CN218877605U - Scouting and printing integrated remote control unmanned aerial vehicle and system - Google Patents
Scouting and printing integrated remote control unmanned aerial vehicle and system Download PDFInfo
- Publication number
- CN218877605U CN218877605U CN202223261994.1U CN202223261994U CN218877605U CN 218877605 U CN218877605 U CN 218877605U CN 202223261994 U CN202223261994 U CN 202223261994U CN 218877605 U CN218877605 U CN 218877605U
- Authority
- CN
- China
- Prior art keywords
- aerial vehicle
- unmanned aerial
- control unit
- foot rest
- flight
- 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
Images
Classifications
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Toys (AREA)
Abstract
The utility model provides a scouting and batting integrated remote control unmanned aerial vehicle and system, including the unmanned aerial vehicle main part, be equipped with horn, foot rest and photoelectricity nacelle in the main part, the main part bottom is equipped with the block portion, be equipped with joint portion on the foot rest, the foot rest through joint portion with main part bottom block portion joint, install shooting device on the foot rest, the foot rest can be dismantled fast, makes things convenient for the ammunition supply of shooting device, the main part still is equipped with the cavity, puts control module and power supply unit in the cavity, saves space, control module includes flight control unit, photoelectricity nacelle control unit, shooting control unit and RTK measuring apparatu, the RTK measuring apparatu with the flight control unit is connected, the flight control unit is used for controlling unmanned aerial vehicle flight; the photoelectric pod control unit is used for controlling the photoelectric pod to acquire and transmit data; the fire control launching process is simple in time sequence, and meets the tasks of attacking and intercepting ground and aerial targets.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field, in particular to examine and beat integrative remote control unmanned aerial vehicle and system.
Background
The existing micro unmanned aerial vehicle is low in cost, convenient to carry and operate and high in radar concealment, and equipment can be used for urban anti-terrorism special combat and individual combat. The main purpose is to provide instant on-site information, which is beneficial to the assistance of combat decision, the reconnaissance and search and rescue of a closed space, the continuous monitoring and target identification of a combat area, and the like. But in the in-service use process, current miniature unmanned aerial vehicle also has multiple defect and challenge, and current miniature unmanned aerial vehicle generally only carries the camera, does not carry the shooting part, and the killer chain of fighting is imperfect.
The reconnaissance and striking integrated unmanned aerial vehicle is developed on the basis of a reconnaissance unmanned aerial vehicle and has reconnaissance and striking capabilities. The attack robot has the advantages of long dead time, quick attack rhythm, wide attack range and the like, can adapt to information battles, and is suitable for equipping fast response troops.
Along with the rapid development of a domestic and overseas investigation and combat integrated unmanned aerial vehicle system, the small unmanned helicopter has the advantages of small size, low cost, capability of vertical take-off and landing and hovering, low requirement on a take-off and landing field, and high popularity of more and more users, and can be widely applied to tasks such as aerial photography investigation, accurate combat, battlefield monitoring and the like. However, the traditional small unmanned helicopter has the disadvantages of difficult ammunition supply, high noise, large volume for detecting load, heavy weight, short endurance time, high manufacturing cost and complex fire control launching process time sequence. Therefore, a low-cost, light-weight and simply-controlled integrated unmanned aerial vehicle and a control system for surveying and shooting need to be designed to meet the tasks of attacking and intercepting ground and aerial targets, aerial photography and reconnaissance, accurate fighting, battlefield monitoring and the like.
SUMMERY OF THE UTILITY MODEL
The utility model aims to solve the technical problem that a remote control is examined and is beaten integrative unmanned aerial vehicle and system is provided, aim at solving among the prior art unmanned aerial vehicle and carry ammunition supply difficult, listen bulky, the weight of load big, with high costs, technical problem such as fire control transmission flow chronogenesis complicacy.
