CN106864741A - A kind of solar energy auxiliary charging unmanned plane - Google Patents
A kind of solar energy auxiliary charging unmanned plane Download PDFInfo
- Publication number
- CN106864741A CN106864741A CN201710162678.3A CN201710162678A CN106864741A CN 106864741 A CN106864741 A CN 106864741A CN 201710162678 A CN201710162678 A CN 201710162678A CN 106864741 A CN106864741 A CN 106864741A
- Authority
- CN
- China
- Prior art keywords
- fuselage
- unmanned plane
- motor
- solar energy
- battery
- 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.)
- Withdrawn
Links
- 229910052739 hydrogen Inorganic materials 0.000 claims description 12
- 239000001257 hydrogen Substances 0.000 claims description 12
- 239000002775 capsule Substances 0.000 claims description 11
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 claims description 10
- 125000004435 hydrogen atom Chemical group [H]* 0.000 claims 1
- 238000000034 method Methods 0.000 abstract description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 3
- 238000013461 design Methods 0.000 description 2
- 238000011161 development Methods 0.000 description 2
- 230000005611 electricity Effects 0.000 description 2
- 238000005265 energy consumption Methods 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 238000011160 research Methods 0.000 description 1
- 238000012360 testing method Methods 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/34—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like comprising inflatable structural components
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/12—Rotor drives
-
- B64D27/353—
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/19—Propulsion using electrically powered motors
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Remote Sensing (AREA)
- Toys (AREA)
- Charge And Discharge Circuits For Batteries Or The Like (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Abstract
The invention discloses a kind of solar energy auxiliary charging unmanned plane, it is related to unmanned air vehicle technique field, including fuselage, fuselage surface is provided with charging hole, it is connected with battery, the fuselage interior includes controller, charging draw-in groove and battery, wherein controller is located at back, the controller is connected with wireless signal transceiver, charging draw-in groove is located at waist, the charging draw-in groove and battery clamping, the fuselage outer side is connected with 4 pieces of faggings, solar panel is bonded with fagging, the solar panel is connected with battery, the outer end of every piece of fagging is connected with wing arm, the wing arm top is equipped with motor and by motor-driven rotor, motor is externally provided with motor casing, the motor is connected with controller.Solar panel is converted into electric energy and charges a battery by absorbing solar energy, by solar energy, to increase unmanned plane cruising time.
Description
Technical field
The present invention relates to unmanned plane field, specially a kind of solar energy auxiliary charging unmanned plane
Background technology
Unmanned plane is UAV, is do not have driver on machine, is flown automatically or by people on ground by programme-control
The aircraft being remotely controlled on face or machine tool.It is equipped with automatic pilot, program control system, remote control and telemetry system, leads automatically
The conditions such as boat system, automatic landing system realize that far distance controlled is flown by these systems, external first using nothing from the thirties
After the electrically-energized model of an airplane of line is as target drone, the development of unmanned plane is very rapid, and particularly in recent years, China is to unmanned plane
Development also accelerate paces with exploitation, establish unmanned aerial vehicle design research institution by support of institution of higher education, and with voluntarily
Design and small serial production ability.Common electric power unmanned plane is artificial charging, only can just be filled after unmanned plane grounds
Electricity, result in the unmanned plane during flying time of short duration, it is impossible to continue a journey for a long time.
The content of the invention
Present invention aim at providing a kind of solar energy auxiliary charging unmanned plane, to solve what is proposed in above-mentioned background technology
Problem.
A kind of solar energy auxiliary charging unmanned plane, including fuselage, fuselage surface are provided with charging hole, are connected with battery, institute
State fuselage interior and be provided with controller, charging draw-in groove and battery, wherein controller is located at back, the controller connection
There is wireless signal transceiver, charging draw-in groove is located at waist, the charging draw-in groove and battery clamping, the fuselage outer side
4 pieces of faggings are connected with, solar panel is bonded with fagging, the solar panel is connected with battery, every piece of fagging
Outer end be connected with Power Component, the Power Component includes wing arm, motor and rotor, the wing arm top equipped with motor with
And by motor-driven rotor, motor is externally provided with motor casing, the motor is connected with controller.
Preferably, the fuselage is generally conical, and fuselage tip is excessive by circular arc.
Preferably, bottom is provided with hydrogen capsule in the fuselage.
Preferably, the fuselage inner bottom part is equipped with camera.
Preferably, the cross section of the fagging is trapezoidal.
Preferably, it is provided with hydrogen capsule inside the wing arm.
The advantage of the invention is that：A kind of solar energy auxiliary charging unmanned plane simple structure of the present invention, easy to control, circular cone
Shape housing can reduce air drag, and by solar recharging, can considerably increase the cruising time of unmanned plane, and
Hydrogen capsule is housed in enclosure interior, the deadweight of unmanned plane is alleviated, battery power consumption is reduced.
Brief description of the drawings
Fig. 1 is a kind of empty dual-purpose equiaxial test chart of unmanned plane of water of the present invention.
Fig. 2 is a kind of empty dual-purpose unmanned plane front view of water of the present invention.
Fig. 3 is a kind of empty dual-purpose unmanned plane top view of water of the present invention.
Fig. 4 is Fig. 2 along A-A directions sectional view.
Fig. 5 is Fig. 2 along B-B directions sectional view.
Wherein：1-fuselage, 2-jack, 3-fagging, 4-solar panel, 5-wing arm, 6-rotor, 7-motor,
8-controller, 9-charging draw-in groove, 10-battery, 11-charging hole, 12-camera, 13-hydrogen capsule, 71-motor casing.
Specific embodiment
For technological means, creation characteristic, reached purpose and effect for making present invention realization are easy to understand, with reference to
Specific embodiment, is expanded on further the present invention.
