CN216128436U - Integrated triphibian unmanned aerial vehicle with flying wings - Google Patents
Integrated triphibian unmanned aerial vehicle with flying wings Download PDFInfo
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- CN216128436U CN216128436U CN202120377709.9U CN202120377709U CN216128436U CN 216128436 U CN216128436 U CN 216128436U CN 202120377709 U CN202120377709 U CN 202120377709U CN 216128436 U CN216128436 U CN 216128436U
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Abstract
The utility model discloses a flying wing integrated triphibian unmanned aerial vehicle, which comprises an unmanned aerial vehicle main body and wings arranged at the upper end of the unmanned aerial vehicle main body, and further comprises a rudder wing landing gear, an air cushion ups and downs device, amphibious driving frame wheels and frame wheel storage assemblies, wherein the rudder wing landing gear is arranged on two sides of the wings, the amphibious driving frame wheels are arranged on the lower end surface of the unmanned aerial vehicle main body, the frame wheel storage assemblies are arranged between the unmanned aerial vehicle main body and the amphibious driving frame wheels and are connected with the unmanned aerial vehicle main body, and the air cushion ups and downs device is arranged on the lower end surface of the unmanned aerial vehicle main body and is connected with the unmanned aerial vehicle main body; the integrated triphibian unmanned aerial vehicle with the flying wings can work in the air, underwater and on the water surface, the lifting rudder wings on the unmanned aerial vehicle body can be used as lifting rudders in the water and also can be used as wings for providing lifting force on the water surface, the amphibious paddle wheels can be used for multiple purposes, are used as driving wheels on the underwater ground and the land, and are used as power paddles in the water, so that the integrated triphibian unmanned aerial vehicle with the flying wings has wide application range, strong adaptability and high detection efficiency.
Description
Technical Field
The utility model relates to an underwater unmanned aerial vehicle, in particular to a flight-wing integrated triphibian unmanned aerial vehicle.
Background
In order to obtain more and better underwater information, various underwater unmanned detectors are developed in many countries in the world and are used for collecting underwater information and controlling the leading right of underwater information battles. The wheel type underwater unmanned detector can contact the underwater environment to the maximum extent, so that information such as submarine geomorphic characteristics, geological conditions, hydrology, magnetic fields, acoustic characteristics and the like can be well acquired, and therefore the wheel type underwater unmanned detector is widely concerned by navies of various countries. Meanwhile, the product is a dual-purpose product for military and civil use, and has wide application prospect in the fields of ocean development, underwater operation, underwater search and rescue and the like.
Traditional unmanned aerial vehicle under water generally only possesses the ability of submarine exploration and surface of water navigation, because unmanned aerial vehicle carries out information investigation in the field, need explore the surrounding environment from many sides, often need arrange aerial detector to use, increased the detection cost undoubtedly, also appear the condition of exposing easily during the investigation, adaptability is not good, needs improve.
SUMMERY OF THE UTILITY MODEL
The utility model aims to provide a flying-wing integrated triphibian unmanned aerial vehicle, which aims to solve the problems in the background technology.
In order to achieve the purpose, the utility model provides the following technical scheme:
a triphibian unmanned aerial vehicle with integrated flying wings comprises an unmanned aerial vehicle main body, wings arranged at the upper end of the unmanned aerial vehicle main body, a rudder wing landing gear, an air cushion sinking and floating device, amphibious driving frame wheels and frame wheel storage assemblies;
the rudder wing landing gear is arranged on two sides of the wing and used for pushing the unmanned aerial vehicle main body to rapidly lift under the water surface and adjusting the flying posture on the water surface;
the amphibious driving frame wheels are arranged on the lower end face of the unmanned aerial vehicle main body, are three groups in total, and are used for pushing the unmanned aerial vehicle main body to move forwards under the water surface and supporting the unmanned aerial vehicle main body to slide on the ground;
the frame wheel storage assembly is arranged between the main body of the unmanned aerial vehicle and the amphibious driving frame wheel, is connected with the main body of the unmanned aerial vehicle and the amphibious driving frame wheel, and is used for storing the amphibious driving frame wheel and controlling the steering of the amphibious driving frame wheel;
the air cushion ups and downs device arranges the lower terminal surface of unmanned aerial vehicle main part in and links up mutually with the unmanned aerial vehicle main part for it provides buoyancy to take off to slide for unmanned aerial vehicle main part surface of water.
Preferably, unmanned aerial vehicle main part upper end center department is equipped with intake duct one, and baffle and backplate before the entry and exit department at intake duct one both ends is equipped with respectively, and it is used for providing the built-in duct engine of power for unmanned aerial vehicle main part flight to install between baffle and the backplate before lieing in the intake duct one.
Preferably, the unmanned aerial vehicle main part and the wing are processed into a whole, and the joint of the unmanned aerial vehicle main part and the wing is in streamline connection into a curved surface.
Preferably, the rudder wing landing gear comprises rudder wings and lifting and diving power paddles, the rudder wings are arranged on two sides of the upper end of the unmanned aerial vehicle main body, one end of each rudder wing is connected with a rudder wing adjusting mechanism arranged in the unmanned aerial vehicle main body, the lifting and diving power paddles are arranged on two sides of the tail end of each wing, the end parts of the lifting and diving power paddles are provided with lifting and diving motors used for controlling the rotation of the lifting and diving motors, and waterproof coatings are arranged on the outer surfaces of the lifting and diving motors.
Preferably, the amphibious driving frame wheel comprises an amphibious slurry wheel, blades driven by a driving motor are arranged in the amphibious slurry wheel, and a waterproof coating is arranged on the outer surface of the driving motor.
Preferably, the frame wheel storage assembly comprises an electric telescopic rod and a paddle wheel built-in bin used for storing the electric telescopic rod and an amphibious driving frame wheel, the bottom end of the electric telescopic rod is connected with the paddle wheel on the water and the land, a three-axis steering engine reversing device is arranged at the joint of the electric telescopic rod and the paddle wheel on the water and the land, and the upper end of the electric telescopic rod is arranged in the paddle wheel built-in bin and matched with the paddle wheel built-in bin.
Preferably, the air cushion ups and downs device includes air cushion mount, air cushion and accomodates storehouse and air cushion, and unmanned aerial vehicle main part lower extreme both sides are arranged in to the air cushion mount, and its top rotates with the unmanned aerial vehicle main part to be connected, and its bottom is accomodate the storehouse up end fixed connection with the air cushion, and the air cushion is arranged in the air cushion and is accomodate the storehouse and be linked together with the vacuum pump that sets up in the air cushion and accomodate the storehouse, and the junction of air cushion and vacuum pump still is equipped with and releases the air control valve and aerifys check valve.
Preferably, aerify check valve include the second and fill the air flue of intake duct, fill the air flue and communicate with the second of intake duct, and the junction between them is equipped with the air inlet road mouth department, and air inlet road mouth department is equipped with the one-way sealed slider, and one end of one-way sealed slider is connected with the spring for restoring to the throne, and two one ends of intake duct are kept away from to the air flue are linked together with air pump output, and two one ends of keeping away from the air flue of intake duct are put the storehouse with the air cushion and are linked together.
Preferably, the unmanned aerial vehicle main part is equipped with the response detecting system that is used for reconnoitring the external environment, and the response detecting system is connected with the information processing module who sets up in the unmanned aerial vehicle main part, and information processing module is connected with the information storage module who sets up in the unmanned aerial vehicle main part, and information storage module is connected with the wireless transmission module who sets up in the unmanned aerial vehicle main part, and wireless transmission module is connected with the terminal receiving platform who sets up in the unmanned aerial vehicle main part.
Compared with the prior art, the utility model has the beneficial effects that: the integrated triphibian unmanned aerial vehicle with the flying wings can work in the air, under the water and on the water surface, the lifting rudder wings on the unmanned aerial vehicle body can be used as lifting rudders in the water and also can be used as wings for providing lifting force on the water surface, the amphibious paddle wheel can be used for multiple purposes, can be used as a driving wheel on the underwater ground and the land and used as a power paddle in the water, and has wide application range, strong adaptability and high detection efficiency;
the unmanned aerial vehicle bottom possess the inflatable cushion layer device that can receive and release, enable the quick switching working form of unmanned aerial vehicle, because the integrative triphibian unmanned aerial vehicle's of flying wing and fuselage fuse as an organic whole in addition, can effectively reduce the radar reflection wave, the investigation ability obtains further strengthening.
Drawings
Fig. 1 is a schematic structural diagram of a flight-wing integrated triphibian unmanned aerial vehicle.
Fig. 2 is a schematic structural diagram of a ducted engine built in a triphibian unmanned aerial vehicle with integrated flying wings.
Fig. 3 is a schematic structural diagram of an unmanned aerial vehicle main body in a flying wing integrated triphibian unmanned aerial vehicle.
