CN108357668A - Unmanned plane with propeller heat sinking function - Google Patents
Unmanned plane with propeller heat sinking function Download PDFInfo
- Publication number
- CN108357668A CN108357668A CN201810102296.6A CN201810102296A CN108357668A CN 108357668 A CN108357668 A CN 108357668A CN 201810102296 A CN201810102296 A CN 201810102296A CN 108357668 A CN108357668 A CN 108357668A
- Authority
- CN
- China
- Prior art keywords
- side wall
- end side
- unmanned plane
- propeller
- screw
- 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.)
- Granted
Links
- 230000000694 effects Effects 0.000 claims description 6
- 230000005611 electricity Effects 0.000 claims 1
- 230000017525 heat dissipation Effects 0.000 description 3
- 238000000034 method Methods 0.000 description 3
- 238000001816 cooling Methods 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 230000005855 radiation Effects 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- 239000002699 waste material Substances 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/08—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of power plant cooling systems
- B64D33/10—Radiator arrangement
-
- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05K—PRINTED CIRCUITS; CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS
- H05K7/00—Constructional details common to different types of electric apparatus
- H05K7/20—Modifications to facilitate cooling, ventilating, or heating
- H05K7/20845—Modifications to facilitate cooling, ventilating, or heating for automotive electronic casings
- H05K7/20863—Forced ventilation, e.g. on heat dissipaters coupled to components
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Microelectronics & Electronic Packaging (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Toys (AREA)
Abstract
The invention discloses the unmanned planes with propeller heat sinking function,Including unmanned plane main body,One end side wall of the unmanned plane main body is fixedly connected with link block by screw,One end side wall of the link block is equipped with push-rod electric machine,One end side wall of the push-rod electric machine is connected with the first telescopic rod,One end side wall of the link block is also fixedly connected with mounting blocks by screw,One end side wall of the mounting blocks is welded with rotating device,One end side wall screw of the rotating device is fixed with connecting rod,The upper end side wall riveting of the connecting rod has fixed link,One end side wall of the fixed link is connected with motion bar,The bottom end side wall screw of the motion bar is fixed with the second telescopic rod,One end side wall of the sliding bar is welded with propeller,The energy that the present apparatus can be generated using propeller is that unmanned plane radiates,Not only having saved the energy can also radiate to unmanned plane under different flying heights.
Description
Technical field
The present invention relates to air vehicle technique fields, more particularly to the unmanned plane with propeller heat sinking function.
Background technology
Unmanned plane be with wireless remotecontrol or by itself program control based on not manned aircraft.It succeeding in developing and fighting
Field uses, and has opened with remote attack smart weapon, the new piece that intelligent weapon is leading " untouchable war "
Chapter.And the heat dissipation of unmanned plane now depends on heat dissipation refrigerator, heat dissipation water pump and radiator fan etc. in cooling system, for
The propeller carried on existing unmanned plane is no and cooling system is to being connected, and is generated without rational interests propeller
Wind energy radiates to unmanned plane, makes energy waste.
Invention content
The purpose of the present invention is to solve disadvantages existing in the prior art, and what is proposed has propeller heat sinking function
Unmanned plane.
To achieve the goals above, present invention employs following technical solutions：
One end side wall of unmanned plane with propeller heat sinking function, including unmanned plane main body, the unmanned plane main body passes through spiral shell
Nail is fixedly connected with link block, and one end side wall of the link block is equipped with push-rod electric machine, one end side wall of the push-rod electric machine
It is connected with the first telescopic rod, one end side wall of the link block is also fixedly connected with mounting blocks, the installation by screw
One end side wall of block is welded with rotating device, and one end side wall screw of the rotating device is fixed with connecting rod, the connecting rod
The riveting of upper end side wall there is fixed link, one end side wall of the fixed link to be connected with motion bar, the bottom end of the motion bar
Side wall screw is fixed with the second telescopic rod, and one end side wall of the motion bar is fixedly connected with sliding bar, the sliding bar sliding
It is connected to the inside of sliding rail, one end side wall of the sliding bar is welded with propeller.