As shown in Figures 1 to 4, a kind of solar energy auxiliary charging unmanned plane, including fuselage 1, the surface of fuselage 1 is provided with charging hole
2, it is connected with battery 10, the inside of the fuselage 1 includes controller 8, charging draw-in groove 9 and battery 10, and wherein controller 8 sets
Portion on the fuselage 1, the controller 8 is connected with wireless signal transceiver, and charging draw-in groove 9 is located at the middle part of fuselage 1, the charging
Draw-in groove 9 and the clamping of battery 10, the fuselage 1 are connected with 4 pieces of faggings 3, are bonded with solar panel 4 on fagging 3, it is described too
It is positive can cell panel 4 be connected with battery 10, the outer end of every piece of fagging 3 is connected with wing arm 5, the top of wing arm 5 be equipped with motor 7 with
And the rotor 6 driven by motor 7, motor 7 is externally provided with motor casing 71, and the motor 7 is connected with controller 8.
In the present embodiment, the fuselage 1 is generally conical, and fuselage tip excessively, can effectively be subtracted by circular arc
Few unmanned plane air drag in uphill process.
In the present embodiment, bottom is provided with hydrogen capsule 13 in the fuselage 1, and hydrogen density is less than air, and hydrogen capsule 13 can
Mitigate the deadweight of unmanned plane, reduce the energy consumption of battery, be conducive to the continuation of the journey of unmanned plane.
In the present embodiment, the inner bottom part of the fuselage 1 is equipped with camera 12, can be by the picture of aerial photographing earth's surface.
In the present embodiment, the cross section of the fagging 3 is trapezoidal, increases solar panel 4 by direct sunlight
Area, is conducive to the collection of luminous energy, improves charge efficiency.
In the present embodiment, hydrogen capsule is provided with inside the wing arm 5, hydrogen capsule can mitigate the deadweight of unmanned plane, reduce electricity
The energy consumption in pond, is conducive to the continuation of the journey of unmanned plane.
Easy to operate based on a kind of above-mentioned, solar energy auxiliary charging unmanned plane simple structure of the invention, the present invention is using too
The charge mode of positive energy auxiliary charging, considerably increases unmanned plane skyborne cruising time, under conditions of having sunlight, the sun
Energy cell panel 4 can convert light energy into electric energy, and constantly be charged to battery 10 by charging slot 9, to reach continuation of the journey
Purpose, the hydrogen capsule 13 in housing 1 helps to mitigate the deadweight of unmanned plane, reduces energy loss, extends unmanned plane in the air
Shooting time.
As known by the technical knowledge, the present invention can be by other essence without departing from its spirit or the embodiment party of essential feature
Case is realized.Therefore, embodiment disclosed above, for each side, is all merely illustrative, and is not only.Institute
Have within the scope of the present invention or be included in the invention in the change being equal in the scope of the present invention.
Claims (6)
1. a kind of solar energy auxiliary charging unmanned plane, including fuselage, it is characterised in that fuselage surface is provided with charging hole, with electric power storage
Pond connects, and the fuselage interior is provided with controller, charging draw-in groove and battery, and wherein controller is located at back, described
Controller is connected with wireless signal transceiver, and charging draw-in groove is located at waist, the charging draw-in groove and battery clamping, institute
State fuselage outer side and be connected with 4 pieces of faggings, solar panel is bonded with fagging, the solar panel connects with battery
Connect, the outer end of every piece of fagging is connected with Power Component, and the Power Component includes wing arm, motor and rotor, on the wing arm
Equipped with motor and by motor-driven rotor, motor is externally provided with motor casing, and the motor is connected with controller in portion.
2. a kind of solar energy auxiliary charging unmanned plane according to claim 1, it is characterised in that the fuselage is generally justified
Taper, fuselage tip is excessive by circular arc.
3. a kind of solar energy auxiliary charging unmanned plane according to claim 1, it is characterised in that bottom sets in the fuselage
There is hydrogen capsule.
4. a kind of solar energy auxiliary charging unmanned plane according to claim 1, it is characterised in that the fuselage bottom is equipped with
Camera.
5. a kind of solar energy auxiliary charging unmanned plane according to claim 1, it is characterised in that the cross section of the fagging
For trapezoidal.
6. a kind of solar energy auxiliary charging unmanned plane according to claim 1, it is characterised in that be provided with inside the wing arm
Hydrogen capsule.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710162678.3A CN106864741A (en) | 2017-03-18 | 2017-03-18 | A kind of solar energy auxiliary charging unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710162678.3A CN106864741A (en) | 2017-03-18 | 2017-03-18 | A kind of solar energy auxiliary charging unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106864741A true CN106864741A (en) | 2017-06-20 |
Family
ID=59172189
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710162678.3A Withdrawn CN106864741A (en) | 2017-03-18 | 2017-03-18 | A kind of solar energy auxiliary charging unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106864741A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108839793A (en) * | 2018-05-31 | 2018-11-20 | 智飞智能装备科技东台有限公司 | A kind of continue a journey for unmanned plane increases the generating equipment of journey |
| CN109927891A (en) * | 2017-12-18 | 2019-06-25 | 国鹄航空科技(杭州)股份有限公司 | A kind of miniature drone with solar recharging |
-
2017
- 2017-03-18 CN CN201710162678.3A patent/CN106864741A/en not_active Withdrawn
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109927891A (en) * | 2017-12-18 | 2019-06-25 | 国鹄航空科技(杭州)股份有限公司 | A kind of miniature drone with solar recharging |
| CN108839793A (en) * | 2018-05-31 | 2018-11-20 | 智飞智能装备科技东台有限公司 | A kind of continue a journey for unmanned plane increases the generating equipment of journey |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20170620 |
|
| WW01 | Invention patent application withdrawn after publication |