Fig. 4 is a schematic structural diagram of a one-way sealing slide block of a flying wing integrated triphibian unmanned aerial vehicle.
In the figure: 1. a first air inlet channel; 2. an unmanned aerial vehicle main body; 3. a rudder wing; 4. an airfoil; 5. an air cushion fixing frame; 6. an air cushion; 7. a pulp wheel is internally provided with a bin; 8. an electric telescopic rod; 9. a three-axis steering engine reversing device; 10. land and water paddle wheels; 11. an air cushion storage bin; 12. lifting and submerging a motor; 13. a ducted engine is arranged inside; 14. lifting and submerging the power paste; 15. a paddle; 16. a drive motor; 17. a front baffle; 18. a tailgate; 19. a rudder wing adjusting mechanism; 20. a gas discharge control valve; 21. a second air inlet channel; 22. a spring; 23. an air charging passage; 24. a one-way sealing slide block; 25. an air inlet.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
Referring to fig. 1-4, in an embodiment of the present invention, a flight-wing integrated triphibian unmanned aerial vehicle includes an unmanned aerial vehicle main body 2, wings 4 disposed on an upper end of the unmanned aerial vehicle main body 2, a rudder wing landing gear, an air cushion levitation device, amphibious driving frame wheels, and frame wheel storage assemblies; the unmanned aerial vehicle main body 2 and the wings 4 are integrally processed, and the joint of the unmanned aerial vehicle main body 2 and the wings 4 is in streamline connection to form a curved surface; the joint of the unmanned aerial vehicle main body 2 and the wing 4 is connected into a rhombic surface at a certain angle or is connected into a curved surface in a streamline manner so as to reduce the reflection of radar waves;
an air inlet channel I1 is arranged at the center of the upper end of the unmanned aerial vehicle main body 2, a front baffle 17 and a rear baffle 18 are respectively arranged at the inlet and outlet at the two ends of the air inlet channel I1, and a built-in ducted engine 13 for providing power for the unmanned aerial vehicle main body 2 to fly is arranged in the air inlet channel I1 and located between the front baffle 17 and the rear baffle 18; the wing-flying integrated triphibian unmanned aerial vehicle is provided with a group of built-in ducted engines 13 for providing power for the flight of the unmanned aerial vehicle, the built-in ducted engines 13 are built in an air inlet passage I1 of an unmanned aerial vehicle main body 2, a front baffle 17 and a rear baffle 18 for water isolation are arranged at the front end and the rear end of the air inlet passage I1, when the unmanned aerial vehicle dives, the front baffle 17 and the rear baffle 18 are closed, and the front baffle 17 and the rear baffle 18 of the air inlet passage are opened during the flight in the air;
the rudder wing landing gear is arranged on two sides of the wing 4 and used for pushing the unmanned aerial vehicle main body 2 to rapidly lift under the water surface and adjusting the flying posture on the water surface; the rudder wing landing device comprises a rudder wing 3 and a lifting and submerging power propeller 14, the rudder wing 3 is arranged on two sides of the upper end of the unmanned aerial vehicle main body 2, one end of the rudder wing 3 is connected with a rudder wing adjusting mechanism 19 arranged in the unmanned aerial vehicle main body 2, the lifting and submerging power propeller 14 is arranged on two sides of the tail end of the wing 4, the end part of the lifting and submerging power propeller is provided with a lifting and submerging motor 12 for controlling the rotation of the lifting and submerging power propeller, and the outer surface of the lifting and submerging motor 12 is provided with a waterproof coating; the flying wing integrated triphibian unmanned aerial vehicle is provided with two groups of rudder wings 3, the rudder wings 3 are controlled by a rudder wing adjusting mechanism 19, when the unmanned aerial vehicle main body 2 ascends and descends in water, the unmanned aerial vehicle main body 2 mainly embodies an angle-adjustable elevator, the rapid ascending and descending of the unmanned aerial vehicle main body 2 in water are realized by matching with the ascending and descending power propeller 14, when the unmanned aerial vehicle main body 2 advances on the water surface, the unmanned aerial vehicle main body 2 is fixedly used as an auxiliary wing at a horizontal angle, and the flying posture of the unmanned aerial vehicle is mainly adjusted; the diving power propeller 14 is positively rotated to realize the diving of the main body 2 of the unmanned aerial vehicle, and is reversely rotated to realize the ascending of the main body 2 of the unmanned aerial vehicle;
the amphibious driving frame wheels are arranged on the lower end face of the unmanned aerial vehicle main body 2, are three in number, and are used for pushing the unmanned aerial vehicle main body 2 to move forwards under the water surface and supporting the unmanned aerial vehicle main body 2 to slide on the ground; the amphibious driving frame wheel comprises an amphibious paddle wheel 10, paddles 15 driven by a driving motor 16 are arranged in the amphibious paddle wheel 10, and a waterproof coating is arranged on the outer surface of the driving motor 16;
the frame wheel storage assembly is arranged between the unmanned aerial vehicle main body 2 and the amphibious driving frame wheel, is connected with the amphibious driving frame wheel and is used for storing the amphibious driving frame wheel and controlling the steering of the amphibious driving frame wheel; the frame wheel storage assembly comprises an electric telescopic rod 8 and a paddle wheel built-in bin 7 used for storing the electric telescopic rod 8 and an amphibious driving frame wheel, the bottom end of the electric telescopic rod 8 is connected with an amphibious paddle wheel 10, a three-axis steering engine reversing device 9 is arranged at the joint of the electric telescopic rod 8 and the amphibious paddle wheel 10, and the upper end of the electric telescopic rod 8 is arranged in the paddle wheel built-in bin 7 and matched with the paddle wheel built-in bin 7; the flying wing integrated triphibian unmanned aerial vehicle drives blades 15 in amphibious driving frame wheels to rotate through three driving motors 16 to provide power for underwater navigation, the blades 15 are made of carbon fiber materials, and an appearance fixing frame is made of composite materials, so that the weight can be reduced, the hardness requirement can be met, and the three unmanned aerial vehicles can be used for performing multi-dimensional turning direction through a three-axis steering engine reversing device 9 and performing different functions; in addition, the amphibious driving frame wheel can be collected into the paddle wheel built-in bin 7 during flying in the air, and is used for reducing the flying resistance;
the air cushion sinking and floating device is arranged on the lower end face of the unmanned aerial vehicle main body 2, is connected with the unmanned aerial vehicle main body 2 and is used for providing buoyancy for the water surface gliding takeoff of the unmanned aerial vehicle main body 2; the air cushion sinking and floating device comprises an air cushion fixing frame 5, an air cushion accommodating bin 11 and an air cushion 6, wherein the air cushion fixing frame 5 is arranged on two sides of the lower end of the unmanned aerial vehicle main body 2, the top end of the air cushion fixing frame is rotatably connected with the unmanned aerial vehicle main body 2, the bottom end of the air cushion fixing frame is fixedly connected with the upper end face of the air cushion accommodating bin 11, the air cushion 6 is arranged in the air cushion accommodating bin 11 and is communicated with a vacuum pump arranged in the air cushion accommodating bin 11, and a gas release control valve 20 and an inflation one-way valve are further arranged at the connection part of the air cushion 6 and the vacuum pump;
the inflation one-way valve comprises an air inlet channel II 21 and an air inflation channel 23, the air inflation channel 23 is communicated with the air inlet channel II 21, an air inlet channel opening 25 is arranged at the joint of the air inlet channel II 21 and the air inflation channel II, a one-way sealing slide block 24 is arranged at the air inlet channel opening 25, one end of the one-way sealing slide block 24 is connected with a return spring 22, one end, far away from the air inlet channel II 21, of the air inflation channel 23 is communicated with the output end of the air pump piece, and one end, far away from the air inflation channel 23, of the air inlet channel II 21 is communicated with the air cushion storage bin 11; the flying wing integrated triphibian unmanned aerial vehicle is provided with two air cushion sinking and floating devices capable of charging and discharging air, an air charging one-way valve in an air cushion storage bin 11 is opened through controlling a steering engine to charge air, buoyancy is provided for the unmanned aerial vehicle to slide on the water surface to take off, after the unmanned aerial vehicle takes off stably, the air cushion sinking and floating devices are discharged through controlling an air discharging control valve 20, a vacuum pump built in an unmanned aerial vehicle body is started to exhaust air, the interior of the air cushion storage bin 11 is in a vacuum state, and a negative pressure recovery air cushion 6 is formed;
an induction detection system for detecting an external environment is mounted on the unmanned aerial vehicle main body 2, the induction detection system is connected with an information processing module arranged in the unmanned aerial vehicle main body 2, the information processing module is connected with an information storage module arranged in the unmanned aerial vehicle main body 2, the information storage module is connected with a wireless transmission module arranged in the unmanned aerial vehicle main body 2, and the wireless transmission module is connected with a terminal receiving platform arranged in the unmanned aerial vehicle main body 2; the information surveyed and mapped by the induction detection system is stored in the information storage module through the information processing module, and the information storage module transmits the information to the terminal receiving platform through the wireless transmission module; the induction detection system comprises a navigation device, a detector, a gyroscope, a microwave obstacle avoidance radar and a photoelectric sensor.
The working principle is as follows: the flying wing integrated triphibian unmanned aerial vehicle realizes the submergence and the ascent of the unmanned aerial vehicle and the advancing in water by controlling an amphibious driving frame wheel and a rudder wing landing gear; the built-in ducted engine 13 and the front baffle 17 and the rear baffle 18 at the inlet and the outlet of the air inlet channel I1 are controlled to be closed, the steering engine is controlled to open the inflating one-way valve in the air cushion storage bin 11 to inflate, buoyancy is provided for the spring 22 to enable the spring 22 to slide on the air cushion storage bin to take off, during detection, information detected and measured by the induction detection system is stored in the information storage module through the information processing module, the information storage module transmits information to the terminal receiving platform through the wireless transmission module, different working purposes are achieved by hanging different function modules, and the built-in ducted engine has different special function diversity and great expansibility.
It will be evident to those skilled in the art that the utility model is not limited to the details of the foregoing illustrative embodiments, and that the present invention may be embodied in other specific forms without departing from the spirit or essential attributes thereof. The present embodiments are therefore to be considered in all respects as illustrative and not restrictive, the scope of the utility model being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein. Any reference sign in a claim should not be construed as limiting the claim concerned.
Furthermore, it should be understood that although the present description refers to embodiments, not every embodiment may contain only a single embodiment, and such description is for clarity only, and those skilled in the art should integrate the description, and the embodiments may be combined as appropriate to form other embodiments understood by those skilled in the art.
Claims (9)
1. A triphibian unmanned aerial vehicle integrating flying wings comprises an unmanned aerial vehicle main body (2) and wings (4) arranged at the upper end of the unmanned aerial vehicle main body (2), and is characterized by further comprising a rudder wing landing gear, an air cushion sinking and floating device, amphibious driving frame wheels and frame wheel storage assemblies;
the rudder wing landing gear is arranged on two sides of the wing (4) and used for pushing the unmanned aerial vehicle main body (2) to rapidly lift under the water surface and adjusting the flight attitude on the water surface;
the amphibious driving frame wheels are arranged on the lower end face of the unmanned aerial vehicle main body (2) and are divided into three groups, and the amphibious driving frame wheels are used for pushing the unmanned aerial vehicle main body (2) to move forwards under the water surface and supporting the unmanned aerial vehicle main body (2) to slide on the ground;
the frame wheel storage assembly is arranged between the unmanned aerial vehicle main body (2) and the amphibious driving frame wheel, is connected with the amphibious driving frame wheel and is used for storing the amphibious driving frame wheel and controlling the steering of the amphibious driving frame wheel;
the air cushion sinking and floating device is arranged on the lower end face of the unmanned aerial vehicle main body (2), is connected with the unmanned aerial vehicle main body (2) and is used for providing buoyancy for the water surface of the unmanned aerial vehicle main body (2) to slide and take off.
2. The flying wing integrated triphibian unmanned aerial vehicle as claimed in claim 1, wherein an air inlet duct (1) is arranged at the center of the upper end of the unmanned aerial vehicle main body (2), a front baffle (17) and a rear baffle (18) are respectively arranged at the inlet and outlet at the two ends of the air inlet duct (1), and a built-in ducted engine (13) for providing power for the unmanned aerial vehicle main body (2) to fly is installed in the air inlet duct (1) and between the front baffle (17) and the rear baffle (18).
3. The flying wing integrated triphibian unmanned aerial vehicle according to claim 1, wherein the unmanned aerial vehicle main body (2) and the wings (4) are integrally machined, and the joint of the unmanned aerial vehicle main body (2) and the wings (4) is formed by streamline connection into a curved surface.
4. The all-in-one triphibian with flying wings as claimed in claim 1, wherein the rudder wing landing gear comprises a rudder wing (3) and a lifting and submerging power paddle (14), the rudder wing (3) is placed on two sides of the upper end of the main body (2) of the unmanned plane, one end of the rudder wing landing gear is connected with a rudder wing adjusting mechanism (19) arranged in the main body (2) of the unmanned plane, the lifting and submerging power paddle (14) is placed on two sides of the tail end of the wing (4), the end of the lifting and submerging power paddle is provided with a lifting and submerging motor (12) for controlling the rotation of the lifting and submerging motor, and the outer surface of the lifting and submerging motor (12) is provided with a waterproof coating.
5. The flying wing integrated triphibian unmanned aerial vehicle of claim 1, wherein the amphibious driving frame wheel comprises an amphibious propeller wheel (10), blades (15) driven by a driving motor (16) are arranged in the amphibious propeller wheel (10), and the outer surface of the driving motor (16) is provided with a waterproof coating.
6. The all-in-one flying-wing triphibian unmanned aerial vehicle as claimed in claim 4, wherein the frame wheel storage assembly comprises an electric telescopic rod (8) and a paddle wheel built-in bin (7) for storing the electric telescopic rod (8) and amphibious driving frame wheels, the bottom end of the electric telescopic rod (8) is connected with the amphibious paddle wheels (10), a three-axis steering engine reversing device (9) is arranged at the joint of the electric telescopic rod (8) and the amphibious paddle wheels (10), and the upper end of the electric telescopic rod (8) is arranged in the paddle wheel built-in bin (7) and matched with the paddle wheel built-in bin (7).
7. The all-in-one triphibian flying wing unmanned aerial vehicle of claim 1, wherein the air cushion submerging and surfacing device comprises an air cushion fixing frame (5), an air cushion storage bin (11) and an air cushion (6), the air cushion fixing frame (5) is arranged on two sides of the lower end of the unmanned aerial vehicle main body (2), the top end of the air cushion fixing frame is rotatably connected with the unmanned aerial vehicle main body (2), the bottom end of the air cushion fixing frame is fixedly connected with the upper end face of the air cushion storage bin (11), the air cushion (6) is arranged in the air cushion storage bin (11) and is communicated with a vacuum pump arranged in the air cushion storage bin (11), and a relief control valve (20) and an inflation one-way valve are further arranged at the joint of the air cushion (6) and the vacuum pump.
8. The unmanned aerial vehicle of claim 7, an integrative triphibian of all-wing aircraft, characterized in that aerify check valve include intake duct two (21) and aerify way (23), it is linked together with intake duct two (21) to aerify way (23), and the junction between them is equipped with inlet port mouth (25), inlet port mouth (25) department is equipped with one-way sealed slider (24), one-way sealed slider (24) one end is connected with and resets and uses spring (22), it is linked together with air pump spare output to aerify two (21) one end of intake duct to keep away from in air duct (23), intake duct two (21) are kept away from and are aerifyd duct (23) one end and are put storehouse (11) with the air cushion and are linked together.
9. The flying wing integrated triphibian unmanned aerial vehicle as claimed in claim 1, wherein the main body (2) of the unmanned aerial vehicle is provided with an inductive detection system for detecting the external environment, the inductive detection system is connected with an information processing module arranged in the main body (2) of the unmanned aerial vehicle, the information processing module is connected with an information storage module arranged in the main body (2) of the unmanned aerial vehicle, the information storage module is connected with a wireless transmission module arranged in the main body (2) of the unmanned aerial vehicle, and the wireless transmission module is connected with a terminal receiving platform arranged in the main body (2) of the unmanned aerial vehicle.
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| Application Number | Priority Date | Filing Date | Title |
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| CN202120377709.9U CN216128436U (en) | 2021-02-18 | 2021-02-18 | Integrated triphibian unmanned aerial vehicle with flying wings |
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| CN202120377709.9U CN216128436U (en) | 2021-02-18 | 2021-02-18 | Integrated triphibian unmanned aerial vehicle with flying wings |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114771832A (en) * | 2022-05-31 | 2022-07-22 | 浙江大学 | Self-powered cross-medium unmanned aerial vehicle for operation and maintenance of offshore wind turbine |
| CN116256763A (en) * | 2023-05-10 | 2023-06-13 | 武汉理工大学 | Bridge disease detection device and detection method |
-
2021
- 2021-02-18 CN CN202120377709.9U patent/CN216128436U/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114771832A (en) * | 2022-05-31 | 2022-07-22 | 浙江大学 | Self-powered cross-medium unmanned aerial vehicle for operation and maintenance of offshore wind turbine |
| CN116256763A (en) * | 2023-05-10 | 2023-06-13 | 武汉理工大学 | Bridge disease detection device and detection method |
| CN116256763B (en) * | 2023-05-10 | 2023-08-15 | 武汉理工大学 | Bridge disease detection device and detection method |
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