In order to solve the technical problem, the utility model discloses a technical scheme be: the provided scouting and batting integrated remote control unmanned aerial vehicle comprises an unmanned aerial vehicle main body, wherein a machine arm, a foot rest and a photoelectric pod are arranged on the main body, one end of the machine arm is fixed on a main body shell, and the other end of the machine arm is provided with a propeller driven by a brushless motor; the unmanned aerial vehicle comprises a main body and is characterized in that a clamping part is arranged at the bottom of the main body, a clamping part is arranged on a foot rest, the foot rest is clamped with the clamping part at the bottom of the main body through the clamping part, a shooting device is mounted on the foot rest, a photoelectric pod is movably mounted on the main body, the main body is also provided with a cavity, a control module and a power supply device are arranged in the cavity, the control module comprises a flight control unit, a photoelectric pod control unit, a shooting control unit and a RTK measuring instrument, the RTK measuring instrument is connected with the flight control unit, and the flight control unit is used for controlling the unmanned aerial vehicle to fly; the photoelectric pod control unit is used for controlling the photoelectric pod to acquire and transmit data; the shooting control unit is used for controlling the shooting device to shoot.
Furthermore, the number of the machine arms is four, the machine arms are Y-shaped, the brushless motors and the propellers are fixed above and below the ends of the Y-shaped arms, the number of the brushless motors and the propellers is eight, and the brushless motors are electrically connected with the power supply device.
Further, the horn middle section is equipped with folding mechanism, and when unmanned aerial vehicle stop work, folding mechanism makes the horn be the formula of embracing folding.
Furthermore, still be equipped with the device of propaganda directed to communicate on the main part, the device of propaganda directed to communicate with ground through the radio.
Further, the shooting device is an aviation gun or an aviation cannon.
Furthermore, the foot rest is provided with a fixing hole, the shooting device is fixed on the foot rest through the fixing hole, and the bottom of the foot rest is provided with two parallel cross rods.
The utility model also provides a scouting and batting integrated remote control unmanned aerial vehicle system, which comprises a ground end and a flying end, wherein the ground end and the flying end pass through a wireless network to transmit signals mutually;
the ground end is used for receiving the flight end data and sending an instruction to the flight end;
the flight end comprises a flight control unit, a photoelectric pod control unit, a shooting control unit and an RTK measuring instrument, the RTK measuring instrument is connected with the flight control unit, and the flight control unit is used for controlling the unmanned aerial vehicle to fly; the photoelectric pod control unit is used for controlling the photoelectric pod to acquire and transmit data; the shooting control unit is used for controlling the shooting device to shoot.
Further, the ground end is equipped with the speech communication unit, the speech communication unit is used for controlling the calling device of carrying on the unmanned aerial vehicle.
The beneficial effects of the utility model reside in that: the utility model provides a scouting and batting integrated remote control unmanned aerial vehicle, through installing the shooting device on the foot rest, the foot rest passes through joint portion and main part bottom block portion joint, the foot rest can be dismantled and assembled fast, make things convenient for the ammunition supply of shooting device, the main part still is equipped with the cavity, puts control module and power supply unit in the cavity, saves space, and the horn quantity is four, is Y style of calligraphy, four-axis eight-oar structure, powerful power redundancy, reduces unmanned aerial vehicle's volume, improves continuation of the journey and load-carrying capacity; the horn middle section is equipped with folding mechanism, and when unmanned aerial vehicle stop work, folding mechanism makes the horn be the formula of embracing folding, conveniently carries. The utility model also provides an it transmits each other to observe and beat integrative remote control system, through ground end and flight end data instruction, carries out remote control and carries out corresponding order according to the instruction that ground end sent to unmanned aerial vehicle high-efficiently, and fire control emission flow is simple controllable, has improved work efficiency greatly.
Drawings
In order to more clearly illustrate the technical solutions of the embodiments of the present invention, the drawings required for the embodiments or the prior art descriptions will be briefly introduced below, and it is obvious that the drawings in the following description are only some embodiments of the present invention, and it is obvious for those skilled in the art to obtain other drawings without inventive labor.
