CN215851916U - Many rotor unmanned aerial vehicle of boat wing - Google Patents
Many rotor unmanned aerial vehicle of boat wing Download PDFInfo
- Publication number
- CN215851916U CN215851916U CN202121990910.0U CN202121990910U CN215851916U CN 215851916 U CN215851916 U CN 215851916U CN 202121990910 U CN202121990910 U CN 202121990910U CN 215851916 U CN215851916 U CN 215851916U
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- water pipe
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- fixedly connected
- pipe
- cooling
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- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims abstract description 45
- 238000001816 cooling Methods 0.000 claims abstract description 36
- 239000000498 cooling water Substances 0.000 claims abstract description 21
- 230000017525 heat dissipation Effects 0.000 claims abstract description 19
- 239000011324 bead Substances 0.000 claims description 2
- 230000000694 effects Effects 0.000 abstract description 6
- 230000033001 locomotion Effects 0.000 abstract description 6
- 230000002035 prolonged effect Effects 0.000 abstract description 4
- 230000005611 electricity Effects 0.000 description 9
- 238000010438 heat treatment Methods 0.000 description 6
- 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 3
- 239000011049 pearl Substances 0.000 description 3
- 238000010586 diagram Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- WHXSMMKQMYFTQS-UHFFFAOYSA-N Lithium Chemical compound [Li] WHXSMMKQMYFTQS-UHFFFAOYSA-N 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- 230000001174 ascending effect Effects 0.000 description 1
- 230000033228 biological regulation Effects 0.000 description 1
- 238000009835 boiling Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 239000006185 dispersion Substances 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 229910052744 lithium Inorganic materials 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000003068 static effect Effects 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
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- Cooling Or The Like Of Electrical Apparatus (AREA)
Abstract
The utility model discloses a boat wing multi-rotor unmanned aerial vehicle which comprises an unmanned aerial vehicle body, wherein a lower side wall of the unmanned aerial vehicle body is fixedly connected with an assembly box, an assembly plate is arranged in the assembly box, the outer wall of the assembly plate is fixedly connected with a cooling assembly, a water pipe is arranged in the cooling assembly, two ends of the water pipe penetrate through the cooling assembly, two ends of the water pipe are respectively provided with a one-way valve I and a one-way valve II, one end of the water pipe is connected with a cooling box, cooling water is arranged in the cooling box, the other end of the water pipe is connected with a connecting pipe, a guide pipe is jointly connected between the lower side wall of the connecting pipe and the cooling box, and a one-way valve III is arranged in the guide pipe. According to the utility model, through the intermittent meshing of the incomplete gear and the sawtooth groove, the intermittent suction type movement of cooling water in the water pipe is realized, so that the cooling water slowly flows and cools heat generated on the assembly plate, and meanwhile, the heat dissipation plate is utilized to dissipate heat of the assembly plate, so that the heat dissipation effect of the assembly plate is greatly improved, and the service life of the electronic control unit is prolonged.
Description
Technical Field
The utility model relates to the technical field of unmanned aerial vehicles, in particular to a submarine wing multi-rotor unmanned aerial vehicle.
Background
The field of aviation has emerged at present, and many devices can help people to complete tasks in extreme environments by means of the carrier of the aircraft. Many rotor unmanned aerial vehicle, also can be called multiaxis unmanned aerial vehicle, according to screw quantity, can be subdivided into four rotors, six rotors, eight rotors etc. again.
In order to solve the defects of small loading capacity, small flight time, poor wind resistance and the like of the multi-rotor unmanned aerial vehicle, the multi-rotor unmanned aerial vehicle with the boat wings mainly comprises a boat bag, wings, a motor, propellers, a machine body, a battery, a flight control system and the like, wherein the power is supplied by a lithium battery pack, the flight control system controls a plurality of motors, and when the propellers reach a certain rotating speed, the aircraft leaves the ground; because the buoyancy of the airship is equal to the weight of the battery, the two airship bags are driven to move by the flexible steel wire lines at the wing tips of the wings in the process of ascending and descending or forward and backward movement of the multiple rotors.
The size of the airship is reduced by using the double airship bags, and the battery components are hung below the airship bags, so that the buoyancy of the airship only bears the weight of the battery when the unmanned aerial vehicle flies, and the airship bags are small in size and convenient to fly, transport and the like; when the unmanned aerial vehicle rapidly advances, the wing part provides lift force at the same time, so that the multi-rotor power set can reduce the rotating speed, the power consumption can be further reduced, and the endurance time can be prolonged; meanwhile, when multiple rotors break down, the boat bag protects the rotors, and ground personnel and equipment cannot be injured.
However, the electricity among the current unmanned aerial vehicle is often fixed in the inside of subassembly case for arrange the inside electricity of subassembly case in and to be connected with the inside flight control system of subassembly case, and the subassembly case often is in encapsulated situation, and this is very easily so that the electricity that is fixed in the inside electricity of subassembly case is transferred heat dispersion extremely badly, very easily generates heat or sends out the boiling hot in the course of the work, finally damages the electricity and transfers, influences unmanned aerial vehicle's normal flight.
SUMMERY OF THE UTILITY MODEL
The utility model aims to solve the problems in the background art and provides a boat wing multi-rotor unmanned aerial vehicle.
In order to achieve the purpose, the utility model adopts the following technical scheme:
a boat wing multi-rotor unmanned aerial vehicle comprises an unmanned body, wherein a lower side wall of the unmanned body is fixedly connected with a component box, a component plate is arranged in the component box, an outer wall of the component plate is fixedly connected with a cooling component, a water pipe is arranged in the cooling component, two ends of the water pipe penetrate through the cooling component, a one-way valve I and a one-way valve II are respectively arranged at two ends of the water pipe, one end of the water pipe is connected with the cooling box, cooling water is arranged in the cooling box, the other end of the water pipe is connected with a connecting pipe, a guide pipe is jointly connected between the lower side wall of the connecting pipe and the cooling box, a three-way valve is arranged in the guide pipe, a connecting rod is slidably inserted at one end of the connecting pipe, which is far away from the water pipe, a piston is fixedly connected at one end of the connecting rod, which is positioned in the water pipe, and a spring sleeved on the outer wall of the connecting rod is fixedly connected between the piston and the inner wall of the connecting pipe, the cooling box is characterized in that one end of the connecting rod, which is positioned outside the connecting pipe, is fixedly connected with an L-shaped rod, a sawtooth groove is formed in the lower side wall of the L-shaped rod, a motor is fixedly connected to the upper side wall of the cooling box through the upper side wall of the cooling box, and an incomplete gear meshed with the sawtooth groove is fixedly connected to the tail end of an output shaft of the motor.
Preferably, the outer wall of the assembly plate is provided with a heat dissipation plate, and the outer wall of the assembly box is provided with heat dissipation holes opposite to the heat dissipation plate.
Preferably, the section of the water pipe located in the cooling assembly is in a continuous loop shape.
Preferably, a guide rod fixedly connected with the outer wall of the guide pipe is slidably inserted into the end part of the L-shaped rod.
Preferably, a plurality of resistance beads are movably embedded in the inner wall of the water pipe.
Preferably, four corners of the heat dissipation plate are fixedly connected with fixing blocks, and the outer wall of each fixing block is in threaded connection with bolts in threaded connection with the outer wall of the assembly plate.
Compared with the prior art, this many rotor unmanned aerial vehicle of boat wing's advantage lies in:
1. the piston and the cooling box are arranged, the reciprocating motion of the piston is realized through the intermittent meshing of the incomplete gear and the sawtooth groove, so that cooling water in the water pipe and the cooling box is sucked, meanwhile, the intermittent suction type motion of the cooling water in the water pipe is realized by matching with the one-way principle of the one-way valve, the cooling water slowly flows and cools heat generated on the component board, the heat dissipation effect of the component board is further realized, and the service life of the electric regulator is prolonged;
2. the heat dissipation plate is arranged, and the heat generated by the assembly plate can be brought out of the assembly box by the heat dissipation plate through convection between the heat dissipation plate and the heat dissipation holes, so that the heat dissipation efficiency of the electric regulation is further improved;
in conclusion, the intermittent suction type electric control device realizes intermittent suction type movement of cooling water in the water pipe through intermittent meshing of the incomplete gear and the sawtooth groove, so that the cooling water flows slowly and cools heat generated on the assembly plate, and meanwhile, the assembly plate is cooled by the cooling plate, so that the cooling effect of the assembly plate is greatly improved, and the service life of the electric control device is prolonged.
Drawings
Fig. 1 is a cross-sectional view of a component box in a kayak-wing multi-rotor unmanned aerial vehicle according to the present invention;
fig. 2 is a schematic structural diagram of a kayak-wing multi-rotor unmanned aerial vehicle according to the present invention;
fig. 3 is a schematic partial structure diagram of a kayak-wing multi-rotor unmanned aerial vehicle according to the present invention;
fig. 4 is a cross-sectional view of a water pipe in the kayak-wing multi-rotor unmanned aerial vehicle according to the present invention.
In the figure: the device comprises a component box 1, a component plate 2, a cooling component 3, a water pipe 4, a cooling box 5, a connecting pipe 6, a guide pipe 7, a check valve I8, a check valve II 9, a connecting rod 10, a piston 11, a spring 12, a L-shaped rod 13, a motor 14, an incomplete gear 15, a guide rod 16, a resistance ball 17, a heat dissipation plate 18, a heat dissipation hole 19, a fixing block 20, a bolt 21 and a check valve 22.
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.
In the description of the present invention, it is to be understood that the terms "upper", "lower", "front", "rear", "left", "right", "top", "bottom", "inner", "outer", and the like, indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, are merely for convenience in describing the present invention and simplifying the description, and do not indicate or imply that the device or element being referred to must have a particular orientation, be constructed and operated in a particular orientation, and thus, should not be construed as limiting the present invention.
Referring to fig. 1-4, a many rotor unmanned aerial vehicle of boat wing, includes unmanned organism, the lower lateral wall fixedly connected with subassembly case 1 of unmanned organism, be equipped with assembly plate 2 in the subassembly case 1, it needs to explain here that be equipped with circuit board, electric capacity, resistance and electricity on assembly plate 2 and wait for circuit work related parts.
The outer wall fixedly connected with cooling module 3 of assembly board 2 is equipped with water pipe 4 in the cooling module 3, and the inner wall activity of water pipe 4 is inlayed and is equipped with a plurality of resistance pearls 17, and when the cooling water in the water pipe 4 contacted with resistance pearls 17, resistance pearls 17 can carry out the deceleration to rivers to make the cooling water increase the contact time of cooling water and assembly board 2, make the cooling water can be to the abundant cooling of assembly board 2.
The setting of cooling module 3 is run through at the both ends of water pipe 4, check valve 8 and two 9 check valves are installed respectively at the both ends of water pipe 4, the one end of water pipe 4 is connected with cooler bin 5, be equipped with the cooling water in the cooler bin 5, one section that water pipe 4 is located cooler bin 3 is the setting of returning the shape in succession, the water pipe 4 that is the setting of connecting returning the shape has increased its and assembly board 2 area of contact, thereby increased the cooling area of cooling water to assembly board 2, the radiating effect is improved.
The other end of water pipe 4 is connected with connecting pipe 6, be connected with pipe 7 between the lower lateral wall of connecting pipe 6 and the cooler bin 5 jointly, be equipped with check valve three 22 in the pipe 7, the one end that water pipe 4 was kept away from to connecting pipe 6 slides and inserts and be equipped with connecting rod 10, one end fixedly connected with piston 11 that connecting rod 10 is located water pipe 4, common fixedly connected with cup joints spring 12 on connecting rod 10 outer wall between piston 11 and the 6 inner walls of connecting pipe, connecting rod 10 is located the outer one end fixedly connected with L type pole 13 of connecting pipe 6, the tip of L type pole 13 slides and inserts and is equipped with guide bar 16 with pipe 7 outer wall fixed connection, guide bar 16 can guarantee the stability of L type pole north at the reciprocating motion in-process.
The lower side wall of the L-shaped rod 13 is provided with a sawtooth groove, the upper side wall of the cooling box 5 is fixedly connected with a motor 14 through the middle, the tail end of an output shaft of the motor 14 is fixedly connected with an incomplete gear 15 meshed with the sawtooth groove, the motor 14 is started to drive the incomplete gear 15 to rotate, when the incomplete gear 15 is meshed with the sawtooth groove, the L-shaped rod is driven to move rightwards, then a piston 11 is driven to move rightwards through a connecting rod 10, a spring 12 is compressed, at the moment, under the suction of the piston 11, a one-way valve I8 and a one-way valve II 9 are opened, a one-way valve III 22 is closed, then cooling water in the cooling box 5 is pumped into a water pipe 4 through the one-way valve II 9 by using suction force, so that the water after cooling the component plate 2 flows into a connecting pipe 6 through the one-way valve I8 to be temporarily stored, the cooling water between the one-way valve I8 and the one-way valve II 9 is in a static state, and then when the incomplete gear 15 is not meshed with the sawtooth groove, piston 11 moves to the left under spring 12's elasticity, check valve 8 and check valve two 9 are closed this moment, check valve three 22 is opened, make the water of keeping in the connecting pipe 6 pass through pipe 7 and get into to the cooler bin 5 in the recooling, with this reciprocating, make the cooling water in the cooler bin 5 can be intermittent type one-way flow in water pipe 4, the well cooling water of intermittent time can carry out cooling to assembly board 2, last continuous cooling water of renewal in to water pipe 4, the realization is to the cooling heat dissipation of assembly board 2, the radiating effect of electricity accent has been improved greatly, the life of electricity accent has been improved.
Further, unless otherwise specifically stated or limited, the above-described fixed connection is to be understood in a broad sense, and may be, for example, welded, glued, or integrally formed as is conventional in the art.
The above description is only for the preferred embodiment of the present invention, but the scope of the present invention is not limited thereto, and any person skilled in the art should be considered to be within the technical scope of the present invention, and equivalent alternatives or modifications according to the technical solution of the present invention and the inventive concept thereof should be covered by the scope of the present invention.
Claims (6)
1. The utility model provides a many rotor unmanned aerial vehicle of boat wing, includes unmanned organism, its characterized in that, the lower side wall fixedly connected with subassembly case (1) of unmanned organism, be equipped with subassembly board (2) in subassembly case (1), the outer wall fixedly connected with cooling module (3) of subassembly board (2), be equipped with water pipe (4) in cooling module (3), the both ends of water pipe (4) are run through cooling module (3) and are set up, check valve one (8) and check valve two (9) are installed respectively to the both ends of water pipe (4), the one end of water pipe (4) is connected with cooler bin (5), be equipped with the cooling water in cooler bin (5), the other end of water pipe (4) is connected with connecting pipe (6), be connected with pipe (7) between the lower side wall of connecting pipe (6) and cooler bin (5) jointly, be equipped with check valve three (22) in pipe (7), the one end that water pipe (4) were kept away from in connecting pipe (6) slides and inserts and be equipped with connecting rod (10), one end fixedly connected with piston (11) that connecting rod (10) are located water pipe (4), common fixedly connected with cup joints spring (12) on connecting rod (10) outer wall between piston (11) and connecting pipe (6) inner wall, connecting rod (10) are located the outer one end fixedly connected with L type pole (13) of connecting pipe (6), the sawtooth groove has been seted up to the lower lateral wall of L type pole (13), fixedly connected with motor (14) between the last lateral wall of cooler bin (5) passes through, the terminal fixedly connected with of output shaft and the incomplete gear (15) of sawtooth groove engaged with of motor (14).
2. The airship wing multi-rotor Unmanned Aerial Vehicle (UAV) according to claim 1, wherein a heat dissipation plate (18) is installed on the outer wall of the assembly plate (2), and heat dissipation holes (19) opposite to the heat dissipation plate (18) are formed in the outer wall of the assembly box (1).
3. A boatlift multi-rotor drone according to claim 1, wherein the section of the water pipe (4) inside the cooling module (3) is arranged in a continuous loop.
4. The hoverboard multi-rotor drone according to claim 1, characterized in that the end of the L-shaped bar (13) is slidingly inserted with a guide bar (16) fixedly connected to the outer wall of the duct (7).
5. The airship wing multi-rotor Unmanned Aerial Vehicle (UAV) according to claim 1, wherein a plurality of resistance beads (17) are movably embedded in the inner wall of the water pipe (4).
6. The airship wing multi-rotor unmanned aerial vehicle of claim 2, wherein fixing blocks (20) are fixedly connected to four corners of the heat dissipation plate (18), and bolts (21) are screwed to the outer wall of the assembly plate (2) to the outer wall of each fixing block (20).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121990910.0U CN215851916U (en) | 2021-08-20 | 2021-08-20 | Many rotor unmanned aerial vehicle of boat wing |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121990910.0U CN215851916U (en) | 2021-08-20 | 2021-08-20 | Many rotor unmanned aerial vehicle of boat wing |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN215851916U true CN215851916U (en) | 2022-02-18 |
Family
ID=80241694
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202121990910.0U Expired - Fee Related CN215851916U (en) | 2021-08-20 | 2021-08-20 | Many rotor unmanned aerial vehicle of boat wing |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN215851916U (en) |
-
2021
- 2021-08-20 CN CN202121990910.0U patent/CN215851916U/en not_active Expired - Fee Related
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| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20220218 |
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| CF01 | Termination of patent right due to non-payment of annual fee |