CN113815855A - Examine and beat integrative unmanned aerial vehicle - Google Patents
Examine and beat integrative unmanned aerial vehicle Download PDFInfo
- Publication number
- CN113815855A CN113815855A CN202111151566.0A CN202111151566A CN113815855A CN 113815855 A CN113815855 A CN 113815855A CN 202111151566 A CN202111151566 A CN 202111151566A CN 113815855 A CN113815855 A CN 113815855A
- Authority
- CN
- China
- Prior art keywords
- unmanned aerial
- aerial vehicle
- vehicle body
- sleeve
- bent
- 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.)
- Pending
Links
- 230000005540 biological transmission Effects 0.000 claims description 17
- 230000006835 compression Effects 0.000 claims description 5
- 238000007906 compression Methods 0.000 claims description 5
- 238000011835 investigation Methods 0.000 claims description 3
- 238000000034 method Methods 0.000 claims 1
- 230000000694 effects Effects 0.000 description 3
- 230000035939 shock Effects 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
- 238000009529 body temperature measurement Methods 0.000 description 2
- 230000003139 buffering effect Effects 0.000 description 2
- 238000006243 chemical reaction Methods 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 230000010354 integration Effects 0.000 description 2
- 238000010521 absorption reaction Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000013016 damping Methods 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 230000013011 mating Effects 0.000 description 1
- 239000011159 matrix material Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000003287 optical effect Effects 0.000 description 1
- 238000005096 rolling process Methods 0.000 description 1
- 230000001502 supplementing effect Effects 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/22—Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/58—Arrangements or adaptations of shock-absorbers or springs
- B64C25/62—Spring shock-absorbers; Springs
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
-
- 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
- B64D47/00—Equipment not otherwise provided for
- B64D47/08—Arrangements of cameras
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Closed-Circuit Television Systems (AREA)
Abstract
The invention relates to the field of unmanned aerial vehicle equipment, in particular to a scouting and batting integrated unmanned aerial vehicle, which comprises: the unmanned aerial vehicle comprises an unmanned aerial vehicle body, wherein a main wing is fixedly installed at the upper end of the unmanned aerial vehicle body through a bolt, and two ailerons are arranged at the rear end of the unmanned aerial vehicle body; the two ailerons and the main wing cooperate to form a triangular section; the tail end of the unmanned aerial vehicle body is provided with three blades, and an included angle formed between every two adjacent blades is 120 degrees; the unmanned aerial vehicle comprises an unmanned aerial vehicle body, and is characterized in that a motor and a battery are arranged in the unmanned aerial vehicle body, a pan-tilt camera and an airspeed tube are arranged at the front end of the unmanned aerial vehicle body, a support assembly is installed at the lower end of the front side of the unmanned aerial vehicle body, and a lifting assembly is arranged at the lower end of the rear side of the unmanned aerial vehicle body; observe and beat integrative unmanned aerial vehicle and form triangle-shaped at whole unmanned aerial vehicle body lower extreme through the subassembly that rises and falls that sets up and supporting component cooperation, triangle-shaped possesses stability, consequently observe and beat integrative unmanned aerial vehicle and place and take off when slideing and all possess better stability.
Description
Technical Field
The invention relates to the field of unmanned aerial vehicle equipment, in particular to a scouting and batting integrated unmanned aerial vehicle.
Background
Unmanned aircraft, commonly known as: unmanned aircraft, unmanned aerial vehicles, unmanned combat aircraft, and bee-type machines; the airplane is a wide range of remote control aircrafts without the need of a pilot to board and pilot, and is generally in particular to an unmanned reconnaissance airplane of the military.
The scouting and batting unmanned aerial vehicle is improved on the basis of the scouting unmanned aerial vehicle, and the scouting unmanned aerial vehicle has multiple functions of scouting, batting and the like, so that the use range is wider and the application frequency is higher; and the high-frequency application of the unmanned aerial vehicle is also used for providing higher requirements for the undercarriage when the unmanned aerial vehicle goes up and down.
Aiming at the problems in the background technology, the invention aims to provide a scouting and printing integrated unmanned aerial vehicle.
Disclosure of Invention
The invention aims to provide a scouting and batting integrated unmanned aerial vehicle to solve the problems in the background technology.
In order to achieve the purpose, the invention provides the following technical scheme:
an investigation and play integrated unmanned aerial vehicle, the investigation and play integrated unmanned aerial vehicle includes:
the unmanned aerial vehicle comprises an unmanned aerial vehicle body, wherein a main wing is fixedly installed at the upper end of the unmanned aerial vehicle body through bolts, two ailerons are arranged at the rear end of the unmanned aerial vehicle body, and the two ailerons are fixedly installed on the unmanned aerial vehicle body through the cooperation of a second connecting rod and a first connecting rod; the two ailerons and the main wing cooperate to form a triangular section;
the tail end of the unmanned aerial vehicle body is provided with three blades, and an included angle formed between every two adjacent blades is 120 degrees; the unmanned aerial vehicle body is internally provided with a motor and batteries, the number of the batteries is two, and the two batteries are one;
the front end of the unmanned aerial vehicle body is provided with a pan-tilt camera and an airspeed head, and the upper end of the unmanned aerial vehicle body is also fixedly provided with a signal rod;
supporting component is installed to unmanned aerial vehicle body front side lower extreme, and unmanned aerial vehicle body rear side lower extreme is equipped with the subassembly that rises and falls.
As a further scheme of the invention: the unmanned aerial vehicle body still matches and is equipped with picture biography system and wireless transmission system.
As a further scheme of the invention: the support assembly comprises a sleeve, a sleeve rod and a shaft seal, the upper end of the sleeve is connected with the unmanned aerial vehicle body, the lower end of the sleeve is movably mounted on the sleeve rod, the shaft seal is arranged at the lower end of the sleeve rod, and a compression spring is mounted on the part, between the sleeve and the shaft seal, of the sleeve rod; the shaft seal is movably provided with a rotating shaft inside, and rollers are arranged on two sides of the rotating shaft.
As a further scheme of the invention: the lifting assembly comprises a mounting plate, bent pipes and bent rods, the upper end of the mounting plate is fixedly mounted at the lower end of the unmanned aerial vehicle body through bolts, the bent pipes are arranged on the left side and the right side of the lower end of the mounting plate, the bent rods are movably mounted at the lower ends of the bent pipes, a mounting frame is arranged at the lower end of each bent rod, and a travelling wheel is mounted at one end of the mounting frame; the part of the bent rod between the bent pipe and the mounting frame is provided with a buffer spring.
Compared with the prior art, the invention has the beneficial effects that:
the reconnaissance and play integrated unmanned aerial vehicle forms a triangular section through the matching action of the two set ailerons and the main wing; the arranged main wing is used for improving the lift force required by the scouting and batting integrated unmanned aerial vehicle during takeoff, and the installed auxiliary wing is used for helping to balance the stability of the scouting and batting integrated unmanned aerial vehicle during flying and facilitating the control of the scouting and batting integrated unmanned aerial vehicle to deflect in direction;
in addition, the arranged pan-tilt camera supports wide-angle zooming real-time switching, supports target intelligent following and can identify video target real-time tracking; the system is provided with a picture transmission system and a wireless transmission system in a matching way, the picture transmission system supports the integrated wireless transmission system and can transmit the video and flight control data of the unmanned aerial vehicle to the ground control station, the wireless transmission system is provided with various video input and output interfaces, the integration level is high, the transmission delay is low, and the diversified mounting requirements of the unmanned aerial vehicle can be met;
more importantly, the lifting assembly and the supporting assembly are matched to act on the lower end of the whole unmanned aerial vehicle body to form a triangle, and the triangle has stability, so that the unmanned aerial vehicle has good stability when placed and takes off and slides; and the lifting assembly and the supporting assembly have better buffering and damping effects.
Drawings
In order to more clearly illustrate the technical solutions in the embodiments of the present invention, the drawings used in the description of the embodiments or the prior art will be briefly described below, and it is obvious that the drawings in the following description are only some embodiments of the present invention.
Fig. 1 is a front view of a scouting and batting integrated unmanned aerial vehicle according to an embodiment of the present invention.
Fig. 2 is a schematic structural view of an integrated unmanned aerial vehicle for surveying and batting according to an embodiment of the present invention.
Fig. 3 is a schematic structural view of a support assembly of the inspection and printing integrated unmanned aerial vehicle according to the embodiment of the invention.
Fig. 4 is a schematic structural view of a landing gear assembly of a scouting and batting integrated unmanned aerial vehicle according to an embodiment of the present invention.
In the figure: the unmanned aerial vehicle comprises a main wing 1, a aileron 2, a bolt 3, a signal rod 4, a first connecting rod 5, a blade 6, an unmanned aerial vehicle body 7, an airspeed head 8, a pan-tilt camera 9, a landing assembly 10, a support assembly 11, a second connecting rod 12, a sleeve 13, a compression spring 14, a sleeve rod 15, a roller 16, a rotating shaft 17, a shaft seal 18, a mounting plate 19, a bent pipe 20, a buffer spring 21, a bent rod 22, a mounting frame 23 and a road wheel 24.
Detailed Description
In order to make the technical problems, technical solutions and advantageous effects to be solved by the present invention more clearly apparent, the present invention is further described in detail below with reference to the accompanying drawings and embodiments. It should be understood that the specific embodiments described herein are merely illustrative of the invention and are not intended to limit the invention.
Examples
Referring to fig. 1 and fig. 2, in an embodiment of the present invention, an all-in-one drone, includes:
the unmanned aerial vehicle comprises an unmanned aerial vehicle body 7, wherein a main wing 1 is fixedly installed at the upper end of the unmanned aerial vehicle body 7 through a bolt 3, two ailerons 2 are arranged at the rear end of the unmanned aerial vehicle body 7, and the two ailerons 2 are fixedly installed on the unmanned aerial vehicle body 7 through the cooperation of a second connecting rod 12 and a first connecting rod 5; the two ailerons 2 and the main wing 1 cooperate to form a triangular section; the main wing 1 is used for improving the lift force required by the scouting and batting integrated unmanned aerial vehicle during takeoff, and the auxiliary wing 2 is used for balancing the stability of the scouting and batting integrated unmanned aerial vehicle during flying and facilitating the control of the scouting and batting integrated unmanned aerial vehicle for direction deflection;
the tail end of the unmanned aerial vehicle body 7 is provided with three blades 6, and an included angle formed between every two adjacent blades 6 is 120 degrees; the unmanned aerial vehicle body 7 is internally provided with a motor and batteries, the number of the batteries is two, two batteries are one, the maximum endurance time of the batteries is 55 minutes, and the unmanned aerial vehicle has a heating function; the battery provides electric energy for the operation of the motor, and the motor provides kinetic energy required by the rotation of the paddle 6;
the front end of the unmanned aerial vehicle body 7 is provided with a pan-tilt camera 9 and an airspeed tube 8, and the pan-tilt camera 9 supports wide-angle zooming real-time switching and supports target intelligent following; the holder camera 9 is a 2000W pixel 30-time hybrid optical zoom lens, a 1200W wide-angle lens, a high-definition infrared light supplementing lens and a laser ranging radar all-in-one holder, and can support point temperature measurement and area temperature measurement; supporting pointing zooming and ultra-clear matrix photographing; in addition, the pan-tilt camera 9 can tilt: +30 ° to-120 °; translation: 360 DEG, rolling: -40 ° to +40 °; maximum control speed pitching: 120 °/s, translation: 180 DEG/s; the real-time tracking of the video target can be identified, and the video image can be stored to a TF card with the capacity less than or equal to 256G; the set HDMI and the network port output one-key switching, and the SBUS signal control and the serial port control one-key switching; the signal rod 4 is fixedly arranged at the upper end of the unmanned aerial vehicle body 7, and the signal rod 4 is used for receiving and transmitting wireless signals, so that an operator can conveniently perform remote control on the scouting and hitting integrated unmanned aerial vehicle; the mounted airspeed head 8 is used for detecting the flying speed of the reconnaissance and batting integrated unmanned aerial vehicle in real time;
supporting component 11 is installed to 7 front side lower extremes of unmanned aerial vehicle body, and 7 rear side lower extremes of unmanned aerial vehicle body are equipped with the subassembly 10 that rises and falls, and the supporting component 11 and the subassembly 10 cooperation that rises and falls of setting are triangular distribution at 7 lower extremes of unmanned aerial vehicle body, are used for right it plays support and shock attenuation when launching to check and play integrative unmanned aerial vehicle.
Furthermore, the unmanned aerial vehicle body 7 is also provided with a graph transmission system and a wireless transmission system in a matching manner, the graph transmission system supports the integrated wireless transmission system to transmit the video and flight control data of the unmanned aerial vehicle to the ground control station, and simultaneously supports the transmission of control information of the ground station and the remote controller to the unmanned aerial vehicle, so that the requirement of simultaneous transmission of the video and control instructions in application scenes such as unmanned aerial vehicles and robots can be met; the wireless transmission system has various video input and output interfaces, is high in integration level and low in transmission delay, and can meet the diversified mounting requirements of the unmanned aerial vehicle; in addition, the working frequency range of the graph transmission system can be configured to be 7-15 km in an effective range of 800M.
Referring to fig. 3, further, the support assembly 11 includes a sleeve 13, a sleeve rod 15 and a shaft seal 18, the upper end of the sleeve 13 is connected to the unmanned aerial vehicle body 7, the lower end of the sleeve 13 is movably mounted on the sleeve rod 15, the lower end of the sleeve rod 15 is provided with the shaft seal 18, and a compression spring 14 is mounted on a portion of the sleeve rod 15 between the sleeve 13 and the shaft seal 18; a rotating shaft 17 is movably arranged in the shaft seal 18, and rollers 16 are arranged on two sides of the rotating shaft 17;
when observing and beat required power when integrative unmanned aerial vehicle provides flight through pivoted paddle 6, the gyro wheel 16 of setting rolls the displacement subaerial, and the sleeve pipe 13 of setting is then movable mounting on loop bar 15, and the 14 deformation of compression spring who sets up on the loop bar 15 produces elasticity reaction and gives sleeve pipe 13, is used for right observe and beat and play the buffering shock attenuation when integrative unmanned aerial vehicle takes off and descends.
Referring to fig. 4, further, the landing assembly 10 includes a mounting plate 19, elbows 20 and bent rods 22, the upper end of the mounting plate 19 is fixed to the lower end of the unmanned aerial vehicle body 7 through bolts, the elbows 20 are arranged on the left and right sides of the lower end of the mounting plate 19, the bent rods 22 are movably mounted on the lower ends of the elbows 20, a mounting frame 23 is arranged on the lower end of each bent rod 22, and a traveling wheel 24 is mounted on one end of each mounting frame 23; the part of the bent rod 22 between the bent pipe 20 and the mounting frame 23 is provided with a buffer spring 21;
when the scouting and batting integrated unmanned aerial vehicle takes off and lands through the arranged landing assembly 10, the arranged travelling wheel 24 rolls and displaces on the ground during taking off; when the landing device is in landing, the lower end of the arranged bent pipe 20 is movably arranged on the bent rod 22, and the buffer spring 21 deforms to generate elastic force, so that the whole landing assembly 10 has a buffer and shock absorption effect; in addition, the subassembly 10 and the supporting component 11 mating reaction that rises and falls of setting form triangle-shaped at whole unmanned aerial vehicle body 7 lower extreme, and triangle-shaped possesses stability, consequently is in it places and takes off and slide to see and play integrative unmanned aerial vehicle and possess better stability when possessing.
In the description of the present invention, unless otherwise expressly specified or limited, the terms "mounted," "connected," and "connected" are to be construed broadly, e.g., as meaning a fixed connection, a removable connection, or an integral connection; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meanings of the above terms in the present invention can be understood in specific cases to those skilled in the art.
The above description is only for the purpose of illustrating the preferred embodiments of the present invention and is not to be construed as limiting the invention, and any modifications, equivalents and improvements made within the spirit and principle of the present invention are intended to be included within the scope of the present invention.
Claims (4)
1. An investigation and combat integrated unmanned aerial vehicle, comprising: an unmanned aerial vehicle body (7); the method is characterized in that:
the main wing (1) is fixedly installed at the upper end of the unmanned aerial vehicle body (7) through a bolt (3), the two ailerons (2) are arranged at the rear end of the unmanned aerial vehicle body (7), and the two ailerons (2) are fixedly installed on the unmanned aerial vehicle body (7) through the cooperation of a second connecting rod (12) and a first connecting rod (5); the two ailerons (2) and the main wing (1) are matched to form a triangular section;
the unmanned aerial vehicle is characterized in that the tail end of the unmanned aerial vehicle body (7) is provided with three blades (6), and an included angle formed between every two adjacent blades (6) is 120 degrees; the unmanned aerial vehicle body (7) is internally provided with motors and batteries, the number of the batteries is two, and the two batteries are one; a pan-tilt camera (9) and an airspeed head (8) are arranged at the front end of the unmanned aerial vehicle body (7), and a signal rod (4) is fixedly installed at the upper end of the unmanned aerial vehicle body (7);
supporting component (11) are installed to unmanned aerial vehicle body (7) front side lower extreme, and unmanned aerial vehicle body (7) rear side lower extreme is equipped with subassembly (10) that rises and falls.
2. The scout and punch integrated unmanned aerial vehicle of claim 1, wherein: unmanned aerial vehicle body (7) still match and are equipped with picture biography system and wireless transmission system.
3. The scout and punch integrated unmanned aerial vehicle of claim 1, wherein: the unmanned aerial vehicle is characterized in that the supporting assembly (11) comprises a sleeve (13), a sleeve rod (15) and a shaft seal (18), the upper end of the sleeve (13) is connected with the unmanned aerial vehicle body (7), the lower end of the sleeve (13) is movably mounted on the sleeve rod (15), the shaft seal (18) is arranged at the lower end of the sleeve rod (15), and a compression spring (14) is mounted on the part, between the sleeve (13) and the shaft seal (18), of the sleeve rod (15); a rotating shaft (17) is movably mounted in the shaft seal (18), and rollers (16) are arranged on two sides of the rotating shaft (17).
4. The scout and punch integrated unmanned aerial vehicle of claim 1, wherein: the lifting assembly (10) comprises a mounting plate (19), bent pipes (20) and bent rods (22), the upper end of the mounting plate (19) is fixedly mounted at the lower end of the unmanned aerial vehicle body (7) through bolts, the bent pipes (20) are arranged on the left side and the right side of the lower end of the mounting plate (19), the bent rods (22) are movably mounted at the lower end of the bent pipes (20), a mounting frame (23) is arranged at the lower end of the bent rods (22), and travelling wheels (24) are mounted at one end of the mounting frame (23); the part of the bent rod (22) between the bent pipe (20) and the mounting frame (23) is provided with a buffer spring (21).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202111151566.0A CN113815855A (en) | 2021-09-29 | 2021-09-29 | Examine and beat integrative unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202111151566.0A CN113815855A (en) | 2021-09-29 | 2021-09-29 | Examine and beat integrative unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN113815855A true CN113815855A (en) | 2021-12-21 |
Family
ID=78921533
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202111151566.0A Pending CN113815855A (en) | 2021-09-29 | 2021-09-29 | Examine and beat integrative unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN113815855A (en) |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN208559744U (en) * | 2018-04-16 | 2019-03-01 | 江西中轻智能设备有限公司 | A kind of environmental monitoring unmanned plane undercarriage |
| CN109808913A (en) * | 2019-01-29 | 2019-05-28 | 西北工业大学 | A kind of unmanned aerial vehicle design method with deflectable winglet |
| CN112849412A (en) * | 2021-02-08 | 2021-05-28 | 陕西北斗金箭航空科技有限公司 | Hydrogen-electricity nacelle body integrated scouting and batting unmanned aerial vehicle |
| CN113120231A (en) * | 2021-06-01 | 2021-07-16 | 合肥工业大学 | Fixed wing forest fire control scouting hits unmanned aerial vehicle |
| CN216581001U (en) * | 2021-09-29 | 2022-05-24 | 安徽徽光智能科技有限责任公司 | Scouting and beating integrated unmanned aerial vehicle |
-
2021
- 2021-09-29 CN CN202111151566.0A patent/CN113815855A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN208559744U (en) * | 2018-04-16 | 2019-03-01 | 江西中轻智能设备有限公司 | A kind of environmental monitoring unmanned plane undercarriage |
| CN109808913A (en) * | 2019-01-29 | 2019-05-28 | 西北工业大学 | A kind of unmanned aerial vehicle design method with deflectable winglet |
| CN112849412A (en) * | 2021-02-08 | 2021-05-28 | 陕西北斗金箭航空科技有限公司 | Hydrogen-electricity nacelle body integrated scouting and batting unmanned aerial vehicle |
| CN113120231A (en) * | 2021-06-01 | 2021-07-16 | 合肥工业大学 | Fixed wing forest fire control scouting hits unmanned aerial vehicle |
| CN216581001U (en) * | 2021-09-29 | 2022-05-24 | 安徽徽光智能科技有限责任公司 | Scouting and beating integrated unmanned aerial vehicle |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| WO2021022727A1 (en) | Air-ground amphibious unmanned driving platform | |
| CN216581001U (en) | Scouting and beating integrated unmanned aerial vehicle | |
| RU183717U1 (en) | Multirotor unmanned aerial vehicle | |
| CN107187588B (en) | A kind of Intelligent unattended machine with safety and shock-absorption function | |
| CN103350624B (en) | Propelling type flying car with spiral wings | |
| CN112902759A (en) | Anti-unmanned aerial vehicle system | |
| CN113371182A (en) | Barrel-type transmitted reconnaissance attack rotor unmanned aerial vehicle | |
| CN113815855A (en) | Examine and beat integrative unmanned aerial vehicle | |
| CN104503458A (en) | Micro individual combat unmanned plane system | |
| CN110626500A (en) | Unmanned aerial vehicle | |
| CN103803057B (en) | Row's wing sun power UAV aerodynamic layout structure | |
| CN218806669U (en) | Low-slow small target reconnaissance countercheck system based on multi-rotor unmanned aerial vehicle | |
| CN109823535B (en) | All-terrain mechanical winged insect for reconnaissance and working method thereof | |
| CN115840459B (en) | Monocular vision obstacle avoidance system for ornithopter | |
| CN218400970U (en) | Self-destruction type attack unmanned aerial vehicle | |
| CN217996685U (en) | Six-degree-of-freedom self-locking manually-adjusted unmanned aerial vehicle engine installation vehicle | |
| CN107054638A (en) | A kind of underneath type coaxial double-rotary wing unmanned plane | |
| CN116039985A (en) | High-compactness single-shot unmanned tilt gyroplane transmission system and unmanned aerial vehicle | |
| CN114987777A (en) | Low-slow small target reconnaissance and countercheck system and method based on multi-rotor unmanned aerial vehicle | |
| CN214084763U (en) | Investigation and attack integrated flying patrol device | |
| CN105480428A (en) | Recovery protection type uniaxial tripod head driven by steering engine | |
| CN206311912U (en) | Artillery shooting effect based on movable unmanned helicopter scouts correction system | |
| CN210526870U (en) | Aiming system and unmanned aerial vehicle | |
| CN113859538A (en) | High-speed electric power inspection combined type coaxial unmanned helicopter | |
| CN112902758A (en) | Anti-unmanned aerial vehicle flight platform |
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 |