 for controlling the triple launching cylinder 31 are arranged on the triple launching cylinder 31;
aiming assembly 4, aiming assembly 4 fixed mounting in on cloud platform 2, aiming assembly 4 includes camera 41 and is used for carrying out the optical equipment 42 controlled to camera 41.
There is internal power supply on unmanned aerial vehicle 1, for unmanned aerial vehicle 1 with set up all power consumption subassemblies on unmanned aerial vehicle 1 and supply power, the ballistic axis of ammunition transmitter 3 is unanimous with the coaxial and direction of optical axis who aims subassembly 4, and is the same with 1 flight direction of unmanned aerial vehicle.
As shown in fig. 4, the ammunition launched by the triple-launch canister 31 is controlled by the overall system for controlling launching shown in fig. 4, and the overall system is divided into two parts, namely a ground control center and an air airborne device; the whole firing process of the ammunition is as follows:
1. when in use, the manipulator transmits signals through the ground remote control station to control and operate the aerial equipment; after receiving the signal, the receiver firstly judges whether the signal is true or false, and inputs the signal into a control center after confirmation; and after the control center classifies the instructions, the fire control system and the cradle head are respectively controlled.
2. Starting to execute a task, controlling the unmanned aerial vehicle 1 to lift off by a flying hand, carrying out target search by an equipment operating hand through an operating holder 2, setting an X axis as a horizontal corner component and a Y axis as a vertical corner component by a system, and setting the offset of delta X and delta Y as 0 when a forward heading mechanical axis of the unmanned aerial vehicle is coincident with an optical axis of an optical system; the operator changes the delta X through the rocker, horizontal search can be carried out, distance search can be carried out by changing the delta Y, in application, the delta Y is firstly regulated on a value, the delta X is regulated, and area search is carried out by matching with unmanned flight speed 1; when the flight speed and the scanning speed of the unmanned aerial vehicle are suitable, the delta Y can be properly adjusted to ensure that no leak exists in a search area. The optical axis (view field) of an optical system carried by the tripod head rotates synchronously with the tripod head, the adjustment range of delta X is +/-60 degrees, and the adjustment range of delta Y is 0-90 degrees. The image generated by the optical system is transmitted back to the ground station through the system, and the operator can find and judge the target through the information comparison of the image.
3. When the target is confirmed, locking the target immediately and recording a tracking program; the search tracking mode is divided into an automatic mode and a manual mode, and under the manual tracking mode, the flight state and the target locking of the unmanned aerial vehicle are matched well, and a flight hand and an equipment manipulator are required to be closely matched.
4. In a manual mode, after a target is locked, a flying hand operates the unmanned aerial vehicle 1 to fly to the upper part of the target, and an equipment operating hand adjusts the angle delta Y to tend to 90 degrees and the angle delta X to tend to 0 degree; when Δ Y reaches 90 ° and Δ X reaches 0 °, the target remains in the lock frame and can enter a launch ready state.
5. The triple launching canister 31 on the unmanned aerial vehicle 1 carries three ammunitions, namely a first load, a second load and a third load, and the number of the ammunitions to be thrown can be selected according to instructions or field conditions.
6. The unmanned aerial vehicle flight hand stabilizes unmanned aerial vehicle 1 flight state, equips the operative hand and utilizes handheld remote controller transmission striking instruction, starts load one respectively, load two, load three to attack.
7. After the attack task is completed, the flyer quickly flies the unmanned aerial vehicle 1 away from the site and returns to the base.
8. And (4) filling ammunition, replacing the internal battery of the unmanned aerial vehicle and preparing for next striking.
The triple transmitting tube 31 is provided with a mounting bracket 5 for mounting the triple transmitting tube 31 on the tripod head 2.
The triple barrel 31 carries three rounds of ammunition which can be fired separately as needed.
The runing rest 21 is fixed in unmanned aerial vehicle 1's bottom, driving motor 22's output with mounting bracket 5 fixed connection is used for driving mounting bracket 5 rotates.
The driving motor 22 can drive the mounting bracket 5 to rotate, so that the whole pan/tilt head 2 rotates.
The camera 41 is fixed on the mounting bracket 5 and is positioned below the triple emitter barrel 31.
The inside of unmanned aerial vehicle 1 is provided with information transmission receiving assembly 6, information transmission receiving assembly 6 includes airborne receiver 61 and video transmitter 62, airborne receiver 61 with video transmitter 62 electric connection.
The main control module 7, the main control module 7 is used for right the control of unmanned aerial vehicle to main control module 7 with airborne receiver 61 with video transmitter 62 all electric connection.
The master control module 7 can realize the unified signal transmission of signals and ground control equipment of various signals between the onboard receiver 61 and the video transmitter 62.
The main control module 7 is electrically connected to the driving control module 23, and the video transmitter 62 is electrically connected to the optical device 42.
The image of camera 41 may be transmitted to a surface operator via video transmitter 62.
The working principle of the unmanned airborne ammunition launching platform provided by the invention is as follows:
the unmanned aerial vehicle 1 drives the cradle head 2 and the ammunition emitter 3 to fly, the shooting target is searched by the camera 41, and the shooting target in the camera 41 can be analyzed and tracked by the optical equipment 42, so that the shooting target can be automatically tracked by the camera 41, and an image is emitted to an operator on the ground through the video emitter;
after the ground operator confirms the target to be struck, the locking device 32 locks the target to be struck by the triple launching tube 31, and then the trigger generator 33 controls the triple launching tube 31 to launch the ammunition to strike the target accurately.
Compared with the related art, the unmanned airborne ammunition launching platform provided by the invention has the following beneficial effects:
ammunition transmitter 3 can launch the standard tear-gas shells, the detonation bomb, smog bomb etc, install ammunition transmitter 3 on unmanned aerial vehicle 1, use unmanned aerial vehicle 1 to flight platform, get into the battlefield through ground remote control, rethread aims subassembly 4 and searches for and lock the pursuit avoiding the target, rethread trigeminy launching tube 31 strikes the target respectively, in order to make things convenient for the quick accurate striking to the target, can be quick accurate accomplish the assigned task, and pass back fast through installing quick transmission and the target information image of the airborne receiver 61 and the video transmitter 62 realization signal in unmanned aerial vehicle 1 inside, guarantee real-time and the high efficiency that unmanned aerial vehicle struck.
Second embodiment
Referring to fig. 4 and 5 in combination, a second embodiment of the present application provides an unmanned airborne based ammunition launching platform based on a first embodiment of the present application. The second embodiment is only the preferred mode of the first embodiment, and the implementation of the second embodiment does not affect the implementation of the first embodiment alone.
Specifically, the difference between the unmanned airborne ammunition launching platform provided by the second embodiment of the application is that the unmanned airborne ammunition launching platform further comprises
The ground handheld transceiver 8 is used for controlling the unmanned aerial vehicle 1 matched with the main control module 7, the ground handheld transceiver 8 comprises a shell 81, and a control panel 82 with a plurality of control switches is arranged on the outer surface of the shell 81;
the transceiver 8 is held through the ground and the flight of the whole unmanned aerial vehicle is controlled conveniently through the main control module 7.
The telescopic display screen 92 can be pulled out from the inside of the shell 81 to be watched by manually pulling the handle 95 to the outside of the shell 81, the wear-resistant rubber pad 94 is used for facilitating the sliding of the telescopic display screen 92, and the telescopic display screen 92 is made to conveniently slide to any position through friction force.
Pressing the key on the control panel 82 can remotely generate a corresponding instruction to the unmanned aerial vehicle 1, and display the received image information on the display screen 92.
Spacing recess 10 has been seted up to the both sides of flexible groove 91 inner wall, the spacing iron plate 11 of both sides fixedly connected with of flexible display screen 92, spacing recess 10 with spacing iron plate 11 sliding connection, the equal fixedly connected with in both sides of spacing recess 10 inner wall adsorbs magnetic path 12.
Through spacing recess 10 and 11 sliding connection of spacing iron plate for flexible display screen 92 can only the horizontal slip, and when flexible display screen 92 roll-off completely or totally roll-in, adsorb magnetic path 12 and all can adsorb spacing iron plate 11, make flexible display screen 92 more stable.
Compared with the related art, the unmanned airborne ammunition launching platform provided by the invention has the following beneficial effects:
through the flexible display screen 92 that sets up on the handheld transceiver 8 in ground, can be when not using with flexible display screen 92 inside the income casing 81, for flexible display screen 92 provides prevents pressing the protection, when needing to use the handheld transceiver 8 in ground, can pull out the use of flexible display screen 92, easy operation facilitates the use.
The above description is only an embodiment of the present invention, and not intended to limit the scope of the present invention, and all modifications of equivalent structures and equivalent processes, which are made by using the contents of the present specification and the accompanying drawings, or directly or indirectly applied to other related technical fields, are included in the scope of the present invention.
Claims (10)
1. An unmanned airborne ammunition firing platform, comprising:
an unmanned aerial vehicle;
the cloud platform is fixed at the bottom of the unmanned aerial vehicle and comprises a rotating support, a driving motor and a driving control module are arranged on the rotating support, and an angle sensor used for being matched with the driving control module to control the rotating angle of the rotating support is fixedly connected to one side of the rotating support;
the ammunition launcher is fixedly arranged on the cradle head and comprises a triple launching barrel, and a locking device for aiming and locking and a trigger generator for controlling the triple launching barrel are arranged on the triple launching barrel;
the aiming assembly is fixedly installed on the holder, and comprises a camera and optical equipment used for controlling the camera.
2. An unmanned airborne ammunition firing platform according to claim 1 wherein a mounting bracket is provided on the triplet of firing barrels for mounting the triplet of firing barrels to the cradle head.
3. The unmanned airborne ammunition launching platform of claim 2, wherein the rotating bracket is fixed to the bottom of the unmanned aerial vehicle, and the output end of the driving motor is fixedly connected with the mounting bracket for driving the mounting bracket to rotate.
4. An unmanned airborne ammunition firing platform according to claim 3 wherein the camera is secured to the mounting bracket below the triple launch barrel.
5. The unmanned airborne ammunition launching platform of claim 1, wherein the unmanned aerial vehicle is internally provided with an information launching and receiving assembly, the information launching and receiving assembly comprises an airborne receiver and a video transmitter, and the airborne receiver is electrically connected with the video transmitter.
6. An unmanned airborne ammunition launching platform according to claim 5, wherein said master control module is used for control of said unmanned aerial vehicle and is electrically connected to both said airborne receiver and said video transmitter.
7. An unmanned airborne ammunition launching platform according to claim 6 wherein the master control module is electrically connected to the drive control module and the video transmitter is electrically connected to the optical device.
8. An unmanned airborne ammunition launching platform according to claim 7, further comprising a ground-based hand-held transceiver for controlling the unmanned aerial vehicle in cooperation with the master control module, the ground-based hand-held transceiver comprising a housing, an outer surface of which is provided with a control panel with a plurality of control switches;
the telescopic display screen comprises a telescopic assembly, wherein the telescopic assembly is arranged in the shell and comprises a telescopic groove, the inner part of the telescopic groove is movably connected with a telescopic display screen, a wire is arranged at the bottom of the telescopic display screen, wear-resistant rubber pads are fixedly connected to the two sides of the telescopic display screen, and one side of the telescopic display screen is fixedly connected with a handle which is used for pulling the telescopic display screen out of the telescopic groove.
9. An unmanned airborne ammunition launching platform according to claim 8, wherein the telescopic slot is provided inside the unmanned aerial vehicle, and one end of the wire passes through the unmanned aerial vehicle and is fixedly connected with the control panel.
10. The unmanned aerial vehicle carries ammunition launching platform of claim 8, wherein limiting grooves are formed in two sides of the inner wall of the telescopic groove, limiting iron blocks are fixedly connected to two sides of the telescopic display screen, the limiting grooves are in sliding connection with the limiting iron blocks, and adsorbing magnetic blocks are fixedly connected to two sides of the inner wall of the limiting groove.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202111563854.7A CN114061373A (en) | 2021-12-20 | 2021-12-20 | Unmanned aerial vehicle carries ammunition launching platform |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202111563854.7A CN114061373A (en) | 2021-12-20 | 2021-12-20 | Unmanned aerial vehicle carries ammunition launching platform |
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| Publication Number | Publication Date |
|---|---|
| CN114061373A true CN114061373A (en) | 2022-02-18 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN202111563854.7A Pending CN114061373A (en) | 2021-12-20 | 2021-12-20 | Unmanned aerial vehicle carries ammunition launching platform |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114963898A (en) * | 2022-06-15 | 2022-08-30 | 西安工业大学 | System and method for testing shot blasting point position based on unmanned aerial vehicle |
-
2021
- 2021-12-20 CN CN202111563854.7A patent/CN114061373A/en active Pending
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114963898A (en) * | 2022-06-15 | 2022-08-30 | 西安工业大学 | System and method for testing shot blasting point position based on unmanned aerial vehicle |
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