Fig. 1 is a schematic structural view of an investigation and printing integrated remote control unmanned aerial vehicle of the utility model;
fig. 2 is a schematic structural view of a main body of the scouting and printing integrated remote control unmanned aerial vehicle of the present invention;
fig. 3 is a schematic structural view of a tripod of the scouting and batting integrated remote control unmanned aerial vehicle of the present invention;
fig. 4 is the utility model relates to a reconnaissance and beat integrative remote control unmanned aerial vehicle system schematic diagram.
Description of reference numerals:
10. a main body; 11. A cavity; 20. A foot rest; 21. A clamping part;
22. a cross bar; 23. A fixing hole; 30. A boom; 31. A propeller;
32. a brushless motor; 33. A folding mechanism; 40. A photovoltaic pod; 50. A shooting device;
60. an RTK measuring instrument;
100. a flight end; 101. A flight control unit; 102 a photovoltaic pod control unit;
103. a shooting control unit; 200. And (7) a ground end.
Detailed Description
Reference will now be made in detail to the embodiments of the present invention, examples of which are illustrated in the accompanying drawings, wherein like reference numerals refer to the same or similar elements or elements having the same or similar functions throughout. The embodiments described below by referring to the drawings are exemplary intended for explaining the present invention, and should not be construed as limiting the present invention.
In the description of the present invention, it is to be understood that the terms "length", "width", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", and the like indicate orientations or positional relationships based on those shown in the drawings, and are merely for convenience of description and simplicity of description, and do not indicate or imply that the device or element being 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 invention.
Furthermore, the terms "first", "second" and "first" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance or to implicitly indicate the number of technical features indicated. Thus, a feature defined as "first" or "second" may explicitly or implicitly include one or more of that feature. In the description of the present invention, "a plurality" means two or more unless specifically limited otherwise.
In the present invention, unless otherwise explicitly specified or limited, the terms "mounted," "connected," "secured," and the like are to be construed broadly, e.g., as being fixedly connected, detachably connected, or integrated; can be mechanically or electrically connected; either directly or indirectly through intervening media, either internally or in any other relationship. The specific meaning of the above terms in the present invention can be understood according to specific situations by those skilled in the art.
As shown in fig. 1 to 4, an embodiment of the present invention provides a scouting and batting integrated remote control unmanned aerial vehicle, including an unmanned aerial vehicle main body 10, wherein the main body 10 is provided with a horn 30, a foot rest 20 and a photoelectric pod 40, one end of the horn 30 is fixed on a housing of the main body 10, and the other end is provided with a propeller 31 driven by a brushless motor 32; the unmanned aerial vehicle flight control system is characterized in that a clamping part (not shown) is arranged at the bottom of the main body 10, a clamping part 21 is arranged on the foot stand 20, the foot stand 20 is clamped with the clamping part at the bottom of the main body 10 through the clamping part 21, the shooting device 50 is installed on the foot stand 20, the photoelectric pod 40 is movably installed on the main body 10, the main body 10 is further provided with a cavity 11, a control module and a power supply device are arranged in the cavity, the control module comprises a flight control unit 101, a photoelectric pod control unit 102, a shooting control unit 103 and an RTK measuring instrument 60, the RTK measuring instrument 60 is connected with the flight control unit 101, and the flight control unit 101 is used for controlling the unmanned aerial vehicle to fly; the photoelectric pod control unit 102 is used for controlling the photoelectric pod 40 to acquire and transmit data; the firing control unit 103 is used for controlling firing of the firing means 50.
The utility model discloses an install the shooting device on the foot rest, the foot rest passes through joint portion and main part bottom block portion joint, but foot rest quick assembly disassembly, make things convenient for the ammunition supply of shooting device, the main part still is equipped with the cavity, put control module and power supply unit in the cavity, save space, and through technologies such as overall process remote control, stadia link, combination navigation, possess multiple use and ability such as photoelectric image reconnaissance and supervision, radar image reconnaissance, communication signal detects, have convenient operation, high reliability, maintain characteristics such as the guarantee nature is good. The shooting device is equipped with photoelectric sighting device, large capacity bullet case, installs on the unmanned aerial vehicle foot rest, but foot rest quick assembly disassembly makes things convenient for the ammunition supply of shooting device. The system is suitable for various task requirements of urban street fighting, field fighting, frontier defense, firepower support, small squad operation and the like.
Further, as shown in fig. 1 and 2, the number of the horn 30 is four, the horn 30 is Y-shaped, the brushless motor 32 and the propeller 31 are fixed above and below the end of the Y-shaped, the number of the brushless motor 32 is eight, and the brushless motor 32 is electrically connected to the power supply device. Adopt eight oar structures of four-axis, powerful power is redundant, reduces unmanned aerial vehicle's volume, improves duration and load-carrying capacity.
Further, as shown in fig. 1 and fig. 2, the horn 30 middle section is equipped with folding mechanism 33, and when unmanned aerial vehicle stop work, folding mechanism 33 makes the horn be the formula of embracing folding, conveniently carries, and wherein folding mechanism can have multiple form, like node pre-compaction spring drive mode, flexible buckle mode etc..
Further, a megaphone (not shown) is disposed on the main body, and the megaphone transmits signals to the ground 200 through radio. The target is warned by setting a shouting device.
Further, the shooting device 50 is an aircraft gun or an aircraft cannon. The aerial gun or the aerial cannon is arranged on the foot rest of the unmanned aerial vehicle and can receive signals of the ground end, and the aerial gun or the aerial cannon is controlled by a radar to implement automatic aiming shooting. The unmanned aerial vehicle can execute reconnaissance monitoring and ground striking tasks by matching with a pore-forming radar (SAR), a laser guided missile and a GPS guided bomb, can also perform information collection, electronic warfare and search and rescue, and is suitable for military tasks, anti-terrorism maintenance, border patrol and civil use, such as striking the black flight of the unmanned aerial vehicle (the black flight of the unmanned aerial vehicle refers to the air operation in a no-fly area under the condition that the unmanned aerial vehicle is not controlled to operate, and harms public safety.
Further, as shown in fig. 1 and 3, a fixing hole 23 is formed in the foot rest, the shooting device 50 is fixed to the foot rest 20 through the fixing hole 23, and two parallel cross bars 22 are arranged at the bottom of the foot rest 20. The installation is firm and can keep unmanned aerial vehicle steady descending to ground.
As shown in fig. 4, the utility model also provides a reconnaissance and flight integrated remote control unmanned aerial vehicle system, including ground end 200 and flight end 100, ground end 200 and the wireless network that the flight end 100 passes mutually transmit signals;
the ground end 200 is used for receiving the data of the flight end 100 and sending an instruction to the flight end;
the flight terminal 100 comprises a flight control unit 101, a photoelectric pod control unit 102, a shooting control unit 103 and an RTK measuring instrument 60, wherein the RTK measuring instrument 60 is connected with the flight control unit 101, and the flight control unit 101 is used for controlling the flight of the unmanned aerial vehicle; the photoelectric pod control unit 102 is used for controlling the photoelectric pod to acquire and transmit data; the shooting control unit 103 is used for controlling the shooting of the shooting device.
Further, ground end 200 is equipped with the speech communication unit, the speech communication unit is used for controlling the device of shouting of unmanned aerial vehicle last mount.
