CN205221105U - Solar energy VTOL fixed wing uavs - Google Patents
Solar energy VTOL fixed wing uavs Download PDFInfo
- Publication number
- CN205221105U CN205221105U CN201521009890.9U CN201521009890U CN205221105U CN 205221105 U CN205221105 U CN 205221105U CN 201521009890 U CN201521009890 U CN 201521009890U CN 205221105 U CN205221105 U CN 205221105U
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- China
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- wing
- sides
- canard
- cell panel
- duck
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- Expired - Fee Related
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Abstract
The utility model discloses a solar energy VTOL fixed wing uavs, characterized by fuselage both sides all set up the wing and the duck wing, are equipped with the aileron on the wing, are equipped with duck wing chain of command on the duck wing, and the wing surface sets up panel installation face, and the afterbody sets up to put down and flies driving system, the wing and the equal joint support pole of the duck wing of both sides, the bracing piece of both sides is symmetrical, and both ends all are equipped with the rotor around the bracing piece, install the thin -film solar cell board on the panel installation face. The utility model discloses a reasonable aerodynamic layout to laying solar cell panel on the wing surface, having improved the unmanned aerial vehicle time of leaving a blank greatly, the four -axis provides VTOL power, greatly reduced unmanned aerial vehicle take off and land to the requirement in place.
Description
Technical field
The utility model relates to a kind of solar power fixed-wing VUAV aerodynamic arrangement, belongs to aerodynamic configuration of aircraft technical field.
Background technology
Robot airplane is called for short " unmanned plane ", is the not manned aircraft utilizing radio robot to handle with the process controller provided for oneself.Without driving compartment on machine, but the equipment such as autopilot, process controller is installed.On ground, naval vessels or machine tool command and control station personnel by equipment such as radars, it is followed the tracks of, locates, remote control, remote measurement and digital communication.Can take off as conventional airplane under radio telecommand or launch with booster rocket, also can be taken to by machine tool and throw in flight in the air.During recovery, the available mode automatic Landing the same with conventional airplane landing mission, also reclaims by remote control parachute or block.Can use repeatedly by repetitiousness.Be widely used in aerial reconnaissance, supervision, communication, antisubmarine, electro countermeasure etc.How to reduce flight resistance, improve the Focal point and difficult point that flying power is unmanned aerial vehicle design.
Summary of the invention
The utility model relates to a kind of solar power vertical takeoff and landing fixed-wing unmanned plane, to improve unmanned plane airborne period, and meets the technical requirements of fixed-wing unmanned plane vertical takeoff and landing.
For achieving the above object, the utility model have employed following technical proposals: a kind of solar power vertical takeoff and landing fixed-wing unmanned plane, comprise fuselage, wing, strut bar, rotor, aileron, canard, canard control surface, cell panel attachment face, the flat Force system that flies, fuselage both sides all arrange wing and canard, wing is provided with aileron, canard is provided with canard control surface, aerofoil surface arranges cell panel attachment face, afterbody arranges the flat Force system that flies, the wing of both sides is all connected strut bar with canard, the strut bar of both sides is symmetrical, the rear and front end of strut bar is equipped with rotor.
Cell panel attachment face installs thin-film solar cell panel.
Fuselage requires according to internal placement and determines its profile.Aerofoil surface installs solar panel according to its power demand, preferred film solar panel, and wing adopts maximum ga(u)ge to be the laminar f1ow airfoil profile of 12%.
The utility model by rational aerodynamic arrangement, and lays solar panel in aerofoil surface, and substantially increase unmanned plane airborne period, four axles provide vertical takeoff and landing power, greatly reduce the requirement of unmanned plane landing to place.
Accompanying drawing explanation
Fig. 1 is the utility model schematic diagram.
1. fuselages, 2. wing, 3. aileron, 4. strut bar, 5. rotor, the 6. flat Force system that flies, 7. canard, 8. canard control surface, 9. cell panel attachment face in figure.
Detailed description of the invention
As shown in Figure 1, this solar power vertical takeoff and landing fixed-wing unmanned plane, comprise fuselage 1, wing 2, strut bar 4, rotor 5, aileron 3, canard 7, canard control surface 8, cell panel attachment face 9, the flat Force system 6 that flies, fuselage 1 both sides all arrange wing 2 and canard 7, wing 2 is provided with aileron 3, canard 7 is provided with canard control surface 8, wing 2 surface arranges cell panel attachment face 9, afterbody arranges the flat Force system 6 that flies, the wing 2 of both sides is all connected strut bar 3 with canard 7, the strut bar 3 of both sides is symmetrical, and the rear and front end of strut bar 3 is equipped with rotor 5.
Fuselage according to internal placement require and determine its profile, wing 2 surface according to its power demand install solar panel, preferred film solar panel, wing 2 adopt maximum ga(u)ge be 12% laminar f1ow airfoil profile.
Claims (2)
1. a solar power vertical takeoff and landing fixed-wing unmanned plane, comprise fuselage, wing, strut bar, rotor, aileron, canard, canard control surface, cell panel attachment face, the flat Force system that flies, it is characterized in that: fuselage both sides all arrange wing and canard, wing is provided with aileron, canard is provided with canard control surface, aerofoil surface arranges cell panel attachment face, afterbody arranges the flat Force system that flies, the wing of both sides is all connected strut bar with canard, the strut bar of both sides is symmetrical, and the rear and front end of strut bar is equipped with rotor.
2. solar power vertical takeoff and landing fixed-wing unmanned plane according to claim 1, is characterized in that: cell panel attachment face installs thin-film solar cell panel.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201521009890.9U CN205221105U (en) | 2015-12-08 | 2015-12-08 | Solar energy VTOL fixed wing uavs |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201521009890.9U CN205221105U (en) | 2015-12-08 | 2015-12-08 | Solar energy VTOL fixed wing uavs |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205221105U true CN205221105U (en) | 2016-05-11 |
Family
ID=55896187
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201521009890.9U Expired - Fee Related CN205221105U (en) | 2015-12-08 | 2015-12-08 | Solar energy VTOL fixed wing uavs |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205221105U (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106379525A (en) * | 2016-12-01 | 2017-02-08 | 北京猎鹰无人机科技有限公司 | Wing connected unmanned plane |
| CN106394901A (en) * | 2016-10-31 | 2017-02-15 | 金陵科技学院 | Photovoltaic power generation fixed-wing three-body unmanned aerial vehicle for mapping |
| CN107757914A (en) * | 2016-08-15 | 2018-03-06 | 南京福尔摩斯智能科技有限公司 | Double dynamical VTOL fixed-wing unmanned plane |
| WO2019007433A1 (en) * | 2017-07-06 | 2019-01-10 | Yu Tian | Hybrid vtol fixed-wing drone having wing-tip propellers |
| EP3628593A1 (en) | 2018-09-28 | 2020-04-01 | Airbus Helicopters | Multirotor aircraft with hybrid or electric engine with optimised energy consumption |
-
2015
- 2015-12-08 CN CN201521009890.9U patent/CN205221105U/en not_active Expired - Fee Related
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107757914A (en) * | 2016-08-15 | 2018-03-06 | 南京福尔摩斯智能科技有限公司 | Double dynamical VTOL fixed-wing unmanned plane |
| CN106394901A (en) * | 2016-10-31 | 2017-02-15 | 金陵科技学院 | Photovoltaic power generation fixed-wing three-body unmanned aerial vehicle for mapping |
| CN106379525A (en) * | 2016-12-01 | 2017-02-08 | 北京猎鹰无人机科技有限公司 | Wing connected unmanned plane |
| WO2019007433A1 (en) * | 2017-07-06 | 2019-01-10 | Yu Tian | Hybrid vtol fixed-wing drone having wing-tip propellers |
| EP3628593A1 (en) | 2018-09-28 | 2020-04-01 | Airbus Helicopters | Multirotor aircraft with hybrid or electric engine with optimised energy consumption |
| FR3086641A1 (en) * | 2018-09-28 | 2020-04-03 | Airbus Helicopters | MULTIROTOR AIRCRAFT WITH ELECTRIC OR HYBRID MOTORIZATION WITH OPTIMIZED ENERGY CONSUMPTION |
| CN110963053A (en) * | 2018-09-28 | 2020-04-07 | 空客直升机 | Electric or hybrid multi-rotor aircraft with optimized energy consumption |
| US11066161B2 (en) | 2018-09-28 | 2021-07-20 | Airbus Helicopters | Electrically or hybrid powered multirotor aircraft with optimized energy consumption |
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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 |
Granted publication date: 20160511 Termination date: 20161208 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |