CN207565839U - A kind of novel fixed-wing unmanned plane using solar recharging - Google Patents
A kind of novel fixed-wing unmanned plane using solar recharging Download PDFInfo
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- CN207565839U CN207565839U CN201721579328.9U CN201721579328U CN207565839U CN 207565839 U CN207565839 U CN 207565839U CN 201721579328 U CN201721579328 U CN 201721579328U CN 207565839 U CN207565839 U CN 207565839U
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- wing flap
- unmanned plane
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Abstract
A kind of novel fixed-wing unmanned plane using solar recharging,Including fuselage,Wing,Empennage,Landing pulley and solar panel,Fuselage is fixedly arranged at the front end with driving motor,Screw blade is fixed in the shaft of driving motor,The top of fuselage is equipped with signal receiver,The trailing edge is equipped with two-stage wing flap,Two-stage wing flap includes the first wing flap and the second wing flap,First wing flap and the second wing flap are connect by extension and retraction system with wing,The solar panel is individually fixed in wing,The top of first wing flap and the second wing flap,Fuselage interior is fixed with automatic pilot and accumulator,Solar panel is connect with accumulator,Accumulator is connect with automatic pilot,Automatic pilot respectively with GPS positioning instrument,FPV cameras,Signal receiver,Steering engine,Electron speed regulator is connected with extension and retraction system,Electron speed regulator is connect with driving motor.The fixed-wing unmanned plane not only improves cruising ability, also improves the security performance of its landing.
Description
Technical field
The utility model design unmanned plane field, and in particular to a kind of novel fixed-wing using solar recharging nobody
Machine.
Background technology
Unmanned plane is the not manned aircraft manipulated using radio robot and the presetting apparatus provided for oneself, with tradition
Manned aircraft is compared, and unmanned plane is suitble to the task under various environmental conditions, being particularly under mal-condition for task.
With going deep into for unmanned plane research, unmanned plane cost is more cheap, this has also directly been provided for being widely applied for unmanned plane
Power condition, at present unmanned plane take photo by plane, agricultural, plant protection, miniature express transportation, disaster relief, mapping, electric inspection process etc. field
It is used widely.
Existing common unmanned plane is divided into multi-rotor unmanned aerial vehicle and fixed-wing unmanned plane, and multi-rotor unmanned aerial vehicle is due to small volume
The fields such as it is more suitable for detecting, take photo by plane, but its small volume, load capacity are poor and cruising ability is poor, while severe
Environment stability inferior also not as good as fixed-wing unmanned plane, and the bearing capacity of fixed-wing unmanned plane have compared with multi-rotor unmanned aerial vehicle it is very big
It is promoted, cruising ability is also opposite to be improved, and can carry more equipment to perform more extensive Mission Operations.
However, as fixed-wing unmanned plane mostly using electric energy as unique power resources, cruising ability limits fixed-wing
The development of unmanned plane, existing technology mostly charge to improve cruising ability to its accumulator using solar energy, however not right
Fixed-wing unmanned plane carry out structure on change, rely solely on solar energy provide the extended efficiency of electric energy be it is extremely limited, together
When due to lacking highly efficient glissando, existing fixed-wing unmanned plane is easily damaged or causes during landing
The damage of its precision instrument carried.
Utility model content
The utility model to solve the above-mentioned problems, devise a kind of novel fixed-wing using solar recharging nobody
Machine, the unmanned plane are charged, while the wing of fixed-wing unmanned plane is improved using solar energy for accumulator, make it pneumatic
Performance is more preferable, reduces energy consumption, makes the electric energy of solar energy conversion and the electric energy service efficiency higher of accumulator, so as to greatly improve
The cruising ability of fixed-wing unmanned plane.
In order to realize above-mentioned technical purpose, reach above-mentioned technique effect, the utility model is real by the following technical programs
Existing：
A kind of novel fixed-wing unmanned plane using solar recharging, including fuselage, wing, empennage, landing pulley and too
Positive energy solar panel, fuselage are fixedly arranged at the front end with driving motor, screw blade are fixed in the shaft of driving motor, is set at the top of fuselage
There is signal receiver, it is characterised in that：The trailing edge is equipped with two-stage wing flap, and two-stage wing flap includes the first wing flap and second
Wing flap, the first wing flap and the second wing flap are connect by extension and retraction system with wing, and the solar panel is individually fixed in machine
The top of the wing, the first wing flap and the second wing flap, fuselage interior are fixed with automatic pilot and accumulator, and solar panel is with storing
Battery connects, and the circuit that the solar panel is connect with accumulator is equipped with inverter, accumulator and automatic pilot
Connection, automatic pilot respectively with GPS positioning instrument, FPV cameras, signal receiver, steering engine, electron speed regulator and extension and retraction system
Connection, electron speed regulator are connect with driving motor.
Further, the front fuselage is equipped with anticollision wraping plate, and anticollision wraping plate is individually fixed in the landing pulley of both sides
On, shock-absorbing support is fixed on anticollision wraping plate, the bottom of fuselage is fixed in the upper end of shock-absorbing support.
Further, the extension and retraction system is by folding and unfolding motor, folding storage mechanism, stent, first connecting rod, second
The multi link system that connecting rod, third connecting rod, connecting plate, fourth link, the 5th connecting rod, six-bar linkage and seven-link assembly form, the
One connecting rod is fixed in the shaft of folding and unfolding motor, and head rod is hinged with the second connecting rod, and second connecting rod one end is fixed
In on stent and the other end is hinged with connecting plate, third connecting rod is hinged with the second connecting rod, and the 4th connecting rod is connect with third
Bar is hinged, and the 5th connecting rod is hinged with the 4th connecting rod, and the 6th connecting rod one end and the 5th connecting rod be hinged and the other end and the
Seven connecting rods are hinged, and the connecting plate is fixed on the right end of the first wing flap, and the 5th connecting rod is fixed on the side of the first wing flap
On, the side middle of the first wing flap is fixed in one end of six-bar linkage, is provided with sliding slot on the side left end of the first wing flap, and the 7th
Connecting rod is fixed on the right side end of the second wing flap, and seven-link assembly can to the left slide along sliding slot and the second wing flap is pulled to shrink or open up
It opens.
Further, the automatic pilot inner set communication module, the communications protocol that communication module uses is 2G/
One kind in 3G/4G/WIFI/BlueTooth/ZigBee.
The beneficial effects of the utility model are：The unmanned plane using solar energy for accumulator charging, while to fixed-wing without
Man-machine wing is improved, and makes its aeroperformance more preferable, reduces energy consumption, makes the electric energy of solar energy conversion and the electricity of accumulator
Energy service efficiency higher so as to greatly improve the cruising ability of fixed-wing unmanned plane, and can be protected effectively during unmanned plane landing
Protect fuselage and its precision instrument of carrying, safety higher.
Description of the drawings
In order to illustrate more clearly of the technical solution of the utility model embodiment, make required for being described below to embodiment
Attached drawing is briefly described, it should be apparent that, the accompanying drawings in the following description is only some embodiments of the utility model,
For those of ordinary skill in the art, without creative efforts, it can also be obtained according to these attached drawings
Other attached drawings.
Fig. 1 is a kind of overall structure diagram of the novel fixed-wing unmanned plane using solar recharging；
Fig. 2 is a kind of each composition modular construction schematic diagram of novel fixed-wing unmanned plane using solar recharging；
Fig. 3 is a kind of attachment structure schematic diagram of the wing flap of the novel fixed-wing unmanned plane using solar recharging；
Fig. 4 is a kind of wing aerodynamic principle of optimality figure of the novel fixed-wing unmanned plane using solar recharging；
Fig. 5 is a kind of structure diagram of the novel fixed-wing unmanned plane using solar recharging.
In attached drawing, parts list represented by the reference numerals are as follows：
1- fuselages, 11- wings, 12- wing flaps, 13- driving motors, 14- screw blades, 15- shock-absorbing supports, 16- signals connect
Receipts device, 17- automatic pilots, 18- accumulators, 19- steering engines, 2- solar panels, 3- folding storages mechanism, 31- stents,
32- first connecting rods, 33- second connecting rods, 34- third connecting rods, 35- connecting plates, 36- fourth links, the 5th connecting rods of 37-, 38- the 6th
Connecting rod, 39- seven-link assemblies, 111- folding and unfolding motor, the first wing flaps of 121-, the second wing flaps of 122-, 123- sliding slots, 151- landings are slided
Wheel, 152- shock-absorbing supports, 153- anticollision wraping plates, 171-GPS position indicators, 172-FPV cameras, 173- electron speed regulators, 174-
Extension and retraction system, 175- communication modules, 181- inverters.
Specific embodiment
The following is a combination of the drawings in the embodiments of the present utility model, and the technical scheme in the embodiment of the utility model is carried out
It clearly and completely describes, it is clear that the described embodiments are only a part of the embodiments of the utility model rather than whole
Embodiment.Based on the embodiment in the utility model, those of ordinary skill in the art are without creative efforts
The all other embodiment obtained, shall fall within the protection scope of the present invention.
Refering to shown in Fig. 1-5, a kind of novel fixed-wing unmanned plane using solar recharging, including fuselage (1), wing
(11), empennage, landing pulley (151) and solar panel (2), fuselage (1) are fixedly arranged at the front end with driving motor (13), driving
Screw blade (14) is fixed in the shaft of motor (13), the top of fuselage (1) is equipped with signal receiver (16), wing (11) rear
Equipped with two-stage wing flap (12), two-stage wing flap includes the first wing flap (121) and the second wing flap (122), the first wing flap (121) and second
Wing flap (122) is connect by extension and retraction system (174) with wing (11), and solar panel (2) is individually fixed in wing (11),
The top of one wing flap (121) and the second wing flap (122), fuselage (1) is internal to be fixed with automatic pilot (17) and accumulator (18),
Solar panel (2) is connect with accumulator (18), and the circuit that solar panel (2) is connect with accumulator (18) is equipped with inverse
Become device (181), accumulator (18) connect with automatic pilot (17), automatic pilot (17) respectively with GPS positioning instrument (171),
FPV cameras (172), signal receiver (16), steering engine (19), electron speed regulator (173) and extension and retraction system (174) connection, electricity
Sub- governor (173) connect with driving motor (13).
Therein, described fuselage (1) front end is equipped with anticollision wraping plate (153), and anticollision wraping plate (153) is individually fixed in both sides
Landing pulley (151) on, shock-absorbing support (152) is fixed on anticollision wraping plate (153), the upper end of shock-absorbing support (152) is fixed
In the bottom of fuselage, the shock-absorbing support (152) in the present embodiment is made using elastic rod body material, when fixed-wing unmanned plane
During landing, shock-absorbing support (152) is absorbable to be unable to impact energy, while anticollision wraping plate (153) is with can preventing fuselage (1) head impact
The security performance of its landing is improved in face.
Therein, the extension and retraction system (174) is by folding and unfolding motor (111), folding storage mechanism (3), stent
(31), first connecting rod (32), second connecting rod (33), third connecting rod (34), connecting plate (35), fourth link (36), the 5th connecting rod
(37), the multi link system of six-bar linkage (38) and seven-link assembly (39) composition, first connecting rod (32) are fixed on folding and unfolding motor
(111) in shaft, head rod (32) is hinged with the second connecting rod (33), and stent is fixed in the second connecting rod (33) one end
(31) on and the other end is hinged with connecting plate (35), and third connecting rod (34) is hinged with the second connecting rod (32), the 4th connecting rod
(36) hinged with third connecting rod (34), the 5th connecting rod (37) is hinged with the 4th connecting rod (36), the 6th connecting rod (38) one
End is hinged with the 5th connecting rod (37) and the other end and the 7th connecting rod (39) are hinged, and the connecting plate (35) is fixed on first
The right end of wing flap (121), the 5th connecting rod (37) are fixed on the side of the first wing flap (121), one end of six-bar linkage (38)
The side middle of the first wing flap (121) is fixed on, sliding slot (123) is provided on the side left end of the first wing flap (121), the 7th connects
Bar (39) is fixed on the right side end of the second wing flap (122), and seven-link assembly (39) can be slided and be pulled to the left along sliding slot (123)
Second wing flap (122) is shunk or expansion.
The air-flow principle of optimality of wing flap in the present embodiment is：When the expansion that automatic pilot (17) satellite receiver is sent out
During wing flap (2) on wing, automatic pilot (17) exports high level to folding and unfolding motor (111), and folding and unfolding motor (111) drives
Multi link system in dynamic extension and retraction system, that is, the present embodiment flexes outward, at this time the first wing flap (121) and the second wing flap (122) to
Wing (11) rear is unfolded, and the air-flow stroke flowed through above wing (11) is longer, and the air-flow below wing (11) is along wing
Flows, when the air-flow of bottom flow to the first wing flap (121) and the second wing flap (122), air-flow two stock branch of formation, one
Air-flow supports the upper surface flowing of the first wing flap (121), and a upper surface along the second wing flap (122) is flowed, and wing (11) bottom
The air-flow velocity in portion, the first wing flap (121) bottom and the second wing flap (122) bottom faster, forms wall attachment effect, wing (1)
Lift further improves, so as to save the electric energy of driving motor (13) acting consumption.
Due to being respectively fixed with solar cell at the top of wing (11), the first wing flap (121) and the second wing flap (122)
Plate (2), in great abundance of sunshine, solar panel (2) converts solar energy into electrical energy, and the rectification of process inverter (181),
Become accumulator (18) storable electric energy after filtering and inversion, further improve the cruising ability of fixed-wing unmanned plane.
In the description of this specification, the description of reference term " one embodiment ", " example ", " specific example " etc. means
At least one of the utility model is contained in reference to the embodiment or example particular features, structures, materials, or characteristics described
In embodiment or example.In the present specification, schematic expression of the above terms be not necessarily referring to identical embodiment or
Example.
The preferred embodiment in the utility model disclosed above is only intended to help to illustrate the utility model.Preferred embodiment is simultaneously
There is no the details that detailed descriptionthe is all, it is only the specific embodiment also not limit the utility model.Obviously, according to this theory
The content of bright book can make many modifications and variations.This specification is chosen and specifically describes these embodiments, is in order to preferably
The principle and practical application of the utility model is explained, so as to which skilled artisan be enable to be best understood by and utilize this
Utility model.The utility model is limited only by the claims and their full scope and equivalents.
Claims (5)
1. a kind of novel fixed-wing unmanned plane using solar recharging, including fuselage, wing, empennage, landing pulley and the sun
Energy solar panel, fuselage are fixedly arranged at the front end with driving motor, screw blade are fixed in the shaft of driving motor, and the top of fuselage is equipped with
Signal receiver, it is characterised in that：The trailing edge is equipped with two-stage wing flap, and two-stage wing flap includes the first wing flap and second flap
The wing, the first wing flap and the second wing flap are connect by extension and retraction system with wing, the solar panel be individually fixed in wing,
The top of first wing flap and the second wing flap, fuselage interior are fixed with automatic pilot and accumulator, solar panel and electric power storage
Pond connects, and accumulator connect with automatic pilot, automatic pilot respectively with GPS positioning instrument, FPV cameras, signal receiver,
Steering engine, electron speed regulator are connected with extension and retraction system, and electron speed regulator is connect with driving motor.
2. a kind of novel fixed-wing unmanned plane using solar recharging according to claim 1, it is characterised in that：It is described
Front fuselage be equipped with anticollision wraping plate, anticollision wraping plate is individually fixed on the landing pulley of both sides, is fixed with and subtracts on anticollision wraping plate
Shake support, the bottom of fuselage is fixed in the upper end of shock-absorbing support.
3. a kind of novel fixed-wing unmanned plane using solar recharging according to claim 1, it is characterised in that：It is described
Extension and retraction system be by folding and unfolding motor, folding storage mechanism, stent, first connecting rod, second connecting rod, third connecting rod, connecting plate,
The multi link system that fourth link, the 5th connecting rod, six-bar linkage and seven-link assembly form, first connecting rod are fixed on folding and unfolding motor
Shaft on, head rod is hinged with the second connecting rod, and second connecting rod one end is fixed on stent and the other end and connection
Plate is hinged, and third connecting rod is hinged with the second connecting rod, and the 4th connecting rod is hinged with third connecting rod, the 5th connecting rod and the 4th
Connecting rod is hinged, and the 6th connecting rod one end is hinged with the 5th connecting rod and the other end is hinged with the 7th connecting rod, the connection
Plate is fixed on the right end of the first wing flap, and the 5th connecting rod is fixed on the side of the first wing flap, and one end of six-bar linkage is fixed on
The side middle of first wing flap is provided with sliding slot on the side left end of the first wing flap, and seven-link assembly is fixed on the right side of the second wing flap
On the head of side, seven-link assembly can to the left slide along sliding slot and the second wing flap is pulled to shrink or be unfolded.
4. a kind of novel fixed-wing unmanned plane using solar recharging according to claim 1, it is characterised in that：It is described
The circuit that is connect with accumulator of solar panel be equipped with inverter.
5. a kind of novel fixed-wing unmanned plane using solar recharging according to claim 1, it is characterised in that：It is described
Automatic pilot inner set communication module, the communications protocol that communication module uses is 2G/3G/4G/WIFI/BlueTooth/
One kind in ZigBee.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721579328.9U CN207565839U (en) | 2017-11-22 | 2017-11-22 | A kind of novel fixed-wing unmanned plane using solar recharging |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721579328.9U CN207565839U (en) | 2017-11-22 | 2017-11-22 | A kind of novel fixed-wing unmanned plane using solar recharging |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207565839U true CN207565839U (en) | 2018-07-03 |
Family
ID=62691629
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721579328.9U Expired - Fee Related CN207565839U (en) | 2017-11-22 | 2017-11-22 | A kind of novel fixed-wing unmanned plane using solar recharging |
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| Country | Link |
|---|---|
| CN (1) | CN207565839U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112278227A (en) * | 2019-07-24 | 2021-01-29 | 广州极飞科技有限公司 | Aircraft with a flight control device |
-
2017
- 2017-11-22 CN CN201721579328.9U patent/CN207565839U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112278227A (en) * | 2019-07-24 | 2021-01-29 | 广州极飞科技有限公司 | Aircraft with a flight control device |
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| 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: 20180703 Termination date: 20181122 |