CN104307183A - Solar model airplane - Google Patents
Solar model airplane Download PDFInfo
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- CN104307183A CN104307183A CN201410621506.4A CN201410621506A CN104307183A CN 104307183 A CN104307183 A CN 104307183A CN 201410621506 A CN201410621506 A CN 201410621506A CN 104307183 A CN104307183 A CN 104307183A
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- airplane
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- flying
- solar
- model airplane
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Abstract
The invention provides a solar model airplane which is characterized by comprising an airplane body, wings and a tail fin. The wings are wide flying wings. Solar panels are arranged on the upper surfaces of the wings. Storage batteries are arranged on the lower surface of the airplane body, and bulbs connected with the storage batteries are arranged at the edges of the wings. The solar model airplane can generate large buoyancy when flying in the air due to the large flying wings, and therefore the solar model airplane can fly stably, has a good flying effect and long flying distance, can save energy, and provides feasibility for bearing the solar panels. In addition, thanks to sound equipment and the bulbs, the application range of the solar model airplane is greatly enlarged that the solar model airplane can enter narrow space to transmit sounds and light sources. When the storage batteries are connected with a power system of the airplane to serve as a reserve power supply, the endurance of the airplane during every flying can be prolonged.
Description
Technical field
The invention belongs to aeromodelling airplane field, relate generally to a kind of solar energy aeromodelling airplane.
Background technology
At present, the aeromodelling airplane of domestic production, the wing of aircraft is all less, so be not suitable for carrying solar panel, the equipment that aircraft is carried is very limited.
Summary of the invention
Technical problem to be solved by this invention be to provide a kind ofly to have a smooth flight, solar energy aeromodelling airplane with sound device, bulb.
The present invention is achieved through the following technical solutions:
A kind of solar energy aeromodelling airplane, it is characterized in that, comprise fuselage, wing, empennage, described wing is wider all-wing aircraft type, at the upper surface of described wing, be provided with solar panel, below fuselage, be provided with battery, at the edge of wing, be provided with bulb, bulb is connected with battery.
As preferably, below described fuselage, be also provided with the sound equipment be connected with battery.
Further, also can being connected with the dynamical system of aircraft of described battery, the effect of stand-by power supply is played.
Beneficial effect of the present invention: aeromodelling airplane of the present invention, because adopt larger all-wing aircraft type wing, larger buoyancy is produced aloft when can fly, make to have a smooth flight, flight effect is good, flying distance is far away, economize energy, for carrying solar energy electroplax plate provides feasibility, in addition, because have sound equipment and bulb, the scope of application of the model of an airplane can be made greatly to improve, sound, light source etc. is transmitted for entering crawl space, when battery is connected with the dynamical system of aircraft, play the effect of stand-by power supply, the cruising time that aircraft is each can be extended.
Accompanying drawing explanation
Examples of the present invention will be described by way of reference to the accompanying drawings, wherein:
Fig. 1 is the top view of model plane aircaft configuration schematic diagram in the embodiment of the present invention;
Fig. 2 be in the embodiment of the present invention model plane aircaft configuration schematic diagram front view.
Detailed description of the invention
Arbitrary feature disclosed in this description, unless specifically stated otherwise, all can be replaced by other equivalences or the alternative features with similar object.That is, unless specifically stated otherwise, each feature is an example in a series of equivalence or similar characteristics.
As illustrated in fig. 1 and 2, a kind of solar energy aeromodelling airplane, is characterized in that, comprise fuselage 1, wing 2, empennage 3, described wing 2 is wider all-wing aircraft type, at the upper surface of described wing 2, be provided with solar panel 4, below fuselage 1, be provided with battery, at the edge of wing 2, be provided with bulb 6, bulb 6 is connected with battery 5.Below described fuselage 1, be also provided with the sound equipment be connected with battery 5.Also can being connected with the dynamical system of aircraft of described battery 5, play the effect of stand-by power supply.
Aeromodelling airplane of the present invention, because adopt larger all-wing aircraft type wing, larger buoyancy is produced aloft when can fly, make to have a smooth flight, flight effect is good, flying distance is far away, economize energy, for carrying solar energy electroplax plate provides feasibility, in addition, because have sound equipment and bulb, the scope of application of the model of an airplane can be made greatly to improve, sound, light source etc. is transmitted for entering crawl space, when battery is connected with the dynamical system of aircraft, play the effect of stand-by power supply, the cruising time that aircraft is each can be extended.
The present invention is not limited to aforesaid detailed description of the invention.The present invention expands to any new feature of disclosing in this manual or any combination newly, and the step of the arbitrary new method disclosed or process or any combination newly.
Claims (3)
1. a solar energy aeromodelling airplane, it is characterized in that, comprise fuselage (1), wing (2), empennage (3), described wing (2) is wider all-wing aircraft type, at the upper surface of described wing (2), be provided with solar panel (4), below fuselage (1), be provided with battery, at the edge of wing (2), be provided with bulb (6), bulb (6) is connected with battery (5).
2. solar energy aeromodelling airplane according to claim 1, is characterized in that, below described fuselage (1), is also provided with the sound equipment (7) be connected with battery (5).
3. solar energy aeromodelling airplane according to claim 1, is characterized in that, also can being connected with the dynamical system of aircraft of described battery (5), plays the effect of stand-by power supply.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410621506.4A CN104307183A (en) | 2014-11-07 | 2014-11-07 | Solar model airplane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410621506.4A CN104307183A (en) | 2014-11-07 | 2014-11-07 | Solar model airplane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN104307183A true CN104307183A (en) | 2015-01-28 |
Family
ID=52362578
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410621506.4A Pending CN104307183A (en) | 2014-11-07 | 2014-11-07 | Solar model airplane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN104307183A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104815444A (en) * | 2015-04-08 | 2015-08-05 | 王超群 | Remote control aircraft |
-
2014
- 2014-11-07 CN CN201410621506.4A patent/CN104307183A/en active Pending
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104815444A (en) * | 2015-04-08 | 2015-08-05 | 王超群 | Remote control aircraft |
| CN104815444B (en) * | 2015-04-08 | 2017-03-01 | 王超群 | A kind of telecontrolled aircraft |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| WD01 | Invention patent application deemed withdrawn after publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20150128 |