CN209270816U - A kind of small-sized solar aeromodelling airplane - Google Patents
A kind of small-sized solar aeromodelling airplane Download PDFInfo
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- CN209270816U CN209270816U CN201822140181.4U CN201822140181U CN209270816U CN 209270816 U CN209270816 U CN 209270816U CN 201822140181 U CN201822140181 U CN 201822140181U CN 209270816 U CN209270816 U CN 209270816U
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- casing
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- blade
- aeromodelling airplane
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Abstract
The utility model discloses a kind of small-sized solar aeromodelling airplanes, including casing, four pieces of arc-shaped solar panels are provided with outside casing, solar panel is connect with current voltage regulator and battery, casing quadrangle is provided with rotor bracket, rotating bar is provided with by mounting base on rotor bracket, rotating bar upper end is provided with blade mounting base, blade mounting base both ends are provided with blade, and it is provided with balancing device, balancing device includes balancing pole, balancing pole is arranged in blade mounting base, balancing pole both sides are provided with counter weight device, and both ends are provided with balance paddle, casing is provided with several first springs, rotor bracket is provided with second spring, anti- billiards is provided on first spring and the first spring, several stabilizer blades are provided with below casing, controller is additionally provided in casing, controller and remote controler communicate to connect.The utility model solves the problems, such as that cruise duration is short, balance is not easy to grasp and collsion damage model plane influence service life.
Description
Technical field
The utility model belongs to aeromodelling airplane technical field, and in particular to arrives a kind of small-sized solar aeromodelling airplane.
Background technique
Aeromodelling airplane is taking photo by plane, agricultural, plant protection, miniature self-timer, is observing wild animal, news report, electric inspection process at present
With the application in the fields such as movies-making, the purposes of aeromodelling airplane itself is greatly expanded, country also answers in actively extension industry
With with develop the technology.But the electricity of aeromodelling airplane accumulators store is limited, causes the flight time shorter, limits unmanned plane
Using further development；The balance of aeromodelling airplane all leans on the manual force of airplane hobbyist to control, therefore operationally has
There is very big difficulty for beginner in high requirement, meanwhile, model plane are all to bring rising by the high speed rotation of blade
Power, powerful centrifugal force bring acid test to the go to action of aeromodelling airplane again, and aeromodelling airplane may also be because of turning to
When fallen out because powerful centrifugal force acts on disequilibrium, so that the safety of its manipulator and body itself is on the hazard；And flying
During row, sometimes due to being unfamiliar with to geographical location or misoperation, it may occur that collision, to a variety of precisions in fuselage
Components cause to damage, and influence its service life.
Utility model content
In view of the above deficiencies, the utility model provides a kind of small-sized solar aeromodelling airplane, efficiently solves cruise duration
The problem of short, balance is not easy to grasp and collsion damage model plane influence service life.
To achieve the above object, the technical scheme adopted by the utility model to solve the technical problem is as follows: providing a kind of small
Type solar energy aeromodelling airplane, including casing, casing is arc-shaped, and casing internal is provided with current voltage regulator, battery and several electricity
Machine, is provided with four pieces of dismountable arc-shaped solar panels outside casing, solar panel successively with current voltage regulator and
Battery connection, the centrosymmetric quadrangle of casing are provided with rotor bracket, solar panel are also equipped on rotor bracket, revolve
Rotating bar is provided with by mounting base on wing support, rotating bar upper end is provided with blade mounting base, blade installation by mounting hole
Seat is S-shaped, and both ends are provided with blade, and rotating bar is connect with motor output end, vertical blade direction setting in blade mounting base
There is balancing device, balancing device includes balancing pole, and balancing pole is arranged in blade mounting base, and balancing pole both sides are provided with refitting
It sets, and both ends are provided with balance paddle, several first springs is provided at casing edge center, rotor bracket outer end is provided with second
Spring is provided with anti-billiards on the first spring and second spring, is provided with several stabilizer blades below casing, is additionally provided in casing
Controller, controller are connect with battery and motor, and controller is communicated to connect by transmitting probe and receiving transducer and remote controler.
The beneficial effects of the utility model are: assigning instruction, controller starting electricity by controller of the remote controler to aircraft
Machine drives blade rotation by rotating bar, and manipulation aircraft flies, and after the completion of flight, control aircraft is dropped using stabilizer blade
It falling, solar panel is collected solar energy and is stored in battery after photoelectric conversion, for being used when flight, the casing of arc
It can reduce air drag with solar panel, increase the cruising ability of aircraft, improve flight reappearance；It is provided with balance dress
It sets, operation requirement of the aeromodelling airplane to balance can be reduced, by the cooperation of counter weight device and balance paddle and centrosymmetric
The effect of four balancing devices makes aeromodelling airplane automatically keep balance in flight and steering, flies more steady, prevents
Safety accident；On casing and it is respectively arranged with the first spring and second spring on rotor bracket, is equipped with anti-billiards, it can be careless
When colliding with object, using the buffer function of anticollision ball and spring, the damage that collision generates is prevented or slowed down, protects body
It preserves from, prolongs its service life.
Further, electron speed regulator is provided on motor, electron speed regulator is connect with controller.
Beneficial effect using above-mentioned further scheme is: by adjusting electron speed regulator, motor rotation speed is adjusted, from
And the flying speed of aeromodelling airplane is controlled, achieve the purpose that real-time monitoring flying speed.
Further, electric quantity metering chip is provided on battery, electric quantity metering chip is connect with controller.
Beneficial effect using above-mentioned further scheme is: electric quantity metering chip it can be concluded that battery real time electrical quantity,
Reasonable planning distribution is made to the aircraft of model plane, prevents not enough power supply and falls suddenly, damage model plane.
Further, solar panel is three-stage.
Beneficial effect using above-mentioned further scheme is: three-stage solar battery is conducive to the collection of electric current, increases
The electricity of solar power generation stores more energy in battery.
Further, bracket reinforcing plate is provided on rotor bracket.
Beneficial effect using above-mentioned further scheme is: bracket reinforcing plate can reinforce the intensity and stabilization of rotor bracket
Property, shake is prevented, keeps flight more steady.
Further, rubber pad is provided on stabilizer blade.
Beneficial effect using above-mentioned further scheme is: rubber pad can mitigate the shake generated when landing, play slow
Punching effect, protection aeromodelling airplane are injury-free.
Further, GPS positioning plate is provided in casing.
Beneficial effect using above-mentioned further scheme is: GPS positioning plate can position the position of aeromodelling airplane in real time, to
Operator feeds back, and prevents phenomena such as model plane are missing, collide or be strayed into no-fly zone.
Detailed description of the invention
Fig. 1 is the schematic diagram of the utility model；
Fig. 2 is the top view of the utility model；
Fig. 3 is the schematic diagram of balancing device；
Wherein, 1, casing；2, solar panel；3, stabilizer blade；4, the first spring；5, rotor bracket；6, second spring；7,
Anti- billiards；8, blade；9, balancing device；10, blade mounting base；11, mounting hole；12, balancing pole；13, counter weight device；14, it puts down
Weigh paddle.
Specific embodiment
Specific embodiment of the present utility model is described in detail with reference to the accompanying drawing.
In one embodiment of the utility model, as shown in Figure 1-3, providing a kind of small-sized solar aeromodelling airplane, wrap
Casing 1 is included, casing 1 is arc-shaped, and casing 1 is internally provided with TLV705 type current voltage regulator, battery and several SN-112 types electricity
Machine, is provided with four pieces of dismountable arc-shaped solar panels 2 outside casing 1, solar panel 2 successively with current voltage regulator
It is connected with battery, solar panel 2 is collected solar energy and is stored in battery after photoelectric conversion, for making when flight
With the casing 1 and solar panel 2 of arc can reduce air drag, increase the cruising ability of aircraft, improve flight matter
Amount；The centrosymmetric quadrangle of casing 1 is provided with rotor bracket 5, and solar panel, rotor bracket are also equipped on rotor bracket
Rotating bar is provided with by mounting base on 5, rotating bar upper end is provided with blade mounting base 10, blade mounting base by mounting hole 11
10 is S-shaped, and both ends are provided with blade 8, and rotating bar is connect with motor output end, 8 direction of vertical blade in blade mounting base 10
It is provided with balancing device 9, balancing device 9 includes balancing pole 12, and balancing pole 12 is arranged in blade mounting base 10, and 12 liang of balancing pole
While being provided with counter weight device 13, counter weight device 13 can be clump weight, and clump weight plays balanced action, and both ends are provided with balance paddle
14, the balancing device 9 of setting can reduce operation requirement of the aeromodelling airplane to balance, pass through counter weight device 13 and balance paddle 14
Cooperation and centrosymmetric four balancing devices effect, so that aeromodelling airplane is automatically kept balance in flight and steering,
It flies more steady, prevents safety accident；Several first springs 4 are provided at 1 edge center of casing, outside rotor bracket 5
End is provided with second spring 6, and anti-billiards 7 is provided on the first spring 4 and second spring 6, can occur accidentally with object
When collision, using the buffer function of anti-billiards 7 and spring, the damage that collision generates is prevented or slowed down, protection body preserves from,
It prolongs its service life；It is provided with several stabilizer blades 3 below casing 1, is additionally provided with controller in casing 1, controller is
STM32F103ZET6 type single-chip microcontroller, controller are connect with battery and motor, controller by transmitting probe and receiving transducer with
Remote controler communication connection, transmitting probe model OMP40-2, receiving transducer model OMP40-3, by remote controler to aircraft
Controller assigns instruction, and controller starts motor, drives blade 8 to rotate by rotating bar, and manipulation aircraft flies, and has flown
Cheng Hou, control aircraft are landed using stabilizer blade 3.
Electron speed regulator, electron speed regulator model ATV11-WK are provided on motor, electron speed regulator and controller connect
It connects, by adjusting electron speed regulator, adjusts motor rotation speed to control the flying speed of aeromodelling airplane and reach real-time tune
Control the purpose of flying speed；Electric quantity metering chip is provided on battery, electric quantity metering chip model is CS5463, electric quantity metering
Chip is connect with controller, electric quantity metering chip it can be concluded that battery real time electrical quantity, the aircraft of model plane is made reasonably
Planning distribution, prevents not enough power supply and falls suddenly, damages model plane；Solar panel 2 is three-stage, three-stage solar energy
Solar panel 2 is conducive to the collection of electric current, increases the electricity of solar power generation, and more energy are stored in battery；Rotor branch
Bracket reinforcing plate is provided on frame 5, bracket reinforcing plate can reinforce the strength and stability of rotor bracket 5, shake is prevented,
Keep flight more steady；Rubber pad is provided on stabilizer blade 3, rubber pad can mitigate the shake generated when landing, play buffering and make
With protection aeromodelling airplane is injury-free；GPS positioning plate is provided in casing 1, GPS positioning plate model GPS15X-W, GPS is fixed
Position plate can position the position of aeromodelling airplane in real time, feed back to operator, prevent model plane and be missing, collide or be strayed into
Phenomena such as no-fly zone.
In use, solar panel 2 is converted solar energy into electrical energy and is stored in battery, it is distant for being used when flight
Control device transmission signal makes controller start motor, and rotating bar drives blade 8 to rotate, and adjusts electron speed regulator and adjusts flying speed,
Balance is automatically kept in the case where counter weight device 13 and balance paddle 14 act on, prevents unstable phenomenon, while being equipped with the GPS positioning plate palm
Aeromodelling airplane situation is held, if colliding accidentally, using the buffer function of anti-billiards 7 and spring, protects body not by big
Damage, after the completion of flight, landed using stabilizer blade 3, rubber pad is buffered, and when not flight can also store up under illumination condition
Deposit electric energy.The utility model efficiently solve cruise duration it is short, balance be not easy grasp and collsion damage model plane influence service life
The problem of.
Although being described in detail in conjunction with attached drawing to specific embodiment of the present utility model, should not be construed as pair
The restriction of the protection scope of this patent.In range described by claims, those skilled in the art are without creative labor
The dynamic various modifications that can be made and deformation still belong to the protection scope of this patent.
Claims (7)
1. a kind of small-sized solar aeromodelling airplane, which is characterized in that including casing (1), the casing (1) is arc-shaped, the machine
Shell (1) is internally provided with current voltage regulator, battery and several motors, and four pieces are provided with outside the casing (1) removably
Arc-shaped solar panel (2), the solar panel (2) successively connect with the current voltage regulator and the battery,
The centrosymmetric quadrangle of the casing (1) is provided with rotor bracket (5), is also equipped with the sun on the rotor bracket (5)
Can solar panel (2), rotating bar is provided with by mounting base on the rotor bracket (5), the rotating bar upper end passes through mounting hole
(11) it is provided with blade mounting base (10), the blade mounting base (10) is S-shaped, and both ends are provided with blade (8), the rotation
Bar is connect with the motor output end, and vertical blade (8) direction is provided with balancing device on the blade mounting base (10)
(9), the balancing device (9) includes balancing pole (12), and the balancing pole (12) is arranged on the blade mounting base (10), institute
It states balancing pole (12) both sides to be provided with counter weight device (13), and both ends are provided with balance paddle (14), casing (1) edge center
Place is provided with several first springs (4), and rotor bracket (5) outer end is provided with second spring (6), first spring (4)
With anti-billiards (7) are provided on the second spring (6), be provided with several stabilizer blades (3), the machine below the casing (1)
It is additionally provided with controller in shell (1), the controller is connect with the battery and the motor, and the controller passes through transmitting
Probe and receiving transducer and remote controler communicate to connect.
2. small-sized solar aeromodelling airplane as described in claim 1, which is characterized in that be provided with electronic speed regulation on the motor
Device, the electron speed regulator are connect with the controller.
3. small-sized solar aeromodelling airplane as described in claim 1, which is characterized in that be provided with voltameter on the battery
Chip is measured, the electric quantity metering chip is connect with the controller.
4. small-sized solar aeromodelling airplane as described in claim 1, which is characterized in that the solar panel (2) is three
Segmentation.
5. small-sized solar aeromodelling airplane as described in claim 1, which is characterized in that be provided on the rotor bracket (5)
Bracket reinforcing plate.
6. small-sized solar aeromodelling airplane as described in claim 1, which is characterized in that be provided with rubber on the stabilizer blade (3)
Pad.
7. small-sized solar aeromodelling airplane as described in claim 1, which is characterized in that it is fixed to be provided with GPS in the casing (1)
Position plate.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201822140181.4U CN209270816U (en) | 2018-12-19 | 2018-12-19 | A kind of small-sized solar aeromodelling airplane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201822140181.4U CN209270816U (en) | 2018-12-19 | 2018-12-19 | A kind of small-sized solar aeromodelling airplane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209270816U true CN209270816U (en) | 2019-08-20 |
Family
ID=67611868
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201822140181.4U Expired - Fee Related CN209270816U (en) | 2018-12-19 | 2018-12-19 | A kind of small-sized solar aeromodelling airplane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN209270816U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112781550A (en) * | 2020-12-30 | 2021-05-11 | 镇江市勘察测绘研究院 | Unmanned aerial vehicle-based terrain mapping method for mine pit landform |
-
2018
- 2018-12-19 CN CN201822140181.4U patent/CN209270816U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112781550A (en) * | 2020-12-30 | 2021-05-11 | 镇江市勘察测绘研究院 | Unmanned aerial vehicle-based terrain mapping method for mine pit landform |
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Legal Events
| 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: 20190820 Termination date: 20211219 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |