CN104787314A - Dismountable solar cell panel four-axis aircraft - Google Patents
Dismountable solar cell panel four-axis aircraft Download PDFInfo
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- CN104787314A CN104787314A CN201510182872.9A CN201510182872A CN104787314A CN 104787314 A CN104787314 A CN 104787314A CN 201510182872 A CN201510182872 A CN 201510182872A CN 104787314 A CN104787314 A CN 104787314A
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- axle aircraft
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- Arrangement Or Mounting Of Propulsion Units For Vehicles (AREA)
Abstract
The invention discloses a dismountable solar cell panel four-axis aircraft which is structurally characterized in that a solar cell panel is attached to the surface of a kt support plate; the upper end of a carbon fiber pressure bearing frame bears the solar cell panel and the kt support plate; the lower end of the carbon fiber pressure bearing frame is connected with a carbon fiber triangular pyramid arm; a motor is mounted at each of the left end and the right end of the carbon fiber triangular pyramid arm; propellers are connected onto the motors; a solar stabilized voltage supply and cache group is embedded in the middle of the carbon fiber pressure bearing frame; and the lower end of the solar stabilized voltage supply and cache group is connected with an undercarriage. The aircraft has the technical effects: (1) the aircraft carries out unmanned monitoring aloft, and has wide applications in on-site plotting and detecting fields; (2) a GPS (global position system) position finder is employed, so that the aircraft can carry out fixed positioning and is used for transportation fields of communication, express and the like; and (3) the aircraft has the advantages of zero discharge, solar driving, good flight performance, low cost, long endurance, wide application and the like.
Description
Technical field
The present invention relates to a kind of utilization field of airborne aircraft, be specifically related to a kind of detouchable solar panel four-axle aircraft.
Background technology
Developing solar power, is novel modern new forms of energy developing direction.Day by day emphasizing the civil aviation field of energy-saving and environmental protection, low-carbon (LC), the good characteristic such as to introduce when clean energy resource can realize zero carbon, environmental protection, long boat, be expected to " the star's aircraft " that become low-carbon economy and utilization of new energy resources.Be the world at home, short during the boat of four-axle aircraft, load is low still needs further development and perfection.For this problem, our team is from truss fuselage design, ultra-thin solar plate packaging technology and solar powered three aspects are done and deep are researched and analysed design, by the analytical investigation to these three aspects, to the motor of this aircraft and the configuration of oar, four axle flying platforms, dynamic structure allotment and entire arrangement have done innovative research design, by the design to these aspects, flying platform is expanded to every field, take other function device facilities thereon, like this, the potential value of this aircraft can be realized and made essential step energy-saving and emission-reduction being introduced new field, because, at present in Chinese unmanned plane industry, not exist and realize the fly able unmanned vehicle of the full sun, this is first.This aircraft flight precision is high, can realize spot hover satellite-signal relaying, gather surveying and mapping data information, overlay area is wide, can perform multiple-task, utilize solar power as power source completely, the flight characteristics of its uniqueness is that orthodox flight device is irreplaceable.Can be used for satellite relay Data-Link transfer platform, atmospheric research, weather forecast, environment and disaster monitoring, remote sampling investigation on civilian, crops remote measurement, traffic control, telecommunications and TV service, landscape reservation monitoring, outer celestial body detecting etc.; Militarily can be used for the tasks such as border patrol, scouting, communication repeating, electronic countermeasure.
Summary of the invention
The object of the present invention is to provide a kind of detouchable solar panel four-axle aircraft, this four-axle aircraft flies when can grow boat, and solve the low problem of load-carrying, solar panel is detachable, volume is little, quality is light, of many uses, inherently for load-carrying during long boat provides greatly basis.
The present invention is achieved like this, a kind of detouchable solar panel four-axle aircraft, primarily of kt stay bearing plate, solar panel, sun-generated electric power voltage stabilizing and buffer memory group, inverter, carbon fiber pressure bearing frame, screw propeller, motor, alighting gear, carbon fiber triangular pyramid horn forms, it is characterized in that: solar panel is attached to kt stay bearing plate surface, solar panel and kt stay bearing plate are born in carbon fiber pressure bearing frame upper end, lower end is connected with carbon fiber triangular pyramid horn, about carbon fiber triangular pyramid horn, two ends respectively install a motor, motor is connected with screw propeller, solar power constant voltage power suspply and buffer memory group is studded with in the middle of described carbon fiber pressure bearing frame, solar power constant voltage power suspply and buffer memory group lower end connect alighting gear.
Further, described solar power constant voltage power suspply and buffer memory group are provided with inverter parallel and close that naza flies control, GPS orientator embeds therebetween jointly.
Further, described solar panel from four-axle aircraft dismounting and and can be able to be elevated.
Further, described whole four-axle aircraft adopts carbon fibre material to make.
Further, described kt stay bearing plate is the sheet material of lightweight.
Further, described carbon fiber pressure bearing frame is connected four foot supports and bears solar panels.
Further, described alighting gear has four feets, and each feet scatters for circular arc from centre to surrounding, alleviates four-axle aircraft weight, increases pneumatic property.
Technique effect of the present invention is: (1) carries out unmanned monitoring in high-altitude, surveys and draws on the spot and detecting field has a wide range of applications; (2) GPS orientator adjustable point location is adopted, for passing on the transport fields such as express delivery; (3) when there is zero-emission Driven by Solar Energy, good airworthiness, low cost, long boat, the advantage such as purposes is wide.
Accompanying drawing explanation
Fig. 1 is structural representation of the present invention.
In the drawings, 1, kt stay bearing plate 2, solar panel 3, sun-generated electric power voltage stabilizing and buffer memory group 4, inverter 5, carbon fiber pressure bearing bar 6, screw propeller 7, motor 8, GPS orientator 9, naza fly control 10, alighting gear 11, carbon fiber bar triangular pyramid horn.
Detailed description of the invention
As shown in Figure 1, the present invention comes work and enforcement like this, a kind of detouchable solar panel four-axle aircraft, primarily of kt stay bearing plate 1, solar panel 2, sun-generated electric power voltage stabilizing and buffer memory group 3, inverter 4, carbon fiber pressure bearing frame 5, screw propeller 6, motor 7, alighting gear 10, carbon fiber triangular pyramid horn 11 forms, it is characterized in that: solar panel 2 is attached to kt stay bearing plate 1 surface, solar panel 2 and kt stay bearing plate 1 are born in carbon fiber pressure bearing frame 5 upper end, lower end is connected with carbon fiber triangular pyramid horn 11, carbon fiber triangular pyramid horn about 11 two end respectively installs a motor 7, motor 7 is connected with screw propeller 6, solar power constant voltage power suspply and buffer memory group 3 is studded with in the middle of described carbon fiber pressure bearing frame 5, solar power constant voltage power suspply and buffer memory group 3 lower end connect alighting gear 10, described solar power constant voltage power suspply and buffer memory group 3 are provided with inverter 4 and combine naza and flies control 9, GPS orientator 10 embeds therebetween jointly.
Claims (7)
1. a detouchable solar panel four-axle aircraft, primarily of kt stay bearing plate, solar panel, sun-generated electric power voltage stabilizing and buffer memory group, inverter, carbon fiber pressure bearing frame, screw propeller, motor, alighting gear, carbon fiber triangular pyramid horn forms, it is characterized in that: solar panel is attached to kt stay bearing plate surface, solar panel and kt stay bearing plate are born in carbon fiber pressure bearing frame upper end, lower end is connected with carbon fiber triangular pyramid horn, about carbon fiber triangular pyramid horn, two ends respectively install a motor, motor is connected with screw propeller, solar power constant voltage power suspply and buffer memory group is studded with in the middle of described carbon fiber pressure bearing frame, solar power constant voltage power suspply and buffer memory group lower end connect alighting gear.
2. a kind of detouchable solar panel four-axle aircraft according to claim 1, is characterized in that: described solar power constant voltage power suspply and buffer memory group are provided with inverter parallel and close that naza flies control, GPS orientator embeds therebetween jointly.
3. a kind of detouchable solar panel four-axle aircraft according to claim 1, is characterized in that: described solar panel from four-axle aircraft dismounting and and can be able to be elevated.
4. a kind of detouchable solar panel four-axle aircraft according to claim 1, is characterized in that: described whole four-axle aircraft adopts carbon fibre material to make.
5. a kind of detouchable solar panel four-axle aircraft according to claim 1, is characterized in that: described kt stay bearing plate is the sheet material of lightweight.
6. a kind of detouchable solar panel four-axle aircraft according to claim 1, is characterized in that: described carbon fiber pressure bearing frame is connected four foot supports and bears solar panels.
7. a kind of detouchable solar panel four-axle aircraft according to claim 1, is characterized in that: described alighting gear has four feets, and each feet scatters for circular arc from centre to surrounding.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510182872.9A CN104787314A (en) | 2015-04-17 | 2015-04-17 | Dismountable solar cell panel four-axis aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510182872.9A CN104787314A (en) | 2015-04-17 | 2015-04-17 | Dismountable solar cell panel four-axis aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN104787314A true CN104787314A (en) | 2015-07-22 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510182872.9A Pending CN104787314A (en) | 2015-04-17 | 2015-04-17 | Dismountable solar cell panel four-axis aircraft |
Country Status (1)
| Country | Link |
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| CN (1) | CN104787314A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105070140A (en) * | 2015-09-24 | 2015-11-18 | 中国矿业大学徐海学院 | Quad-rotor flight training rack |
| CN105480422A (en) * | 2015-12-22 | 2016-04-13 | 苏昊纬 | Solar unmanned aerial vehicle |
| CN106882365A (en) * | 2017-04-07 | 2017-06-23 | 金陵科技学院 | A kind of photovoltaic shipping unmanned plane and loading unmanned plane streamline and method of loading |
| CN107364577A (en) * | 2017-08-17 | 2017-11-21 | 西安航空学院 | Solar energy VTOL reconnaissance patrol device |
-
2015
- 2015-04-17 CN CN201510182872.9A patent/CN104787314A/en active Pending
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105070140A (en) * | 2015-09-24 | 2015-11-18 | 中国矿业大学徐海学院 | Quad-rotor flight training rack |
| CN105480422A (en) * | 2015-12-22 | 2016-04-13 | 苏昊纬 | Solar unmanned aerial vehicle |
| CN106882365A (en) * | 2017-04-07 | 2017-06-23 | 金陵科技学院 | A kind of photovoltaic shipping unmanned plane and loading unmanned plane streamline and method of loading |
| CN107364577A (en) * | 2017-08-17 | 2017-11-21 | 西安航空学院 | Solar energy VTOL reconnaissance patrol device |
| CN107364577B (en) * | 2017-08-17 | 2023-04-07 | 西安航空学院 | Solar vertical take-off and landing reconnaissance patrol aircraft |
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Legal Events
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| C06 | Publication | ||
| PB01 | Publication | ||
| WD01 | Invention patent application deemed withdrawn after publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20150722 |