Preferably, the surface of the link block offers mounting hole, and the mounting hole is fixedly connected with nobody by screw
Owner's body.
Preferably, one end side wall of the mounting blocks is welded with the first spill spin block, one end side wall of first spill spin block
Rotatable connection has the second spill spin block, the bottom end side wall of second spill spin block to be welded with mounting plate, the one end of the mounting plate
Wall screw is fixed with connecting rod.
Preferably, the surface activity of the fixed link is connected with convex block, and one end side wall of the convex block is fixed with spring, institute
State the inside that spring is located at fixed link.
Preferably, the inside of the sliding rail offers sliding slot, and the internal slide of sliding slot is connected with sliding bar.
Preferably, one end side wall screw of the unmanned plane main body is fixed with radiator fan, and the quantity of radiator fan has
Two.
The beneficial effects of the invention are as follows：
1, of the invention, it is rotated, is made between connecting rod and mounting blocks using rotating device, push-rod electric machine and the first telescopic rod
Its height between unmanned plane main body can be adjusted according to the height that unmanned plane rises by obtaining propeller, so that dissipating
Hot-air fan can be rotated and be radiated down at various height.
2, of the invention, the wind energy generated during unmanned plane during flying by propeller drives turning for radiator fan
It is dynamic, to radiate to unmanned plane main body using radiator fan, may be implemented to generate unmanned plane in flight course in this way
Energy utilized, and saved the energy again.
Description of the drawings
Fig. 1 is the structural schematic diagram of the unmanned plane proposed by the present invention with propeller heat sinking function；
Fig. 2 is the enlarged drawing of the unmanned plane rotating device proposed by the present invention with propeller heat sinking function；
Fig. 3 is the internal structure schematic diagram of the unmanned plane fixed link proposed by the present invention with propeller heat sinking function.
In figure：1 unmanned plane main body, 2 link blocks, 3 mounting holes, 4 push-rod electric machines, 5 first telescopic rods, 6 mounting blocks, 7 rotations
Device, 71 mounting plates, 72 first spill spin blocks, 73 second spill spin blocks, 8 connecting rods, 9 fixed links, 10 convex blocks, 101 springs, 11 activities
Bar, 12 sliding bars, 13 sliding rails, 14 propellers, 15 second telescopic rods, 16 radiator fans.
Specific implementation mode
Following will be combined with the drawings in the embodiments of the present invention, and technical solution in the embodiment of the present invention carries out clear, complete
Site preparation describes, it is clear that described embodiments are only a part of the embodiments of the present invention, instead of all the embodiments.
Referring to Fig.1-3, the unmanned plane with propeller heat sinking function, including unmanned plane main body 1, the one of unmanned plane main body 1
End side wall is fixedly connected with link block 2 by screw, and the surface of link block 2 offers mounting hole 3, and mounting hole 3 is solid by screw
Surely it is connected with unmanned plane main body 1, one end side wall of link block 2 is equipped with push-rod electric machine 4, one end side wall activity of push-rod electric machine 4
It is connected with the first telescopic rod 5, one end side wall of link block 2 is also fixedly connected with mounting blocks 6, one end of mounting blocks 6 by screw
Sidewall weld has rotating device 7, one end side wall of mounting blocks 6 to be welded with the first spill spin block 72, the one end of the first spill spin block 72
Wall rotatable connection has the second spill spin block 73, the bottom end side wall of the second spill spin block 73 to be welded with mounting plate 71, one end of mounting plate 71
Side wall screw is fixed with connecting rod 8, and one end side wall screw of rotating device 7 is fixed with connecting rod 8, utilizes rotating device 7, push rod
Motor 4 and the first telescopic rod 5 rotate between connecting rod 8 and mounting blocks 6 so that propeller 14 can be according on unmanned plane
The height risen adjusts its height between unmanned plane main body 1, so that radiator fan 16 can be in different height
It is rotated and is radiated under degree, the upper end side wall riveting of connecting rod 8 has fixed link 9, the surface activity of fixed link 9 to be connected with convex block
10, one end side wall of convex block 10 is fixed with spring 101, and spring 101 is located at the inside of fixed link 9, and one end side wall of fixed link 9 is lived
Dynamic to be connected with motion bar 11, the bottom end side wall screw of motion bar 11 is fixed with the second telescopic rod 15, one end side wall of motion bar 11
It is fixedly connected with sliding bar 12, the inside of sliding rail 13 offers sliding slot, and the internal slide of sliding slot is connected with sliding bar 12,
One end side wall of sliding bar 12 is welded with propeller 14, and one end side wall screw of unmanned plane main body 1 is fixed with radiator fan 16, and
There are two the quantity of radiator fan 16, and the wind energy that is generated during unmanned plane during flying by propeller 14 drives radiation air
The rotation of fan 16 may be implemented flying to unmanned plane in this way to radiate to unmanned plane main body 1 using radiator fan 16
The energy generated in the process is utilized, and has saved the energy again.
Embodiment：During being radiated to unmanned plane using the propeller 14 of unmanned plane, first according to unmanned plane
The height of flight is come at a distance from determining the propeller 14 of unmanned plane between unmanned plane main body 1, when the flying height of unmanned plane is higher
When, the wind speed of air is also relatively large at this time, can so that the first telescopic rod 5 is extended using push-rod electric machine 4, then sharp again
It is rotated with rotating device 7, mounting plate 71 rotates under the action of rotary electric machine, and mounting plate 71 can drive the second moving block 73 at this time
Rotation, due to being rotation connection between the first moving block 72 and the second moving block 73, so the first moving block 72 and mounting blocks 6
It is motionless so that connecting rod 8 turns to certain angle, and making it, there are one the angle tilts of vertical direction with mounting blocks 6, at this time again
Sliding bar 12 is slided on sliding rail 13, due to the sliding of sliding bar 12, motion bar 11 also can activity be simultaneously in fixed link 9
And fixed with fixed link 9 using convex block 10 and spring 101, and motion bar the second telescopic rods of utilization 15 of page 11 and connecting rod 8
It is fixed, propeller 14 will be rotated to apart from the closer position of unmanned plane main body 1 at this time, in 14 turns of propeller
When dynamic, propeller 14 can generate wind energy due to rotation, to which wind energy can drive radiator fan 16 right in ceaselessly rotation
It radiates afterwards to unmanned plane main body 1.
The foregoing is only a preferred embodiment of the present invention, but scope of protection of the present invention is not limited thereto,
Any one skilled in the art in the technical scope disclosed by the present invention, according to the technique and scheme of the present invention and its
Inventive concept is subject to equivalent substitution or change, should be covered by the protection scope of the present invention.
Claims (6)
1. the unmanned plane with propeller heat sinking function, including unmanned plane main body（1）, which is characterized in that the unmanned plane main body
（1）One end side wall link block is fixedly connected with by screw（2）, the link block（2）One end side wall be equipped with push rod electricity
Machine（4）, the push-rod electric machine（4）One end side wall be connected with the first telescopic rod（5）, the link block（2）One end
Wall is also fixedly connected with mounting blocks by screw（6）, the mounting blocks（6）One end side wall be welded with rotating device（7）, described
Rotating device（7）One end side wall screw be fixed with connecting rod（8）, the connecting rod（8）The riveting of upper end side wall have fixed link
（9）, the fixed link（9）One end side wall be connected with motion bar（11）, the motion bar（11）Bottom end side wall screw
It is fixed with the second telescopic rod（15）, the motion bar（11）One end side wall be fixedly connected with sliding bar（12）, the sliding bar
（12）It is slidably connected at sliding rail（13）Inside, the sliding bar（12）One end side wall be welded with propeller（14）.
2. the unmanned plane according to claim 1 with propeller heat sinking function, which is characterized in that the link block（2）
Surface offer mounting hole（3）, the mounting hole（3）It is fixedly connected with unmanned plane main body by screw（1）.
3. the unmanned plane according to claim 1 with propeller heat sinking function, which is characterized in that the mounting blocks（6）
One end side wall be welded with the first spill spin block（72）, first spill spin block（72）The rotatable connection of one end side wall have the second rotation
Block（73）, second spill spin block（73）Bottom end side wall be welded with mounting plate（71）, the mounting plate（71）One end side wall
Screw is fixed with connecting rod（8）.
4. the unmanned plane according to claim 1 with propeller heat sinking function, which is characterized in that the fixed link（9）
Surface activity be connected with convex block（10）, the convex block（10）One end side wall be fixed with spring（101）, the spring（101）
Positioned at fixed link（9）Inside.
5. the unmanned plane according to claim 1 with propeller heat sinking function, which is characterized in that the sliding rail
（13）Inside offer sliding slot, and the internal slide of sliding slot is connected with sliding bar（12）.
6. the unmanned plane according to claim 1 with propeller heat sinking function, which is characterized in that the unmanned plane main body
（1）One end side wall screw be fixed with radiator fan（16）, and radiator fan（16）Quantity there are two.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810102296.6A CN108357668B (en) | 2018-02-01 | 2018-02-01 | Unmanned aerial vehicle with screw heat dissipation function |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810102296.6A CN108357668B (en) | 2018-02-01 | 2018-02-01 | Unmanned aerial vehicle with screw heat dissipation function |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN108357668A true CN108357668A (en) | 2018-08-03 |
| CN108357668B CN108357668B (en) | 2022-04-22 |
Family
ID=63004250
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810102296.6A Active CN108357668B (en) | 2018-02-01 | 2018-02-01 | Unmanned aerial vehicle with screw heat dissipation function |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108357668B (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115367036A (en) * | 2022-09-15 | 2022-11-22 | 重庆荣爵科技有限公司 | Motorcycle frame |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB385789A (en) * | 1931-04-17 | 1933-01-05 | Denis Remy Campens | Improvements in or relating to helicopters |
| CN104044725A (en) * | 2014-07-01 | 2014-09-17 | 国家电网公司 | Unmanned plane |
| CN205770144U (en) * | 2016-05-27 | 2016-12-07 | 中国科学院光电研究院 | A kind of dynamical system of rotor craft |
| US20170181330A1 (en) * | 2014-09-16 | 2017-06-22 | SZ DJI Technology Co., Ltd. | Heat dissipation device and uav using the same |
| CN107054650A (en) * | 2017-03-29 | 2017-08-18 | 武汉商学院 | Four rotor wing unmanned aerial vehicles for food delivery |
| CN206623983U (en) * | 2017-04-10 | 2017-11-10 | 河南省酷农航空植保科技有限公司 | Plant protection unmanned plane high-cooling property horn |
-
2018
- 2018-02-01 CN CN201810102296.6A patent/CN108357668B/en active Active
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB385789A (en) * | 1931-04-17 | 1933-01-05 | Denis Remy Campens | Improvements in or relating to helicopters |
| CN104044725A (en) * | 2014-07-01 | 2014-09-17 | 国家电网公司 | Unmanned plane |
| US20170181330A1 (en) * | 2014-09-16 | 2017-06-22 | SZ DJI Technology Co., Ltd. | Heat dissipation device and uav using the same |
| CN205770144U (en) * | 2016-05-27 | 2016-12-07 | 中国科学院光电研究院 | A kind of dynamical system of rotor craft |
| CN107054650A (en) * | 2017-03-29 | 2017-08-18 | 武汉商学院 | Four rotor wing unmanned aerial vehicles for food delivery |
| CN206623983U (en) * | 2017-04-10 | 2017-11-10 | 河南省酷农航空植保科技有限公司 | Plant protection unmanned plane high-cooling property horn |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115367036A (en) * | 2022-09-15 | 2022-11-22 | 重庆荣爵科技有限公司 | Motorcycle frame |
| CN115367036B (en) * | 2022-09-15 | 2024-02-23 | 重庆荣爵科技有限公司 | Motorcycle frame |
Also Published As
| Publication number | Publication date |
|---|---|
| CN108357668B (en) | 2022-04-22 |
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