To sum up, the utility model provides a pair of scouting and fighting integrative remote control unmanned aerial vehicle and system can carry out strategy, battle and tactics reconnaissance, monitors the battlefield, provides the information for the action of combat of army, can regard as attacking unmanned aerial vehicle according to the change of combat mission, attacks, intercepts ground and aerial target, can also be used to the civil affairs usage, like strike "unmanned aerial vehicle black flight" action. The shooting device is arranged on the foot rest, the foot rest is clamped with the clamping portion at the bottom of the main body through the clamping portion, the foot rest can be quickly disassembled and assembled, ammunition supply of the shooting device is facilitated, the main body is further provided with the cavity, the control module and the power supply device are placed in the cavity, space is saved, the number of the arms is four, the arms are Y-shaped, the arms are of a four-axis eight-paddle structure, powerful power redundancy is achieved, the size of the unmanned aerial vehicle is reduced, and endurance and load capacity are improved; the horn middle section is equipped with folding mechanism, and when unmanned aerial vehicle stop work, folding mechanism makes the horn be the formula of embracing folding, conveniently carries. The utility model also provides an it transmits each other to observe and beat integrative remote control system, through ground end and flight end data instruction, carries out remote control and carries out corresponding order according to the instruction that ground end sent to unmanned aerial vehicle high-efficiently, and fire control emission flow is simple controllable, has improved work efficiency greatly.
The above mentioned is only the embodiment of the present invention, and not the limitation of the patent scope of the present invention, all the equivalent transformations made by the contents of the specification and the drawings, or the direct or indirect application in the related technical field, are included in the patent protection scope of the present invention.
Claims (8)
1. A scouting and fighting integrated remote control unmanned aerial vehicle comprises an unmanned aerial vehicle main body and is characterized in that the unmanned aerial vehicle main body is provided with a horn, a foot rest and a photoelectric pod, one end of the horn is fixed on a shell of the unmanned aerial vehicle main body, and the other end of the horn is provided with a propeller driven by a brushless motor; the unmanned aerial vehicle comprises an unmanned aerial vehicle body and is characterized in that a clamping part is arranged at the bottom of the unmanned aerial vehicle body, a clamping part is arranged on a foot rest, the foot rest is clamped with the clamping part at the bottom of the unmanned aerial vehicle body through the clamping part, a shooting device is mounted on the foot rest, a photoelectric pod is movably mounted on the unmanned aerial vehicle body, the unmanned aerial vehicle body is further provided with a cavity, a control module and a power supply device are arranged in the cavity, the control module comprises a flight control unit, a photoelectric pod control unit, a shooting control unit and an RTK measuring instrument, the RTK measuring instrument is connected with the flight control unit, and the flight control unit is used for controlling the unmanned aerial vehicle to fly; the photoelectric pod control unit is used for controlling the photoelectric pod to acquire and transmit data; the shooting control unit is used for controlling the shooting device to shoot.
2. The scout and swatter integrated remote control unmanned aerial vehicle of claim 1, wherein the number of the horn is four, the horn is Y-shaped, the brushless motor and the propeller are fixed above and below the end of the Y-shaped, the number of the brushless motor and the propeller are eight, and the brushless motor is electrically connected with the power supply device.
3. The scouting and printing integrated remote control unmanned aerial vehicle according to claim 1 or 2, wherein a folding mechanism is arranged in the middle section of the horn, and when the unmanned aerial vehicle stops working, the folding mechanism enables the horn to fold in an encircling manner.
4. The unmanned aerial vehicle of claim 1, wherein the main body of the unmanned aerial vehicle is further provided with a megaphone, and the megaphone transmits signals to the ground through radio.
5. The scout and batting integrated remote control unmanned aerial vehicle of claim 1, wherein the shooting device is an aerial gun or an aerial cannon.
6. The scouting and batting integrated remote control unmanned aerial vehicle according to claim 1, wherein fixing holes are formed in the foot rest, the shooting device is fixed to the foot rest through the fixing holes, and two parallel cross rods are arranged at the bottom of the foot rest.
7. A scouting and batting integrated remote control unmanned aerial vehicle system is characterized by comprising a ground end and a flying end, wherein the ground end and the flying end transmit signals to each other through a wireless network;
the ground end is used for receiving the flight end data and sending an instruction to the flight end;
the flight end comprises a flight control unit, a photoelectric pod control unit, a shooting control unit and an RTK measuring instrument, the RTK measuring instrument is connected with the flight control unit, and the flight control unit is used for controlling the unmanned aerial vehicle to fly; the photoelectric pod control unit is used for controlling the photoelectric pod to acquire and transmit data; the shooting control unit is used for controlling the shooting device to shoot.
8. The scouting and printing integrated remote control unmanned aerial vehicle system according to claim 7, wherein the ground end is provided with a voice communication unit for controlling a shouting device mounted on the unmanned aerial vehicle.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202223261994.1U CN218877605U (en) | 2022-12-05 | 2022-12-05 | Scouting and printing integrated remote control unmanned aerial vehicle and system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202223261994.1U CN218877605U (en) | 2022-12-05 | 2022-12-05 | Scouting and printing integrated remote control unmanned aerial vehicle and system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN218877605U true CN218877605U (en) | 2023-04-18 |
Family
ID=85951358
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202223261994.1U Active CN218877605U (en) | 2022-12-05 | 2022-12-05 | Scouting and printing integrated remote control unmanned aerial vehicle and system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN218877605U (en) |
-
2022
- 2022-12-05 CN CN202223261994.1U patent/CN218877605U/en active Active
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US7437985B2 (en) | Weapon launched reconnaissance system | |
| CN111981902B (en) | Multi-joint barrel shooting and patrolling missile, system and working method | |
| CN110631418B (en) | Unmanned aerial vehicle micro weapon system with intelligent observing and hitting integrated function | |
| CN207450216U (en) | A kind of load configuration structure of the dynamic unmanned plane of oil | |
| CN209870743U (en) | Integrated comprehensive avionics system for observing and shooting unmanned aerial vehicle | |
| CN218877605U (en) | Scouting and printing integrated remote control unmanned aerial vehicle and system | |
| CN112977824A (en) | Unmanned aerial vehicle system and method with detection and striking functions and convenient to carry by individual soldier | |
| CN108128456B (en) | Unmanned helicopter airborne fire-fighting nacelle | |
| CN104503458A (en) | Micro individual combat unmanned plane system | |
| CN209013838U (en) | A kind of 3D printing scout missile | |
| CN219277811U (en) | Can section of thick bamboo penetrate foldable unmanned aerial vehicle | |
| CN208216982U (en) | Equip with arms unmanned helicopter | |
| US20240239531A1 (en) | Compact and Lightweight Drone Delivery Device called an ArcSpear Electric Jet Drone System Having an Electric Ducted Air Propulsion System and Being Relatively Difficult to Track in Flight | |
| CN211506261U (en) | Swarm combat unmanned aerial vehicle cluster | |
| US11987403B2 (en) | Method for destroying the enemy's targets using missiles launched from multicopter drones carried inside soldiers' backpacks | |
| CN115465450A (en) | Gun-shot cluster type folding rotor micro unmanned aerial vehicle | |
| KR20110092753A (en) | Cannonball type observer | |
| CN218806669U (en) | Low-slow small target reconnaissance countercheck system based on multi-rotor unmanned aerial vehicle | |
| CN116142459A (en) | Integrated remote control unmanned aerial vehicle, system and method for scouting and beating | |
| CN108016618A (en) | A kind of ammunition emitter and system | |
| CN114889818A (en) | Blade type unmanned aerial vehicle system | |
| CN212099341U (en) | Foldable many rotors rescue unmanned aerial vehicle | |
| CN210882619U (en) | Fire control unmanned aerial vehicle | |
| CN109484611B (en) | Fuselage bearing structure of oil-driven unmanned aerial vehicle | |
| CN219277812U (en) | Can section of thick bamboo shoot horizontal folding unmanned aerial vehicle |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |