CN206910801U - One kind folds model aircraft - Google Patents
One kind folds model aircraft Download PDFInfo
- Publication number
- CN206910801U CN206910801U CN201720888408.6U CN201720888408U CN206910801U CN 206910801 U CN206910801 U CN 206910801U CN 201720888408 U CN201720888408 U CN 201720888408U CN 206910801 U CN206910801 U CN 206910801U
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- CN
- China
- Prior art keywords
- wing
- fuselage
- model aircraft
- empennage
- wing plate
- 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.)
- Expired - Fee Related
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Abstract
The utility model discloses one kind to fold model aircraft, including fuselage, the wing and empennage that are connected with fuselage；Wing includes wing plate and wing tip；Wing plate and wing tip are movably connected by connector；Two wing plate sides are equipped with propeller；Fuselage is connected by connector with empennage；On the surface of empennage and wing covered with a layer solar cell plate；Controller is provided with fuselage；Controller is connected by the anti-overcharge electric module of anti-reverse charging with solar panel；Controller electrically connects with battery, overcurrent protector, rectification filtering module, the second voltage-stablizer, transformer and propeller successively.The utility model by installing torsion spring on wing and fuselage, realizes the foldability of model aircraft, and the installation of solar panel, adds the endurance of model aircraft by cleverly conceiving, and has stronger practicality.
Description
Technical field
The utility model belongs to the technical field of model aircraft, and in particular to one kind folds model aircraft.
Background technology
In recent years, the rise of the model of an airplane, various aircrafts emerge in an endless stream, and wherein assembled model aircraft is deep by joyous
Meet, but be difficult to remove again after assembled completion, it is not easy to carry, except this, assembled model aircraft power consumption is larger, does not have
There is endurance.
Utility model content
The purpose of this utility model is in view of the shortcomings of the prior art, there is provided one kind folds model aircraft, to solve to fly
Machine model is not portable and the problem of endurance difference.
To reach above-mentioned purpose, the utility model adopts the technical scheme that：
One kind folds model aircraft, including fuselage, the wing and empennage that are connected with fuselage；Wing includes wing plate and wing tip；
Wing plate and wing tip are movably connected by connector；Two wing plate sides are equipped with propeller；Fuselage passes through connector and empennage phase
Even；On the surface of empennage and wing covered with a layer solar cell plate；Controller is provided with fuselage；Controller passes through anti-reverse charging
Anti-overcharge electric module is connected with solar panel；Controller successively with battery, overcurrent protector, rectification filtering module,
Two voltage-stablizers, transformer and propeller electrical connection.
Preferably, the anti-overcharge electric module of anti-reverse charging is the anti-reverse charging diode and overcharge discharger being arranged in parallel.
Preferably, battery, overcurrent protector, rectification filtering module, the second voltage-stablizer and transformer are in fuselage.
Preferably, fuselage side is provided with some indicator lamps；The indicator lamp is connected by the first voltage-stablizer with controller.
Preferably, connector includes the torsion spring and rolling bearing of angle [alpha] between regulation wing plate and wing tip；In wing plate and wing tip
On be equipped with the connecting rods of some fixed connection strings.
Preferably, angle [alpha] is 0 ° -25 ° between wing plate and wing tip.
Preferably, the surface area ratio of the surface area of wing and fuselage is 3:1.
Folding model aircraft provided by the utility model, has the advantages that：
Wing is made up of wing plate and wing tip, and wing plate and wing tip are movably connected by torsion spring and rolling bearing, and wing tip can be in the wing
Rotary folding on plate, except this, empennage can also realize folding.In assembling, the angle between selection wing tip and wing plate need to be only adjusted,
The elastic force of torsion spring is born by connecting rope, wing plate is connected with wing tip.Covered with a layer solar cell on fuselage and wing
Plate, power storage is converted light energy into battery, the use for propeller is used, and adds the continuation of the journey energy of model aircraft
Power.
The utility model is by cleverly conceiving, and by installing torsion spring on wing and fuselage, that realizes model aircraft can
Folding property, and the installation of solar panel, the endurance of model aircraft is added, there is stronger practicality.
Brief description of the drawings
Fig. 1 is the structural representation for folding model aircraft.
Fig. 2 is folding model aircraft rearview.
Fig. 3 is folding model aircraft wing structure figure.
Fig. 4 is folding model aircraft solar panel operation principle block diagram.
Wherein, 1, fuselage；2nd, wing；3rd, empennage；4th, propeller；5th, connector；6th, wing plate；7th, wing tip；8th, indicator lamp；
51st, torsion spring；52nd, connecting rod；53rd, connecting rope；54th, rolling bearing.
Embodiment
Specific embodiment of the present utility model is described below, in order to which those skilled in the art understand
The utility model, it should be apparent that the utility model is not limited to the scope of embodiment, to the common skill of the art
For art personnel, if various change in the spirit and scope of the present utility model that appended claim limits and determines,
These changes are it will be apparent that all are created in the row of protection using the utility model of the utility model design.
According to one embodiment of the application, as Figure 1-4, including fuselage 1, the wing 2 and empennage that are connected with fuselage 1
3。
Wing 2 includes wing plate 6 and wing tip 7, and wing plate 6 and wing tip 7 are movably connected by connector 5, and two sides of wing plate 6 are equal
One propeller 4 is installed, propeller 4 is connected with the motor inside fuselage 1.It is provided with the junction of wing plate 6 and wing tip 7
Torsion spring 51 and rolling bearing 54, in its natural state, wing tip 7 are close to wing plate 6, the i.e. folding of wing tip 7 under the elastic force effect of torsion spring 51
It is laminated on wing plate 6, except this, multiple connecting rods 52 is provided with wing plate 6 and wing tip 7, connecting rope 53 connects corresponding connecting rod 52,
The expansion between wing plate 6 and wing tip 7, and adjustable angle [alpha] between wing plate 6 and wing tip 7 are realized, in the range of 0 ° -25 °.Wing 2
The surface area ratio of surface area and fuselage 1 be 3:1, and α presence improves the lift-drag ratio of wing 2, increases wing 2
Stalling angle.
Except this, the annexation between fuselage 1 and empennage 3 is identical between wing tip 7 and wing plate 6.
On the surface of empennage 3 and wing 2 covered with a layer solar cell plate, fuselage 1 is interior to be provided with controller, and controller leads to
The anti-overcharge electric module of anti-reverse charging is crossed to be connected with solar panel, controller successively with battery, overcurrent protector, rectifying and wave-filtering
Module, the second voltage-stablizer, transformer and propeller 4 electrically connect.Wherein, the anti-overcharge electric module of anti-reverse charging is the counnter attack being arranged in parallel
Diode and overcharge discharger are filled, battery, overcurrent protector, rectification filtering module, the second voltage-stablizer and transformer are all provided with
In in fuselage 1.Some indicator lamps 8 of the side of fuselage 1 are connected by the first voltage-stablizer with controller.
The anti-overcharge electric module of anti-reverse charging is the anti-reverse charging diode and overcharge discharger being arranged in parallel, the pole of anti-reverse charging two
Pipe, can avoid solar panel 2 from the problem of short trouble occur when not generating electricity rainy days and night；Overcharge discharger is prevented
Only cause a large amount of outlets of battery because of overcharge, the problem of causing moisture loss and active material to come off, while prevent because of mistake
The problem of discharging and accelerating the corrosion of accumulator grid and irreversible sulphation, and then protect battery not put by overcharge and excessively
The infringement of electricity.The use of solar panel, add the endurance of model aircraft.
The utility model, by installing torsion spring 51 on wing 2 and fuselage 1, realizes model aircraft by cleverly conceiving
Foldability, and the installation of solar panel adds the endurance of model aircraft, has stronger practicality.
Although being described in detail with reference to accompanying drawing to the embodiment of utility model, should not be construed as to this
The restriction of the protection domain of patent.In the scope described by claims, those skilled in the art are without creative work
The various modification and variation that can be made still belong to the protection domain of this patent.
Claims (7)
1. one kind folds model aircraft, it is characterised in that：The wing and empennage being connected including fuselage, with fuselage；The wing bag
Include wing plate and wing tip；The wing plate and wing tip are movably connected by connector；Two wing plate sides are equipped with propeller；Institute
Fuselage is stated by connector with empennage to be connected；On the surface of the empennage and wing covered with a layer solar cell plate；It is described
Controller is provided with fuselage；The controller is connected by the anti-overcharge electric module of anti-reverse charging with solar panel；The control
Device electrically connects with battery, overcurrent protector, rectification filtering module, the second voltage-stablizer, transformer and propeller successively.
2. folding model aircraft according to claim 1, it is characterised in that：The anti-overcharge electric module of anti-reverse charging is parallel connection
The anti-reverse charging diode and overcharge discharger of setting.
3. folding model aircraft according to claim 1, it is characterised in that：The battery, overcurrent protector, rectification filter
Ripple module, the second voltage-stablizer and transformer are in fuselage.
4. folding model aircraft according to claim 1, it is characterised in that：The fuselage side is provided with some indicator lamps；
The indicator lamp is connected by the first voltage-stablizer with controller.
5. folding model aircraft according to claim 1, it is characterised in that：The connector includes regulation wing plate and wing tip
Between angle [alpha] torsion spring and rolling bearing；The connecting rod of some fixed connection strings is equipped with the wing plate and wing tip.
6. folding model aircraft according to claim 5, it is characterised in that：Between the wing plate and wing tip angle [alpha] be 0 °-
25°。
7. folding model aircraft according to claim 1, it is characterised in that：The surface area of the wing and the surface of fuselage
The ratio between product is 3:1.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720888408.6U CN206910801U (en) | 2017-07-21 | 2017-07-21 | One kind folds model aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720888408.6U CN206910801U (en) | 2017-07-21 | 2017-07-21 | One kind folds model aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206910801U true CN206910801U (en) | 2018-01-23 |
Family
ID=61348053
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720888408.6U Expired - Fee Related CN206910801U (en) | 2017-07-21 | 2017-07-21 | One kind folds model aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206910801U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109331479A (en) * | 2018-11-28 | 2019-02-15 | 佛山科学技术学院 | A kind of adjustable model aircraft of plate type assembled |
-
2017
- 2017-07-21 CN CN201720888408.6U patent/CN206910801U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109331479A (en) * | 2018-11-28 | 2019-02-15 | 佛山科学技术学院 | A kind of adjustable model aircraft of plate type assembled |
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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 | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20180123 Termination date: 20190721 |