CN220332951U - Special anti-sniper unmanned aerial vehicle - Google Patents
Special anti-sniper unmanned aerial vehicle Download PDFInfo
- Publication number
- CN220332951U CN220332951U CN202321819273.XU CN202321819273U CN220332951U CN 220332951 U CN220332951 U CN 220332951U CN 202321819273 U CN202321819273 U CN 202321819273U CN 220332951 U CN220332951 U CN 220332951U
- Authority
- CN
- China
- Prior art keywords
- machine body
- fixedly connected
- folding
- unmanned aerial
- aerial vehicle
- 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
- 230000001681 protective effect Effects 0.000 claims description 15
- 238000001931 thermography Methods 0.000 claims description 12
- 230000005540 biological transmission Effects 0.000 claims description 3
- 238000005516 engineering process Methods 0.000 description 4
- 238000001514 detection method Methods 0.000 description 3
- 238000010586 diagram Methods 0.000 description 3
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 description 2
- 238000004891 communication Methods 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
- 230000004044 response Effects 0.000 description 2
- 230000006978 adaptation Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000011521 glass Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000005457 optimization Methods 0.000 description 1
- 238000003825 pressing Methods 0.000 description 1
- 230000008569 process Effects 0.000 description 1
Abstract
The utility model discloses an anti-sniper special unmanned aerial vehicle, which comprises a machine body, wherein an anti-sniper device is fixedly connected to one side of the machine body, a GNSS positioning antenna is rotatably connected to the top surface of one side of the machine body, which is away from the anti-sniper device, through a second folding piece, folding type horn arms are fixedly connected to four corner parts on the outer side of the machine body, folding type screw propellers are fixedly connected to one end, which is away from the machine body, of the machine body, connecting pieces are symmetrically arranged on the bottom surface of the machine body, and pull-plug landing gears are detachably connected to the connecting pieces; and a power supply system is arranged in the machine body and is electrically connected with the GNSS positioning antenna, the anti-sniping device, the folding horn, the folding propeller and the second folding piece. According to the utility model, a reliable mounting platform is provided for the anti-sniping device through the unmanned aerial vehicle, and the anti-sniping device can accurately position and identify the target through flight, hovering, gesture adjustment and the like of the unmanned aerial vehicle, so that a dangerous point reconnaissance task of a reconnaissance area is completed.
Description
Technical Field
The utility model relates to the technical field of special unmanned aerial vehicles, in particular to an anti-sniper special unmanned aerial vehicle.
Background
The unmanned aerial vehicle can quickly reach a target area in complex terrains such as mountains, cities, jungles and the like without being limited by terrains, and the anti-sniping device is arranged on the unmanned aerial vehicle, so that the unmanned aerial vehicle becomes another new concept special device capable of executing diversified tasks such as patrol flight, reconnaissance detection, anti-sniping enemy equipment and the like; with the development of anti-sniping technology and micro unmanned aerial vehicle technology, the anti-sniping unmanned aerial vehicle has extremely wide application prospect in future war.
The existing anti-sniping device adopts thermal imaging, laser ranging and infrared technology, and other lenses except for the lens of the thermal imaging detector are provided with lens protection glass; when anti-sniping is needed, a manual anti-sniping device is usually used, so that the problems of low maneuverability and flexibility exist, and the defect of the anti-sniping range is greatly limited; the unmanned plane is flexible and flexible, and the anti-sniping range can be effectively improved; therefore, what is needed is an anti-sniper special unmanned aerial vehicle, which can realize the search, detection, identification, positioning and striking of snipers and photoelectric equipment in a wider range by combining an anti-sniper device with an unmanned aerial vehicle technology.
Disclosure of Invention
The utility model aims to provide an anti-sniper special unmanned aerial vehicle so as to solve the problems in the prior art.
In order to achieve the above object, the present utility model provides the following solutions: the utility model provides an anti-sniper special unmanned aerial vehicle, which comprises a machine body, wherein an anti-sniper device is fixedly connected to one side of the machine body, a GNSS positioning antenna is rotationally connected to the top surface of one side of the machine body, which is away from the anti-sniper device, through a second folding piece, folding type horn arms are fixedly connected to four corner parts on the outer side of the machine body, folding type screw propellers are fixedly connected to one end, which is away from the machine body, of the machine body, connecting pieces are symmetrically arranged on the bottom surface of the machine body, and pull-plug landing gears are detachably connected to the connecting pieces; the power supply system is arranged in the machine body and is electrically connected with the GNSS positioning antenna, the anti-sniping device, the folding horn, the folding propeller and the second folding piece.
Preferably, the anti-sniping device comprises a protective shell, a sighting telescope is fixedly connected to the center in the protective shell, a thermal imager is arranged on one side of the sighting telescope, an infrared detector and a laser detector are arranged on the other side of the sighting telescope, the laser detector is arranged above the infrared detector, and the thermal imager, the infrared detector and the laser detector are all arranged in the protective shell and are fixedly connected with the protective shell; the bottom surface fixedly connected with attack weapon of protective housing, the gun sight, the thermal imaging appearance, infrared detector, laser detector, attack weapon all with electrical connection of electrical power generating system.
Preferably, the folding horn comprises a first folding member, one end of the first folding member is fixedly connected with a connecting rod, one end of the connecting rod deviating from the first folding member is fixedly connected with the folding propeller, the other end of the first folding member is fixedly connected with the machine body, and the first folding member is electrically connected with the power supply system.
Preferably, the foldable propeller comprises a propeller clamping seat, blades are symmetrically arranged on the top surface of the propeller clamping seat, the blades are fixedly connected with the propeller clamping seat, a motor is connected with the propeller clamping seat in a transmission mode, the motor is fixedly connected with the connecting rod, and the motor is electrically connected with the power supply system.
Preferably, the connecting piece includes the supporting seat, the supporting seat with fuselage fixed connection, the supporting seat deviates from the one end fixedly connected with sleeve of fuselage, a plurality of locating hole has been seted up to symmetry on the telescopic inner wall, the sleeve with pull out plug-in undercarriage detachable connection.
Preferably, the plug-in undercarriage comprises a transverse plate, a vertical rod is fixedly connected to the center of the transverse plate, the vertical rod is perpendicular to the transverse plate, protrusions are symmetrically arranged on one end of the vertical rod, which is away from the transverse plate, in circumferential direction, and are in sliding connection with the vertical rod, and the protrusions are matched with the positioning holes.
Preferably, the power supply system comprises a controller, the controller is electrically connected with a battery, the controller and the battery are all installed in the machine body, and the controller is electrically connected with the sighting telescope, the thermal imaging instrument, the infrared detector, the laser detector, the attack weapon, the motor, the GNSS positioning antenna, the first folding piece and the second folding piece.
The utility model discloses the following technical effects:
1. according to the utility model, the unmanned aerial vehicle is convenient to install and disassemble rapidly through the folding horn, the folding propeller, the GNSS positioning antenna and the pluggable undercarriage, so that the storage space and the installing and disassembling time are effectively saved.
2. According to the utility model, the unmanned aerial vehicle is used as a platform, and the unmanned aerial vehicle has the characteristics of high response speed, high flexibility, good maneuverability, small volume and the like, so that the anti-sniping device is arranged on the unmanned aerial vehicle, the unmanned aerial vehicle provides a reliable installation platform for the anti-sniping device, and the anti-sniping device can accurately position and identify the target through the flight, hovering, posture adjustment and the like of the unmanned aerial vehicle, so that the dangerous point reconnaissance task of the reconnaissance area is completed.
Drawings
In order to more clearly illustrate the embodiments of the present utility model or the technical solutions in the prior art, the drawings that are needed in the embodiments will be briefly described below, and it is obvious that the drawings in the following description are only some embodiments of the present utility model, and other drawings may be obtained according to these drawings without inventive effort for a person skilled in the art.
FIG. 1 is a schematic diagram of the structure of the present utility model;
FIG. 2 is a schematic diagram of a power system according to the present utility model;
FIG. 3 is a schematic view of a folding propeller structure according to the present utility model;
fig. 4 is a schematic diagram of the anti-sniping device of the present utility model;
FIG. 5 is a schematic view of a connector structure according to the present utility model;
FIG. 6 is a schematic cross-sectional view of a vertical rod according to the present utility model;
wherein, 1, the fuselage; 2. folding type arm; 3. folding propeller; 4. a plug-in undercarriage; 5. a GNSS positioning antenna; 6. anti-sniping device; 7. a motor; 8. a power supply system; 9. a first folding member; 10. a paddle; 11. a paddle holder; 12. a connecting piece; 13. a thermal imager; 14. an infrared detector; 15. a laser detector; 16. a second folder; 17. a support base; 18. a sleeve; 19. positioning holes; 20. a protrusion; 21. a spring; 22. a round hole; 23. and a vertical rod.
Detailed Description
The following description of the embodiments of the present utility model will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present utility model, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the utility model without making any inventive effort, are intended to be within the scope of the utility model.
