CN205730364U - A kind of solar energy aeromodelling airplane - Google Patents
A kind of solar energy aeromodelling airplane Download PDFInfo
- Publication number
- CN205730364U CN205730364U CN201620414024.6U CN201620414024U CN205730364U CN 205730364 U CN205730364 U CN 205730364U CN 201620414024 U CN201620414024 U CN 201620414024U CN 205730364 U CN205730364 U CN 205730364U
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- CN
- China
- Prior art keywords
- solar energy
- remote control
- control unit
- aeromodelling airplane
- arranged above
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- Expired - Fee Related
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Abstract
nullThe utility model discloses a kind of solar energy aeromodelling airplane，Including head operative body、Solar energy wing-body and remote control unit，Described head operative body lower end is provided with propeller，Above described propeller, both sides are provided with wire-less inductive devices，On described head operative body, information processor is installed，Described information processor is arranged above motor，Described head operative body is arranged above fuselage，Described fuselage interior is provided with main shaft，On described solar energy wing-body, solar panel group is installed，On the downside of described solar panel group, accumulator is installed，Below described solar energy wing-body, put-put is installed，And put-put is uniformly distributed，Described solar energy wing-body is arranged above a pair vertical tail，Outside described vertical tail, elevator is installed，Outside described elevator, rudder is installed，Described remote control unit lower end is provided with display screen.This utility model, has saved resource, more environmental protection.
Description
Technical field
This utility model relates to aeromodelling airplane manufacturing technology field, is specially a kind of solar energy aeromodelling airplane.
Background technology
In traditional aeromodelling airplane field, mostly using electricity is the energy, the running of aeromodelling airplane is completed by converting electrical energy into the form such as heat energy, kinetic energy, electric energy stores for use by switching on power in accumulator, often there is the generation of the not enough situation of electricity in such traditional mode, traditional mode directly filled also brings along the consumption of resource, and under the overall background of the theory of and people's environmental protection increasingly mature at nowadays solar energy generation technology, traditional aeromodelling airplane can not adapt to current environment.
Summary of the invention
The purpose of this utility model is to provide a kind of solar energy aeromodelling airplane, with the problem solving to propose in above-mentioned background technology.
nullFor achieving the above object，This utility model following technical scheme of offer: a kind of solar energy aeromodelling airplane，Including head operative body、Solar energy wing-body and remote control unit，Described head operative body lower end is provided with propeller，Above described propeller, both sides are provided with wire-less inductive devices，On described head operative body, information processor is installed，Described information processor is arranged above motor，Described head operative body is arranged above fuselage，Described fuselage interior is provided with main shaft，On described solar energy wing-body, solar panel group is installed，On the downside of described solar panel group, accumulator is installed，Below described solar energy wing-body, put-put is installed，And put-put is uniformly distributed，Described solar energy wing-body is arranged above a pair vertical tail，Outside described vertical tail, elevator is installed，Outside described elevator, rudder is installed，Described remote control unit lower end is provided with display screen，Described display screen is arranged above direction to control handle，And direction to control handle is symmetrical，The described remote control unit left and right sides is provided with hand-held handle，Described remote control unit upper end is provided with sending and receiving antenna.
Preferably, described vertical tail upper end is provided with tailplane.
Preferably, described accumulator is provided with PLC ECU.
Preferably, described display screen both sides are provided with supply unit, and supply unit is symmetrical.
Preferably, described remote control unit is provided with functional keys, and functional keys is uniformly distributed.
nullCompared with prior art，The beneficial effects of the utility model are: the solar panel group installed on the solar energy wing-body on this utility model can utilize solar electrical energy generation for aeromodelling airplane as power，The energy can be saved，More environmental protection，The accumulator installed can be accumulator charging when aeromodelling airplane works，Can be stand-by as stand-by power supply or next time，The display screen installed on remote control unit can show practical situation during aeromodelling airplane work intuitively，More there is practicality，The hand-held handle simultaneously installed can easily facilitate and carry and operate，The direction to control handle installed can bring more real control feel to user，Aeromodelling airplane is rational in infrastructure，Make use of the solar energy generation technology of maturation，Save resource，More environmental protection，User is the most convenient、Practical.
Accompanying drawing explanation
Fig. 1 is the overall structure schematic diagram of this utility model a kind of solar energy aeromodelling airplane；
Fig. 2 is the solar energy wing agent structure schematic diagram of this utility model a kind of solar energy aeromodelling airplane；
Fig. 3 is the head operative body structural representation of this utility model a kind of solar energy aeromodelling airplane；
Fig. 4 is the remote control arrangement figure of this utility model a kind of solar energy aeromodelling airplane.
In figure: 1-head operative body；2-main shaft；3-fuselage；4-rudder；5-elevator；6-vertical tail；7-tailplane；8-solar energy wing-body；9-supply unit；The hand-held handle of 10-；11-remote control unit；12-functional keys；13-sending and receiving antenna；14-direction to control handle；15-display screen；16-put-put；17-solar panel group；18-PLC ECU；19-accumulator；20-propeller；21-wire-less inductive devices；22-information processor；23-motor.
Detailed description of the invention
Below in conjunction with the accompanying drawing in this utility model embodiment, the technical scheme in this utility model embodiment is clearly and completely described, it is clear that described embodiment is only a part of embodiment of this utility model rather than whole embodiments.Based on the embodiment in this utility model, the every other embodiment that those of ordinary skill in the art are obtained under not making creative work premise, broadly fall into the scope of this utility model protection.
nullRefer to Fig. 1-4，A kind of embodiment that this utility model provides: a kind of solar energy aeromodelling airplane，Including head operative body 1、Solar energy wing-body 8 and remote control unit 11，Head operative body 1 lower end is provided with propeller 20，Above propeller 20, both sides are provided with wire-less inductive devices 21，Information processor 22 is installed on head operative body 1，Information processor 22 is arranged above motor 23，Head operative body 1 is arranged above fuselage 3，Fuselage 3 is internally installed main shaft 2，Solar panel group 17 is installed on solar energy wing-body 8，Accumulator 19 is installed on the downside of solar panel group 17，PLC ECU 18 is installed in accumulator 19，Put-put 16 is installed below solar energy wing-body 8，And put-put 16 is uniformly distributed，Solar energy wing-body 8 is arranged above a pair vertical tail 6，Vertical tail 6 upper end is provided with tailplane 7，Elevator 5 is installed outside vertical tail 6，Rudder 4 is installed outside elevator 5，Remote control unit 11 lower end is provided with display screen 15，Display screen 15 both sides are provided with supply unit 9，And supply unit 9 is symmetrical，Display screen 15 is arranged above direction to control handle 14，And direction to control handle 14 is symmetrical，Remote control unit 11 left and right sides is provided with hand-held handle 10，Remote control unit 11 upper end is provided with sending and receiving antenna 13，Functional keys 12 is installed on remote control unit 11，And functional keys 12 is uniformly distributed.
Specifically used mode: in utility model works, there is provided electric energy to remote control unit 11 by supply unit 9, when aeromodelling airplane is started working, operating function button 12, sending and receiving antenna 13 delivers a signal to wire-less inductive devices 21, solar panel group 17 is started working, convert solar energy into electrical energy and be stored in accumulator 19, elevator 5 is started working, motor 23 works simultaneously, drive propeller 20 to work simultaneously, aeromodelling airplane is made to begin to ramp up, aeromodelling airplane can control flare maneuver by steering manipulation handle 14 in flight course, flight completes, operating function button 12, send dropping signal, landing rudder 5 is started working, aeromodelling airplane begins to decline, so far the rising of an aeromodelling airplane, flight and landing are fully completed.
It is obvious to a person skilled in the art that this utility model is not limited to the details of above-mentioned one exemplary embodiment, and in the case of without departing substantially from spirit or essential attributes of the present utility model, it is possible to realize this utility model in other specific forms.Therefore, no matter from the point of view of which point, embodiment all should be regarded as exemplary, and be nonrestrictive, scope of the present utility model is limited by claims rather than described above, it is intended that all changes fallen in the implication of equivalency and scope of claim included in this utility model.Should not be considered as limiting involved claim by any reference in claim.
Claims (5)
- null1. a solar energy aeromodelling airplane，Including head operative body (1)、Solar energy wing-body (8) and remote control unit (11)，It is characterized in that: described head operative body (1) lower end is provided with propeller (20)，Both sides, described propeller (20) top are provided with wire-less inductive devices (21)，On described head operative body (1), information processor (22) is installed，Described information processor (22) is arranged above motor (23)，Described head operative body (1) is arranged above fuselage (3)，Described fuselage (3) is internally installed main shaft (2)，On described solar energy wing-body (8), solar panel group (17) is installed，Described solar panel group (17) downside is provided with accumulator (19)，Described solar energy wing-body (8) lower section is provided with put-put (16)，And put-put (16) is uniformly distributed，Described solar energy wing-body (8) is arranged above a pair vertical tail (6)，Described vertical tail (6) outside is provided with elevator (5)，Described elevator (5) outside is provided with rudder (4)，Described remote control unit (11) lower end is provided with display screen (15)，Described display screen (15) is arranged above direction to control handle (14)，And direction to control handle (14) is symmetrical，Described remote control unit (11) left and right sides is provided with hand-held handle (10)，Described remote control unit (11) upper end is provided with sending and receiving antenna (13).
- A kind of solar energy aeromodelling airplane the most according to claim 1, it is characterised in that: described vertical tail (6) upper end is provided with tailplane (7).
- A kind of solar energy aeromodelling airplane the most according to claim 1, it is characterised in that: PLC ECU (18) is installed in described accumulator (19).
- A kind of solar energy aeromodelling airplane the most according to claim 1, it is characterised in that: described display screen (15) both sides are provided with supply unit (9), and supply unit (9) is symmetrical.
- A kind of solar energy aeromodelling airplane the most according to claim 1, it is characterised in that: functional keys (12) is installed on described remote control unit (11), and functional keys (12) is uniformly distributed.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620414024.6U CN205730364U (en) | 2016-05-10 | 2016-05-10 | A kind of solar energy aeromodelling airplane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620414024.6U CN205730364U (en) | 2016-05-10 | 2016-05-10 | A kind of solar energy aeromodelling airplane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205730364U true CN205730364U (en) | 2016-11-30 |
Family
ID=57370487
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620414024.6U Expired - Fee Related CN205730364U (en) | 2016-05-10 | 2016-05-10 | A kind of solar energy aeromodelling airplane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205730364U (en) |
-
2016
- 2016-05-10 CN CN201620414024.6U patent/CN205730364U/en not_active Expired - Fee Related
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| 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: 20161130 Termination date: 20170510 |