CN111703575B - Multifunctional unmanned aerial vehicle - Google Patents
Multifunctional unmanned aerial vehicle Download PDFInfo
- Publication number
- CN111703575B CN111703575B CN202010609860.0A CN202010609860A CN111703575B CN 111703575 B CN111703575 B CN 111703575B CN 202010609860 A CN202010609860 A CN 202010609860A CN 111703575 B CN111703575 B CN 111703575B
- Authority
- CN
- China
- Prior art keywords
- unmanned aerial
- aerial vehicle
- bearing
- column
- motor
- 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
-
- 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
- B60—VEHICLES IN GENERAL
- B60F—VEHICLES FOR USE BOTH ON RAIL AND ON ROAD; AMPHIBIOUS OR LIKE VEHICLES; CONVERTIBLE VEHICLES
- B60F5/00—Other convertible vehicles, i.e. vehicles capable of travelling in or on different media
- B60F5/02—Other convertible vehicles, i.e. vehicles capable of travelling in or on different media convertible into aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D9/00—Equipment for handling freight; Equipment for facilitating passenger embarkation or the like
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Transportation (AREA)
- Forklifts And Lifting Vehicles (AREA)
Abstract
The invention belongs to the technical field of unmanned aerial vehicles, and relates to a multifunctional unmanned aerial vehicle. Including two unmanned aerial vehicles, still include unmanned aerial vehicle organism, first actuating mechanism, second actuating mechanism, searchlighting mechanism, bear mechanism and grafting mechanism, two unmanned aerial vehicle's structural principle, the driving method is the same, first actuating mechanism, second actuating mechanism, searchlighting mechanism, bear mechanism and grafting mechanism all set up on the unmanned aerial vehicle organism, first actuating mechanism and second actuating mechanism all set up inside the unmanned aerial vehicle organism and are connected with the unmanned aerial vehicle organism searchlighting mechanism sets up at unmanned aerial vehicle organism top, bear mechanism and grafting mechanism and all set up in unmanned aerial vehicle organism bottom. The disaster rescue unmanned aerial vehicle solves the problems that in the prior art, a finished product is large and single in use when the disaster rescue unmanned aerial vehicle is actually applied, and the disaster rescue unmanned aerial vehicle cannot be used for a long time without rescue, so that resource waste is caused.
Description
Technical Field
The invention relates to the technical field of unmanned aerial vehicles, in particular to a multifunctional unmanned aerial vehicle.
Background
Unmanned aerial vehicles are unmanned aerial vehicles operated by radio remote control devices and self-contained program control devices, or operated autonomously by an on-board computer, either completely or intermittently. For military use, unmanned aerial vehicles divide into reconnaissance aircraft and target drone. In the civil aspect, the unmanned aerial vehicle + the industry application is really just needed by the unmanned aerial vehicle; at present, the unmanned aerial vehicle is applied to the fields of aerial photography, agriculture, plant protection, miniature self-timer, express transportation, disaster relief, wild animal observation, infectious disease monitoring, surveying and mapping, news reporting, power inspection, disaster relief, film and television shooting, romantic manufacturing and the like, and the application of the unmanned aerial vehicle is greatly expanded.
Patent number CN 111204453A discloses a big load unmanned aerial vehicle rescue device, including big
Load unmanned aerial vehicle, the rescue cabin, the equipment frame, the capstan winch, the assembly pulley, remote control locking part, this device can be used to the war, natural disasters, aerial quick rescue under emergency such as epidemic situation, because of adopting unmanned aerial vehicle flight technique, need not pilot's driving, can get into any danger, unknown zone expandes the rescue, unmanned aerial vehicle need not to descend, can suspend aerial rescue cabin, wait to need the salvage personnel to get into and hang up rescue cabin through the capstan winch behind the rescue cabin, fix in unmanned aerial vehicle bottom through the remote control electronic lock when arriving the highest point, this device can fix rescue cabin in unmanned aerial vehicle bottom, flight is steady, very big guarantee that the wounded can not receive secondary damage, take comfortablely, safety, the cost of manufacture is low, can use manpower sparingly, financial resources, also can solve present aerial rescue resource shortage problem.
However, in the prior art, the disaster relief unmanned aerial vehicle is large in finished product and single in use in practical application, and cannot be used for a long time without rescue, so that resource waste is caused.
Disclosure of Invention
The invention aims to provide a multifunctional unmanned aerial vehicle to solve the technical problem in the background technology.
The invention provides a multifunctional unmanned aerial vehicle which comprises two unmanned aerial vehicles, and further comprises an unmanned aerial vehicle body, a first driving mechanism, a second driving mechanism, a searchlighting mechanism, a bearing mechanism and a plugging mechanism, wherein the two unmanned aerial vehicles have the same structural principle and the same driving mode, the first driving mechanism, the second driving mechanism, the searchlighting mechanism, the bearing mechanism and the plugging mechanism are all arranged on the unmanned aerial vehicle body, the first driving mechanism and the second driving mechanism are all arranged in the unmanned aerial vehicle body and are connected with the unmanned aerial vehicle body, the searchlighting mechanism is arranged at the top of the unmanned aerial vehicle body, and the bearing mechanism and the plugging mechanism are both arranged at the bottom of the unmanned aerial vehicle body.
Further, the unmanned aerial vehicle organism includes fixed part and rotating part, rotating part sets up around fixed part, rotating part is connected with fixed part.
Further, the fixing part comprises a first bearing hollow column, a second bearing hollow column, a bearing plate, a second bearing plate and a bearing box body, the second bearing hollow column is arranged at the top of the first bearing hollow column, the bearing plate and the second bearing plate are respectively arranged on two sides of the first bearing hollow column, and the bearing box body is arranged at the top of the bearing plate.
Further, the rotatable parts includes sensor, six extension frame, six first screw, four foot rests and four pulleys, the sensor sets up in the second bears the weight of empty core post, six the one end of extending the frame all sets up inside first bearing the weight of empty core post, six around the first bearing the weight of empty core post of even distribution of extension frame, six first screw sets up respectively on the other end of extending the frame, four the foot rest sets up respectively at the extension frame top of first bearing the weight of empty core post both sides, four the pulley sets up respectively in the bottom of foot rest.
Further, first actuating mechanism includes first motor, first master gear, six first auxiliary gears, six connection belts and six spliced poles, first motor, first master gear, six first auxiliary gears and six spliced poles all set up in first bearing hollow post, the output and the first master gear of first motor are connected, six first auxiliary gear evenly distributed is around first master gear, six the spliced pole sets up respectively on first auxiliary gear, six the one end of connecting the belt is connected with the spliced pole respectively, six the other end of connecting the belt all runs through first bearing hollow post and is connected with first screw respectively.
Further, the second actuating mechanism includes second motor, second master gear, two second auxiliary gears, two connecting rods and two second screws, second motor, second master gear and second auxiliary gear all set up in bearing box, the output and the second master gear connection of second motor, two the second auxiliary gear sets up around the second master gear, two the second auxiliary gear all meshes with the second master gear, two the connecting rod sets up respectively on the second auxiliary gear, two the other end of connecting rod all runs through bearing box and extends outside the bearing box, two the second screw sets up respectively at the other end of connecting rod.
Further, searchlighting mechanism includes micro motor, motor rack, bearer post, fixed block and camera, the motor rack sets up the top that bears hollow post at the second, micro motor sets up in the motor rack, micro motor's output and bearer post are connected, the fixed block sets up the top at the bearer post, the camera sets up the one side at the fixed block.
Further, the bearing mechanism comprises a fixed plate, two fixed connecting rods, two fixed rods, four first air cylinders, four bases and five placing nets, the tops of the two fixed connecting rods are arranged at the bottom of the first bearing hollow column, the bottoms of the two fixed connecting rods are connected with the top of the fixed plate, the four first air cylinders are respectively arranged at four corners of the bottom of the fixed plate at intervals, the four bases are all arranged at the tops of the first air cylinders and connected with the first air cylinders, one fixed rod is arranged between every two bases, the fixed rods are hinged with the bases, the five placing nets are arranged in a dispersed manner, one placing net is arranged at the top of each fixed rod, the top of each placing net is connected with the bottom of the fixed plate, one placing net is arranged between the two fixed rods, and one placing net is arranged between every two first air cylinders, the top of the placing net between the first air rods is connected with the output end of the first air cylinder, and the bottom of the placing net between the first air rods is connected with the base.
Further, the inserting mechanism comprises a second cylinder, a cylinder fixing plate, a rotating plate, a fixing column and a hook rod, the second cylinder, the cylinder fixing plate and the fixing column are all arranged at the bottom of the second bearing plate, the rotating plate is arranged on the fixing column, the hook rod is arranged on the rotating plate, a hook and a convex angle are arranged on the rotating plate, and the output end of the second cylinder corresponds to the convex angle.
Compared with the prior art, the invention has the beneficial effects that:
the unmanned aerial vehicle comprises an unmanned aerial vehicle body, a first driving mechanism, a second driving mechanism, a searchlighting mechanism, a bearing mechanism and a plugging mechanism, the two unmanned aerial vehicles have the same structural principle and can be plugged into a whole in the same driving mode, the first driving mechanism, the second driving mechanism, the searchlighting mechanism, the bearing mechanism and the plugging mechanism are all arranged on the unmanned aerial vehicle body, the first driving mechanism and the second driving mechanism are all arranged inside the unmanned aerial vehicle body, the searchlighting mechanism is arranged at the top of the unmanned aerial vehicle body, the bearing mechanism and the plugging mechanism are all arranged at the bottom of the unmanned aerial vehicle body, the first driving mechanism can vertically lift the unmanned aerial vehicle body upwards to lift the unmanned aerial vehicle body to the air for flying, the second driving mechanism can drive the unmanned aerial vehicle body on the ground, and the searchlighting mechanism can shoot the periphery of the unmanned aerial vehicle body, bear the mechanism and can place some daily necessities and medical supplies that need transport, when two unmanned aerial vehicle link together, two unmanned aerial vehicle's the mechanism that bears can use together, can make the bearing capacity of unmanned aerial vehicle organism promote greatly, can bear the mechanism this moment and can place some heavier article and injured wounded, grafting mechanism can make two unmanned aerial vehicle docks. The disaster rescue unmanned aerial vehicle solves the problems that in the prior art, a finished product is large and single in use when the disaster rescue unmanned aerial vehicle is actually applied, and the disaster rescue unmanned aerial vehicle cannot be used for a long time without rescue, so that resource waste is caused.
Secondly, the searchlighting mechanism is additionally arranged and comprises a micro motor, a motor placing frame, a bearing column, a fixing block and a camera, the motor placing frame is arranged at the top of the second bearing hollow column, the micro motor is arranged in the motor placing frame, the output end of the micro motor is connected with the bearing column, the fixing block is arranged at the top of the bearing column, the camera is arranged on one side of the fixing block, the motor placing frame is used for placing the micro motor, the micro motor is used for driving the bearing column to operate, the fixing block is used for placing the camera, the camera can shoot and record the periphery of the unmanned aerial vehicle, and under the driving of the micro motor, the camera can rotate, so that the shooting range of the camera is enlarged. Can make unmanned aerial vehicle shoot at the flight in-process, shoot the mechanism and can also make unmanned aerial vehicle provide the picture for the user when the butt joint in the air, make unmanned aerial vehicle more convenient when the butt joint in the air.
Thirdly, the invention adds a bearing mechanism which comprises a fixed plate, two fixed rods, four first air cylinders, four bases and five placing nets, wherein the tops of the two fixed rods are arranged at the bottoms of the first bearing hollow columns, the bottoms of the two fixed rods are connected with the tops of the fixed plates, the four first air cylinders are respectively arranged at four corners of the bottoms of the fixed plates at intervals, the four bases are all arranged at the tops of the first air cylinders and are connected with the first air cylinders, one fixed rod is arranged between every two bases, the fixed rods are hinged with the bases, the five placing nets are arranged in a scattered manner, the top of each fixed rod is provided with one placing net, the top of each placing net is connected with the bottom of the fixed plate, one placing net is arranged between every two first air rods, the top of each placing net between the first air rods is connected with the output end of the first air cylinder, the bottom of the placing net between the first air rods is connected with the base. The bearing mechanism adopted in the invention is composed of the placing net, so that the safety of the article, the wounded and the lightly-placed fragile article can be ensured no matter the article, the wounded and the lightly-placed fragile article are placed, and the condition that the article is damaged due to collision can be avoided.
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, 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 some embodiments of the present invention, and other drawings can be obtained by those skilled in the art without creative efforts.
FIG. 1 is a top view of the present invention;
FIG. 2 is a partial perspective view of the first embodiment of the present invention;
FIG. 3 is a partial perspective view of the second embodiment of the present invention;
FIG. 4 is a third schematic view of a partial perspective structure of the present invention;
FIG. 5 is a cross-sectional view taken along line A-A of FIG. 1;
FIG. 6 is a schematic view of the insertion mechanism and the carrying mechanism of the present invention;
FIG. 7 is an enlarged view at B in FIG. 6;
FIG. 8 is a schematic view of a load bearing mechanism of the present invention;
reference numerals: unmanned aerial vehicle 1, unmanned aerial vehicle body 2, fixed part 201, first bearing hollow column 2011, second bearing hollow column 2012, bearing plate 2013, second bearing plate 2014, bearing box 2015, rotating part 202, sensor 2021, extension frame 2022, first propeller 2023, foot stool 2024, pulley 2025, first driving mechanism 3, first motor 301, first main gear 302, first auxiliary gear 303, connecting belt 304, connecting column 305, second driving mechanism 4, second motor 401, second main gear 402, second auxiliary gear 403, connecting rod 404, second propeller 405, searchlighting mechanism 5, micro motor 501, motor placement frame 502, bearing column 503, fixed block 504, camera 505, bearing mechanism 6, fixed plate 601, fixed connecting rod 606, fixed rod 602, first cylinder 603, base 604, placement net 605, plugging mechanism 7, second cylinder 701, cylinder fixed plate 702, rotating plate 703, cylinder fixing plate 703, positioning mechanism, Fixed post 704, hooked rod 705, hook 7031, lobe 7032.
Detailed Description
The technical solutions of the present invention will be described clearly and completely with reference to the accompanying drawings, and it should be understood that the described embodiments are some, but not all embodiments of the present invention.
The components of embodiments of the present invention generally described and illustrated in the figures herein may be arranged and designed in a wide variety of different configurations. Thus, the following detailed description of the embodiments of the present invention, presented in the figures, is not intended to limit the scope of the invention, as claimed, but is merely representative of selected embodiments of the invention.
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.
In the description of the present invention, it should be noted that the terms "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inner", "outer", etc., indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are only for convenience of description and simplicity of description, but 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 "third" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance.
In the description of the present invention, it should be noted that, unless otherwise explicitly specified or limited, the terms "mounted," "connected," and "connected" are to be construed broadly, e.g., as meaning either 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.
As shown in fig. 1 to 7, an embodiment of the present invention provides a multifunctional unmanned aerial vehicle, which includes two unmanned aerial vehicles 1, and further includes an unmanned aerial vehicle body 2, a first driving mechanism 3, a second driving mechanism 4, a searchlighting mechanism 5, a bearing mechanism 6, and a plugging mechanism 7, the two unmanned aerial vehicles 1 have the same structural principle and the same driving manner, the two unmanned aerial vehicles 1 can be plugged into a whole, the first driving mechanism 3, the second driving mechanism 4, the searchlighting mechanism 5, the bearing mechanism 6, and the plugging mechanism 7 are all disposed on the unmanned aerial vehicle body 2, the first driving mechanism 3 and the second driving mechanism 4 are both disposed inside the unmanned aerial vehicle body 2 and are connected with the unmanned aerial vehicle body 2, the searchlighting mechanism 5 is disposed on the top of the unmanned aerial vehicle body 2, the bearing mechanism 6 and the plugging mechanism 7 are both disposed on the bottom of the unmanned aerial vehicle body 2, the first driving mechanism 3 can lift the unmanned aerial vehicle body 2 vertically upward, make unmanned aerial vehicle organism 2 rise to fly in the air, second actuating mechanism 4 can make unmanned aerial vehicle organism 2 go on the ground, searchlighting mechanism 5 can shoot around unmanned aerial vehicle organism 2, some daily necessities and medical supplies that need transport can be placed to bearing mechanism 6, and when two unmanned aerial vehicle 1 links together, two unmanned aerial vehicle 1's bearing mechanism 6 can use together, can make unmanned aerial vehicle organism 2's bearing capacity promote greatly, can bearing mechanism 6 can place some heavier article and injured wounded this moment, grafting mechanism 7 can make two unmanned aerial vehicle 1 docks.
The unmanned aerial vehicle body 2 comprises a fixed part 201 and a rotating part 202, the rotating part 202 is arranged around the fixed part 201, the rotating part 202 is connected with the fixed part 201, the fixed part 201 is used for placing a first driving mechanism 3, a second driving mechanism 4, a searchlighting mechanism 5, a bearing mechanism 6 and a plugging mechanism 7, and the rotating part 202 is used for flying the unmanned aerial vehicle body 2 and can run on the ground.
Fixed part 201 includes first empty core post 2011 of bearing, the second bears empty core post 2012, loading board 2013, second loading board 2014 and bears box 2015, the second bears empty core post 2012 and sets up at the top of first empty core post 2011 of bearing, loading board 2013 and second loading board 2014 set up respectively in the first both sides of bearing empty core post 2011 of bearing, bear box 2015 and set up at the top of loading board 2013, first empty core post 2011 of bearing is used for placing first actuating mechanism 3, the second bears empty core post 2012 and is used for placing rotor 202, loading board 2013 is used for placing bears box 2015, second loading board 2014 is used for placing grafting mechanism 7, it is used for placing second actuating mechanism 4 to bear box 2015.
The rotating part 202 includes a sensor 2021, six extension stands 2022, six first propellers 2023, four foot stands 2024, and four pulleys 2025, the sensor 2021 is disposed in the second hollow bearing column 2012, one end of each of the six extending frames 2022 is disposed inside the first hollow bearing column 2011, the six extending frames 2022 are uniformly distributed around the first hollow bearing column 2011, the six first propellers 2023 are respectively disposed at the other end of the extending frame 2022, the four foot rests 2024 are respectively disposed at the tops of the extending frames 2022 at two sides of the first hollow bearing column 2011, the four pulleys 2025 are respectively disposed at the bottoms of the foot rests 2024, the sensor 2021 is used for accepting the user to unmanned aerial vehicle 1's control signal, six extend the frame 2022 all is used for placing the screw, four the foot rest 2024 is used for unmanned aerial vehicle organism 2 to play the supporting role when descending to the ground, the pulley 2025 is used for unmanned aerial vehicle organism 2 to provide the sliding force when ground is traveling.
The first driving mechanism 3 includes a first motor 301, a first main gear 302, six first auxiliary gears 303, six connecting belts 304 and six connecting columns 305, the first motor 301, the first main gear 302, six first auxiliary gears 303 and six connecting columns 305 are all disposed in a first hollow bearing column 2011, an output end of the first motor 301 is connected with the first main gear 302, the six first auxiliary gears 303 are uniformly distributed around the main gear, the six connecting columns 305 are respectively disposed on the first auxiliary gears, one ends of the six connecting belts 304 are respectively connected with the connecting columns 305, the other ends of the six connecting belts 304 all penetrate through the first hollow bearing column 2011 and are respectively connected with the first propellers 2023, the first motor 301 is used for driving the main gear, the first main gear 302 can drive the six first auxiliary gears to operate, the first auxiliary gears 303 are used for driving the connecting columns 305 and the connecting belts 304 to operate, the connecting belt 304 may rotate the first propeller 2023.
The second driving mechanism 4 includes a second motor 401, a second main gear 402, two second auxiliary gears 403, two connecting rods 404 and two second propellers 405, the second motor 401, the second main gear 402 and the second auxiliary gears 403 are all disposed in a carrying case 2015, the output end of the second motor 401 is connected with the second main gear 402, the two second auxiliary gears 403 are disposed around the second main gear 402, the two second auxiliary gears 403 are both engaged with the second main gear 402, the two connecting rods 404 are respectively disposed on the second auxiliary gears 403, the other ends of the two connecting rods 404 are both penetrated through the carrying case 2015 and extend out of the carrying case 2015, the two second propellers 405 are respectively disposed at the other ends of the connecting rods 404, the second motor 401 is used for driving the second main gear 402, the second main gear 402 can carry the second auxiliary gears 403 for operation, the two connecting rods 404 will run synchronously with the second auxiliary gear 403 and drive the second propeller 405 to rotate, and the rotation of the second propeller 405 can make the unmanned aerial vehicle 1 run on the ground.
The bearing mechanism 6 comprises a fixing plate 601, two fixing connecting rods 606, two fixing rods 602, four first air cylinders 603, four bases 604 and five placing nets 605, the tops of the two fixing connecting rods 606 are arranged at the bottom of the first bearing hollow column 2011, the bottoms of the two fixing connecting rods 606 are connected with the top of the fixing plate 601, the four first air cylinders 603 are respectively arranged at four corners of the bottom of the fixing plate 601 at intervals, the four bases 604 are respectively arranged at the top of the first air cylinders 603 and connected with the first air cylinders 603, one fixing rod 602 is arranged between every two bases 604, the fixing rods 602 are hinged with the bases 604, the five placing nets 605 are arranged in a scattered manner, one placing net 605 is arranged at the top of each fixing rod 602, the top of the placing net 605 is connected with the bottom of the fixing plate 601, one placing net 605 is arranged between the two fixing rods 602, a placing net 605 is arranged between every two first air rods, the top of the placing net 605 between the first air rods is connected with the output end of the first air cylinder 603, the bottom of the placing net 605 between the first air cylinders 603 is connected with the base 604, the placing net 605 on the fixing rod 602 can suspend the fixing rod 602 at the bottom of the fixing plate 601, the fixing rod 602 can also fix the base 604, the base 604 is hinged with the fixing rod 602 to enable the first air cylinder 603 to change the angle, the first air rods can rotate 90 degrees outwards at most, and the first air rods can drive the placing net 605 to adjust the length.
The plugging mechanism 7 includes a second cylinder 701, a cylinder fixing plate 702, a rotating plate 703, a fixing column 704 and a hook rod 705, the second cylinder 701, the cylinder fixing plate 702 and the fixing column 704 are all arranged at the bottom of the second bearing plate 2014, the rotating plate 703 is arranged on the fixing column 704, the hook rod 705 is arranged on the rotating plate 703, the rotating plate 703 is provided with a hook 7031 and a convex 7032, the output end of the second cylinder 701 corresponds to the convex 7032, the cylinder fixing plate 702 is used for fixing the second cylinder 701, the second cylinder 701 is used for pushing the convex 7032, the hook rod 705 and the hook 7031 are used for butting two unmanned aerial vehicles 1 to play a plugging role, so that the two unmanned aerial vehicles 1 can be fixedly connected.
The working principle is that the two unmanned aerial vehicles 1 can transport some lighter objects when being used independently, when the unmanned aerial vehicle 1 is started independently, the first driving mechanism 3 is operated, the first motor 301 drives the first main gear 302 and the first auxiliary gear 303, the unmanned aerial vehicle can achieve the purpose of flying through the first screw 2023, the second driving mechanism 4 is operated, the second motor 401 drives the second main gear 402 and the second auxiliary gear 403, the unmanned aerial vehicle 1 can achieve the purpose of traveling on the ground through the second screw 405 and the pulley 2025 at the bottom of the foot stand 2024, the bearing mechanism 6 is composed of a fixed rod 602, a fixed plate 601, a first air cylinder 603, an air cylinder base 604 and a placing net 605, when the objects are placed, the two air rods at the bottom side of the fixed plate 601 can be subjected to angle change through the hinging of the air cylinder base 604 on the fixed rod 602, the first air cylinder 603 drives the placing net 605 to change from a vertical state to a horizontal state, when articles are placed on the placing net 605 between the two fixing rods 602, the first air cylinder 603 is rotated to be closed in a vertical state, so that the purpose of transporting the unmanned aerial vehicle 1 can be achieved, when the two unmanned aerial vehicles 1 need to be butted, the two unmanned aerial vehicles 1 can be butted through the plugging mechanisms 7 arranged on the two unmanned aerial vehicles 1, the hook 7031 on the other plugging mechanism 7 can be hooked through the hook rod 705 arranged on the plugging mechanism 7, after the butting is completed, the bearing capacity of the two unmanned aerial vehicles 1 can be increased, the bearing mechanisms 6 can be used in a combined manner, at the moment, the bearing mechanism 6 can transport some heavier articles or can be used as a rescue machine, injured persons can be placed on the two combined bearing mechanisms 6 for transportation, when the butting state needs to be relieved, the second air cylinder 701 pushes the convex angle 7032 to enable the rotating plate 703 to rotate, the hook rod 705 can be separated from the limit of the hook 7031, the butt joint state is released. The disaster rescue unmanned aerial vehicle solves the problems that in the prior art, a finished product is large and single in use when the disaster rescue unmanned aerial vehicle is actually applied, and the disaster rescue unmanned aerial vehicle cannot be used for a long time without rescue, so that resource waste is caused.
Finally, it should be noted that: the above embodiments are only used to illustrate the technical solution of the present invention, and not to limit the same; while the invention has been described in detail and with reference to the foregoing embodiments, it will be understood by those skilled in the art that: the technical solutions described in the foregoing embodiments may still be modified, or some or all of the technical features may be equivalently replaced; and the modifications or the substitutions do not make the essence of the corresponding technical solutions depart from the scope of the technical solutions of the embodiments of the present invention.
Claims (7)
1. A multifunctional unmanned aerial vehicle comprises two unmanned aerial vehicles (1) and is characterized by further comprising an unmanned aerial vehicle body (2), a first driving mechanism (3), a second driving mechanism (4), a searchlighting mechanism (5), a bearing mechanism (6) and a plugging mechanism (7), wherein the two unmanned aerial vehicles (1) have the same structural principle and the same driving mode, the first driving mechanism (3), the second driving mechanism (4), the searchlighting mechanism (5), the bearing mechanism (6) and the plugging mechanism (7) are all arranged on the unmanned aerial vehicle body (2), the first driving mechanism (3) and the second driving mechanism (4) are both arranged in the unmanned aerial vehicle body (2) and are connected with the unmanned aerial vehicle body (2), the searchlighting mechanism (5) is arranged at the top of the unmanned aerial vehicle body (2), the bearing mechanism (6) and the inserting mechanism (7) are arranged at the bottom of the unmanned aerial vehicle body (2);
the unmanned aerial vehicle body (2) comprises a fixed part (201) and a rotating part (202), the rotating part (202) is arranged around the fixed part (201), and the rotating part (202) is connected with the fixed part (201);
fixed part (201) include first bear hollow post (2011), the second bears hollow post (2012), loading board (2013), second loading board (2014) and bear box (2015), the second bears hollow post (2012) and sets up at the first top of bearing hollow post (2011), loading board (2013) and second loading board (2014) set up respectively in the first both sides of bearing hollow post (2011), bear box (2015) and set up at the top of loading board (2013).
2. The multifunctional unmanned aerial vehicle of claim 1, wherein the rotating component (202) comprises a sensor (2021), six extension frames (2022), six first propellers (2023), four foot rests (2024) and four pulleys (2025), the sensor (2021) is arranged in the second hollow load-bearing column (2012), one ends of the six extension frames (2022) are all arranged inside the first hollow load-bearing column (2011), the six extension frames (2022) are uniformly distributed around the first hollow load-bearing column (2011), the six first propellers (2023) are respectively arranged at the other ends of the extension frames (2022), the four foot rests (2024) are respectively arranged at the tops of the extension frames (2022) on two sides of the first hollow load-bearing column (2011), and the four pulleys (2025) are respectively arranged at the bottoms of the foot rests (2024).
3. A multifunctional drone according to claim 2, characterised in that the first driving mechanism (3) comprises a first motor (301), a first main gear (302), six first auxiliary gears (303), six connecting belts (304) and six connecting posts (305), the first motor (301), the first main gear (302), the six first auxiliary gears (303) and the six connecting columns (305) are all arranged in a first bearing hollow column (2011), the output of first motor (301) is connected with first master gear (302), and six first auxiliary gear (303) evenly distributed is around first master gear (302), and six spliced pole (305) set up respectively on first auxiliary gear (303), and six the one end of connecting belt (304) is connected with spliced pole (305) respectively, and six the other end of connecting belt (304) all runs through first bearing hollow post (2011) and is connected with first screw (2023) respectively.
4. A multi-function drone according to claim 1, characterised in that the second driving mechanism (4) comprises a second electric motor (401), a second main gear (402), two second auxiliary gears (403), two connecting rods (404) and two second propellers (405), the second electric motor (401), the second main gear (402) and the second auxiliary gears (403) being all arranged inside a carrying case (2015), the output of the second electric motor (401) being connected with the second main gear (402), the two second auxiliary gears (403) being arranged around the second main gear (402), the two second auxiliary gears (402) being in mesh with the second main gear (402), the two connecting rods (404) being respectively arranged on the second auxiliary gears (403), the other ends of the two connecting rods (404) extending through the carrying case (2015) and out of the carrying case (2015), the two second propellers (405) are respectively arranged at the other end of the connecting rod (404).
5. The multifunctional unmanned aerial vehicle of claim 2, wherein the searchlight mechanism (5) comprises a micro motor (501), a motor placing rack (502), a bearing column (503), a fixing block (504) and a camera (505), the motor placing rack (502) is arranged on the top of the second bearing hollow column (2012), the micro motor (501) is arranged in the motor placing rack (502), the output end of the micro motor (501) is connected with the bearing column (503), the fixing block (504) is arranged on the top of the bearing column (503), and the camera (505) is arranged on one side of the fixing block (504).
6. The multifunctional unmanned aerial vehicle of claim 1, wherein the carrying mechanism (6) comprises a fixed plate (601), two fixed connecting rods (606), two fixed rods (602), four first air cylinders (603), four bases (604) and five placing nets (605), the tops of the two fixed connecting rods (606) are arranged at the bottom of the first carrying hollow column (2011), the bottoms of the two fixed connecting rods (606) are connected with the top of the fixed plate (601), the four first air cylinders (603) are respectively arranged at four corners of the bottom of the fixed plate (601) at intervals, the four bases (604) are respectively arranged at the tops of the first air cylinders (603) and connected with the first air cylinders (603), one fixed rod (602) is arranged between each two bases (604), and the fixed rods (602) are hinged with the bases (604), five place net (605) dispersion settings, every dead lever (602) top all is equipped with one and places net (605) and the top of placing net (605) is connected with the bottom of fixed plate (601), two be equipped with one between dead lever (602) and place net (605), per two all be equipped with one between first cylinder (603) and place net (605), the output of placing net (605) top and first cylinder (603) between the first air pole is connected, the net (605) bottom of placing between the first air pole is connected with base (604).
7. The multifunctional unmanned aerial vehicle of claim 6, wherein the plug-in mechanism (7) comprises a second cylinder (701), a cylinder fixing plate (702), a rotating plate (703), a fixing column (704) and a hook rod (705), the second cylinder (701), the cylinder fixing plate (702) and the fixing column (704) are all arranged at the bottom of the second bearing plate (2014), the rotating plate (703) is arranged on the fixing column (704), the hook rod (705) is arranged on the rotating plate (703), a hook (7031) and a convex angle (7032) are arranged on the rotating plate (703), and an output end of the second cylinder (701) corresponds to the convex angle (7032).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202010609860.0A CN111703575B (en) | 2020-06-29 | 2020-06-29 | Multifunctional unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202010609860.0A CN111703575B (en) | 2020-06-29 | 2020-06-29 | Multifunctional unmanned aerial vehicle |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN111703575A CN111703575A (en) | 2020-09-25 |
| CN111703575B true CN111703575B (en) | 2021-09-14 |
Family
ID=72543307
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202010609860.0A Active CN111703575B (en) | 2020-06-29 | 2020-06-29 | Multifunctional unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN111703575B (en) |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112386845B (en) * | 2020-11-12 | 2021-12-07 | 山东龙翼航空科技有限公司 | Unmanned aerial vehicle docking structure for fire fighting and use method |
| CN112193415B (en) * | 2020-11-12 | 2021-12-17 | 江苏润翔软件技术有限公司 | Combined rescue unmanned aerial vehicle and using method thereof |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2015187259A9 (en) * | 2014-05-08 | 2016-05-06 | Thomas Mcnally | Convertible payload transport aircraft |
| CN205524962U (en) * | 2016-03-30 | 2016-08-31 | 深圳市高巨创新科技开发有限公司 | Modular unmanned aerial vehicle |
| CN108216629A (en) * | 2018-02-26 | 2018-06-29 | 西北工业大学 | A kind of combination transport unmanned plane |
| CN109131885A (en) * | 2018-10-25 | 2019-01-04 | 周军 | A kind of unmanned flight's device for fire rescue |
| CN209479339U (en) * | 2019-01-23 | 2019-10-11 | 南昌航空大学 | A kind of land, water and air three-purpose vehicle |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20140217230A1 (en) * | 2013-02-05 | 2014-08-07 | Biosphere Aerospace, Llc | Drone cargo helicopter |
-
2020
- 2020-06-29 CN CN202010609860.0A patent/CN111703575B/en active Active
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2015187259A9 (en) * | 2014-05-08 | 2016-05-06 | Thomas Mcnally | Convertible payload transport aircraft |
| CN205524962U (en) * | 2016-03-30 | 2016-08-31 | 深圳市高巨创新科技开发有限公司 | Modular unmanned aerial vehicle |
| CN108216629A (en) * | 2018-02-26 | 2018-06-29 | 西北工业大学 | A kind of combination transport unmanned plane |
| CN109131885A (en) * | 2018-10-25 | 2019-01-04 | 周军 | A kind of unmanned flight's device for fire rescue |
| CN209479339U (en) * | 2019-01-23 | 2019-10-11 | 南昌航空大学 | A kind of land, water and air three-purpose vehicle |
Also Published As
| Publication number | Publication date |
|---|---|
| CN111703575A (en) | 2020-09-25 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN111703575B (en) | Multifunctional unmanned aerial vehicle | |
| CN105235912A (en) | Aerial photography collection unmanned aerial vehicle for law enforcement of police fire protection and control method thereof | |
| CN112644732A (en) | Vehicle-mounted multi-rotor unmanned aerial vehicle take-off and landing platform | |
| CN106956776A (en) | A kind of unmanned plane throwing device and unmanned plane | |
| CN210214608U (en) | Unmanned aerial vehicle supervision platform | |
| CN113501131B (en) | Honeycomb type aerial unmanned aerial vehicle launching and recycling device, unmanned aerial vehicle and aerial aircraft carrier | |
| DE102005014948A1 (en) | Four-rotor model helicopter, has detachable plug connection to mechanically connect sub-assemblies, and electrical connections to connect electrical components of sub-assemblies, with electrical connections integrated in plug connection | |
| CN110697020A (en) | Unmanned aerial vehicle lightweight folding frame | |
| CN210653614U (en) | Fixed wing aircraft with quickly detachable wings | |
| CN212448091U (en) | Unmanned aerial vehicle frame is patrolled and examined to bridge and unmanned aerial vehicle is patrolled and examined to bridge | |
| CN207045715U (en) | A kind of novel and multifunctional unmanned plane | |
| CN206734616U (en) | A kind of electronic unmanned plane frame of eight rotors | |
| CN205150229U (en) | Many rotors of multilayer airborne vehicle | |
| CN212099341U (en) | Foldable many rotors rescue unmanned aerial vehicle | |
| CN219619381U (en) | Suspended unmanned aerial vehicle carrying device | |
| US20130276383A1 (en) | Modular structure | |
| CN112793766A (en) | Unmanned aerial vehicle is patrolled and examined to undercarriage folded cascade | |
| CN211969736U (en) | Many rotor crafts's organism and many rotor crafts | |
| CN208484829U (en) | Express delivery unmanned plane | |
| CN209889129U (en) | Scalable comprehensive protection device of unmanned aerial vehicle | |
| CN209938990U (en) | Self-align lift platform and unmanned aerial vehicle space station | |
| CN211766284U (en) | Foldable VTOL reconnaissance monitoring unmanned aerial vehicle | |
| CN113148188A (en) | Dual-power vertical take-off and landing fixed-wing unmanned aerial vehicle | |
| CN210494408U (en) | Unmanned aerial vehicle rescue stretcher | |
| DE69929356T2 (en) | AIRBALLON FOR TRANSPORTING PASSENGERS AND GOODS |
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 | ||
| TA01 | Transfer of patent application right | ||
| TA01 | Transfer of patent application right |
Effective date of registration: 20210826 Address after: 210000 in Jiangsu Software Park, No.1 Dongji Avenue, Jiangning Economic and Technological Development Zone, Nanjing City, Jiangsu Province (Jiangning Development Zone) Applicant after: Nanjing Tuoheng Unmanned System Research Institute Co.,Ltd. Address before: 241000 building d2-8, chengzhiguang, Jiujiang District, Wuhu City, Anhui Province Applicant before: Jin Weiming |
|
| GR01 | Patent grant | ||
| GR01 | Patent grant |