In order that the above-recited objects, features and advantages of the present utility model will become more readily apparent, a more particular description of the utility model will be rendered by reference to the appended drawings and appended detailed description.
Referring to fig. 1-6, the utility model discloses an anti-sniper special unmanned aerial vehicle, which comprises a machine body 1, wherein an anti-sniper device 6 is fixedly connected to one side of the machine body 1, a GNSS positioning antenna 5 is rotatably connected to the top surface of one side of the machine body 1, which is away from the anti-sniper device 6, through a second folding piece 16, folding horn 2 is fixedly connected to four corners on the outer side of the machine body 1, folding screw 3 is fixedly connected to one end of the folding horn 2, which is away from the machine body 1, connecting pieces 12 are symmetrically arranged on the bottom surface of the machine body 1, and the connecting pieces 12 are detachably connected with a pull-plug landing gear 4; the power supply system 8 is arranged in the machine body 1, and the power supply system 8 is electrically connected with the GNSS positioning antenna 5, the anti-sniping device 6, the folding horn 2, the folding propeller 3 and the second folding piece 16.
According to the utility model, the folding horn 2, the folding propeller 3 and the plug-in undercarriage 4 are adopted, so that the unmanned aerial vehicle can be conveniently and rapidly installed and disassembled, and the storage space and the time for installing and detaching are effectively saved; according to the utility model, the unmanned aerial vehicle is used as a platform, and the unmanned aerial vehicle has the characteristics of high response speed, high flexibility, good maneuverability, small volume and the like, so that the anti-sniping device 6 is installed on the unmanned aerial vehicle, the unmanned aerial vehicle provides a reliable installation platform for the anti-sniping device 6, and the anti-sniping device 6 can accurately position and identify the target through the flight, hovering, posture adjustment and the like of the unmanned aerial vehicle, so that the dangerous point reconnaissance task of the reconnaissance area is completed.
According to a further optimization scheme, the anti-sniping device 6 comprises a protective shell, a sighting telescope is fixedly connected to the center in the protective shell, a thermal imager 13 is arranged on one side of the sighting telescope, an infrared detector 14 and a laser detector 15 are arranged on the other side of the sighting telescope, the laser detector 15 is arranged above the infrared detector 14, and the thermal imager 13, the infrared detector 14 and the laser detector 15 are all arranged in the protective shell and are fixedly connected with the protective shell; the bottom surface fixedly connected with attack weapon of protective housing, gun sight, thermal imaging appearance 13, infrared detector 14, laser detector 15, attack weapon all with electrical connection of electrical power generating system 8. The target area can be effectively detected through the sighting telescope, the thermal imaging instrument 13, the infrared detector 14 and the laser detector 15.
Further optimizing scheme, folding horn 2 includes first folding piece 9, and the one end fixedly connected with connecting rod of first folding piece 9, the one end that the connecting rod deviates from first folding piece 9 and folding screw 3 fixed connection, the other end and the fuselage 1 fixed connection of first folding piece 9, first folding piece 9 and electrical power generating system 8 electric connection. The deployment and retraction of the connecting rod can be achieved by controlling the first folding member 9.
Further optimizing scheme, folding screw 3 includes oar holder 11, and the symmetry is provided with paddle 10 on the top surface of oar holder 11, paddle 10 and oar holder 11 fixed connection, and the transmission of oar holder 11 is connected with motor 7, motor 7 and connecting rod fixed connection, motor 7 and electrical power generating system 8 electric connection. The motor 7 drives the paddle holder 11 to rotate, and the paddle holder 11 drives the paddle 10 to rotate, so that the unmanned aerial vehicle can fly.
Further optimizing scheme, connecting piece 12 includes supporting seat 17, and supporting seat 17 and fuselage 1 fixed connection, and supporting seat 17 deviates from the one end fixedly connected with sleeve 18 of fuselage 1, and a plurality of locating hole 19 have been seted up to the symmetry on the inner wall of sleeve 18, and sleeve 18 is connected with the detachable of plug-in undercarriage 4.
Further optimizing scheme, pull out plug-in undercarriage 4 includes the diaphragm, and the center fixedly connected with montant 23 of diaphragm, montant 23 set up perpendicularly with the diaphragm, and the one end circumference upwards symmetry that montant 23 deviates from the diaphragm is provided with protruding 20, protruding 20 and montant 23 sliding connection, protruding 20 and locating hole 19 looks adaptation. Round holes 22 are symmetrically formed in the circumferential direction of the vertical rods 23, one ends of springs 21 are fixedly connected in the round holes 22, the other ends of the springs 21 are fixedly connected with the ends of the protrusions 20 extending into the round holes 22, the vertical rods 23 are inserted into the sleeves 18 through pressing the protrusions 20 into the round holes 22, and the protrusions 20 extend out of the positioning holes 19, so that the vertical rods 23 can be detachably connected with the sleeves 18.
Further optimizing scheme, electrical power generating system 8 includes the controller, and controller electric connection has the battery, and controller, battery are all installed in fuselage 1, and controller and gun sight, thermal imaging appearance 13, infrared detector 14, laser detector 15, attack weapon, motor 7, GNSS location antenna 5, first folding piece 9, second folding piece 16 electric connection. The controller comprises a flight control system, a navigation system and a communication system, and the anti-sniping device 6 and the unmanned aerial vehicle are controlled through the flight control system, the navigation system and the communication system, so that the GNSS positioning antenna 5 can effectively position the unmanned aerial vehicle.
The working process comprises the following steps: remote operation personnel start control system, connect unmanned aerial vehicle's controller, expand through controller control unmanned aerial vehicle folding horn 2, control motor 7 drives paddle 10 and rotates, and then control unmanned aerial vehicle flies, after reaching the target scope, carries out reconnaissance to the target scope through thermal imaging instrument 13, infrared detector 14, laser detector 15, after confirming the target, aims anti-sniping target sniper or photoelectric device through the gun sight to hit the target.
After the unmanned aerial vehicle finishes the task and returns, lift down montant 23 in sleeve 18, make unmanned aerial vehicle's deposit can reduce the occupation in space, effectively practiced thrift the space.
The utility model can be used for executing the tasks of warning, security or anti-sniping detection in battlefield environment in important occasions.
In the description of the present utility model, it should be understood that the terms "longitudinal," "transverse," "upper," "lower," "front," "rear," "left," "right," "vertical," "horizontal," "top," "bottom," "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 present utility model, and do not indicate or imply that the devices or elements referred to must have a particular orientation, be constructed and operated in a particular orientation, and thus should not be construed as limiting the present utility model.
The above embodiments are only illustrative of the preferred embodiments of the present utility model and are not intended to limit the scope of the present utility model, and various modifications and improvements made by those skilled in the art to the technical solutions of the present utility model should fall within the protection scope defined by the claims of the present utility model without departing from the design spirit of the present utility model.
Claims (7)
1. An anti-sniper special unmanned aerial vehicle which characterized in that: the anti-sniping device comprises a machine body (1), an anti-sniping device (6) is fixedly connected to one side of the machine body (1), a GNSS positioning antenna (5) is rotationally connected to the top surface of one side of the machine body (1) deviating from the anti-sniping device (6) through a second folding piece (16), folding type arms (2) are fixedly connected to four corners on the outer side of the machine body (1), folding type propeller (3) is fixedly connected to one end of the folding type arms (2) deviating from the machine body (1), connecting pieces (12) are symmetrically arranged on the bottom surface of the machine body (1), and pull-plug landing gears (4) are detachably connected to the connecting pieces (12). The power supply system (8) is arranged in the machine body (1), and the power supply system (8) is electrically connected with the GNSS positioning antenna (5), the anti-sniping device (6), the folding horn (2), the folding propeller (3) and the second folding piece (16).
2. The anti-sniper special unmanned aerial vehicle of claim 1, wherein: the anti-sniping device (6) comprises a protective shell, a sighting telescope is fixedly connected to the center in the protective shell, a thermal imaging instrument (13) is arranged on one side of the sighting telescope, an infrared detector (14) and a laser detector (15) are arranged on the other side of the sighting telescope, the laser detector (15) is arranged above the infrared detector (14), and the thermal imaging instrument (13), the infrared detector (14) and the laser detector (15) are all arranged in the protective shell and are fixedly connected with the protective shell; the bottom surface fixedly connected with attack weapon of protective housing, the gun sight thermal imaging appearance (13), infrared detector (14), laser detector (15) attack weapon all with electrical connection of electrical power generating system (8).
3. The anti-sniper special unmanned aerial vehicle of claim 2, wherein: the folding horn (2) comprises a first folding piece (9), one end fixedly connected with connecting rod of the first folding piece (9), one end of the connecting rod deviating from the first folding piece (9) is fixedly connected with the folding propeller (3), the other end of the first folding piece (9) is fixedly connected with the machine body (1), and the first folding piece (9) is electrically connected with the power supply system (8).
4. The anti-sniper special unmanned aerial vehicle of claim 3, wherein: the foldable propeller (3) comprises a propeller clamping seat (11), blades (10) are symmetrically arranged on the top surface of the propeller clamping seat (11), the blades (10) are fixedly connected with the propeller clamping seat (11), a motor (7) is connected with the propeller clamping seat (11) in a transmission mode, the motor (7) is fixedly connected with the connecting rod, and the motor (7) is electrically connected with the power supply system (8).
5. The anti-sniper special unmanned aerial vehicle of claim 1, wherein: the connecting piece (12) comprises a supporting seat (17), the supporting seat (17) is fixedly connected with the machine body (1), one end, deviating from the machine body (1), of the supporting seat (17) is fixedly connected with a sleeve (18), a plurality of positioning holes (19) are symmetrically formed in the inner wall of the sleeve (18), and the sleeve (18) is detachably connected with the plug-in undercarriage (4).
6. The anti-sniper special unmanned aerial vehicle of claim 5, wherein: the plug-in undercarriage (4) comprises a transverse plate, a vertical rod (23) is fixedly connected to the center of the transverse plate, the vertical rod (23) is perpendicular to the transverse plate, protrusions (20) are symmetrically arranged on one end of the vertical rod (23) deviating from the transverse plate in circumferential direction, the protrusions (20) are in sliding connection with the vertical rod (23), and the protrusions (20) are matched with the positioning holes (19).
7. The anti-sniper special unmanned aerial vehicle of claim 4, wherein: the power supply system (8) comprises a controller, the controller is electrically connected with a battery, the controller and the battery are all installed in the machine body (1), and the controller is electrically connected with the sighting telescope, the thermal imaging instrument (13), the infrared detector (14), the laser detector (15), the attack weapon, the motor (7), the GNSS positioning antenna (5), the first folding piece (9) and the second folding piece (16).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321819273.XU CN220332951U (en) | 2023-07-12 | 2023-07-12 | Special anti-sniper unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321819273.XU CN220332951U (en) | 2023-07-12 | 2023-07-12 | Special anti-sniper unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN220332951U true CN220332951U (en) | 2024-01-12 |
Family
ID=89455425
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202321819273.XU Active CN220332951U (en) | 2023-07-12 | 2023-07-12 | Special anti-sniper unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN220332951U (en) |
-
2023
- 2023-07-12 CN CN202321819273.XU patent/CN220332951U/en active Active
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN106809402B (en) | Automatic auxiliary landing system of rotor unmanned aerial vehicle and control method thereof | |
| CN109458881A (en) | Aircraft intercepting system | |
| CN109460066A (en) | Virtual reality system for aircraft | |
| CN105292477A (en) | Wrist type portable accompanying flight autonomous supervision unmanned aerial vehicle | |
| CN204916210U (en) | Cloud platform overhead electric power patrols line unmanned aerial vehicle | |
| CN114489148B (en) | Anti-unmanned aerial vehicle system based on intelligent detection and electronic countermeasure | |
| CN220332951U (en) | Special anti-sniper unmanned aerial vehicle | |
| WO2021212870A1 (en) | Unmanned aerial vehicle | |
| CN211167458U (en) | Remote control unmanned aerial vehicle high altitude anti-wind anti-shake device | |
| CN110550198A (en) | Rock wall fixed point type unmanned aerial vehicle | |
| CN218806669U (en) | Low-slow small target reconnaissance countercheck system based on multi-rotor unmanned aerial vehicle | |
| CN205221113U (en) | Portable companion of wrist formula flies autonomic control unmanned aerial vehicle | |
| CN113654408A (en) | Autonomous mine clearance system for throwing type mines based on multi-rotor unmanned aerial vehicle platform | |
| CN212685907U (en) | Survey and drawing unmanned aerial vehicle with protector | |
| CN210618461U (en) | Unmanned aerial vehicle capable of being anchored on cliff | |
| CN209988113U (en) | Unmanned plane | |
| CN212195850U (en) | Unmanned aerial vehicle buffer stop | |
| CN108073189B (en) | Large-load double-shaft automatic tracking holder | |
| CN109782780A (en) | A kind of winged control examination protective device of multi-rotor unmanned aerial vehicle | |
| CN208453241U (en) | A kind of unmanned plane with defencive function for taking photo by plane | |
| CN209988114U (en) | Unmanned plane | |
| CN208412138U (en) | A kind of power patrol unmanned machine | |
| CN215725462U (en) | Autonomous mine clearance system for throwing type mines based on multi-rotor unmanned aerial vehicle platform | |
| CN108248815B (en) | Method and device for acquiring high-precision remote sensing data | |
| KR102322098B1 (en) | Drone capable of precise dropping |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |