CN103832587A - Elliptical aerial vehicle - Google Patents
Elliptical aerial vehicle Download PDFInfo
- Publication number
- CN103832587A CN103832587A CN201410071209.7A CN201410071209A CN103832587A CN 103832587 A CN103832587 A CN 103832587A CN 201410071209 A CN201410071209 A CN 201410071209A CN 103832587 A CN103832587 A CN 103832587A
- Authority
- CN
- China
- Prior art keywords
- aerial vehicle
- combustion engine
- electrical motor
- strut bar
- jack
- 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.)
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- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Jib Cranes (AREA)
Abstract
The invention discloses an elliptical aerial vehicle which comprises an internal combustion engine, wherein a gearbox is connected to the internal combustion engine, and is connected with a main rotating wheel through gears; the lower end of the main rotating wheel is fixedly connected with a rotating wheel; a support rod is positioned on the inner middle part of the aerial vehicle; a steering wheel is connected to each of the upper and lower ends of the support rod; a telescopic rod and a base are connected to the middle part of the support rod; the aerial vehicle can be stably landed through the base; wheel supporting frames are connected to the other ends of upright rods through springs; rails are connected to the middle parts of the inner walls of wings; rail wheels are connected between the rails and power converters; turntables are connected to the outer walls of the wings; the upper and lower ends of the inner walls of the wings are fixedly connected with rotating wheels respectively; wind shields are connected between rail protection shells and the wheel supporting frames; aerial vehicle eyes are arranged on a jack; the internal combustion engine drives the wings to rotate through the gearbox and the rotating wheels. According to the elliptical aerial vehicle, the steering wheels are driven to steer the aerial vehicle through a motor, so that the elliptical aerial vehicle is conveniently and flexibly steered; the elliptical aerial vehicle is simple in structure and low in cost, and can be used for patrolling and the carrying of individual or group sightseeing tourists.
Description
Technical field
The present invention relates to a kind of vertical translation aircraft that combustion engine is power that uses.
Background technology
Known vertical translation aircraft has autogyro, and autogyro adopts top spiral and tail helical structure, and in cabin operator's compartment, setting operation chair and gauge panel, utilize internal combustion engine drive propeller, makes aircraft rise or advance.Helicopter is mainly made up of body and lift (containing rotor and tail-rotor), power, transmission three large systems and airborne flight equipment etc.Rotor is generally driven by the machine driven system being made up of transmission shaft and retarder etc. by turboaxle motor or piston engine, also can be driven by the antagonistic force of the jet generation of blade tip.Bibliography: http://baike.baidu.com/view/22518.htm, fromId=35341.This autogyro complex structure, volume is large, and cost is high, and inconvenience is manufactured.
Summary of the invention
In order to overcome autogyro complex structure, volume is large, and cost is high, and the defect that inconvenience is manufactured, the invention provides a kind of elliptic aerial vehicle, and this elliptic aerial vehicle is simple in structure, and cost is low, easily manufactures.
The technical solution used in the present invention is: this elliptic aerial vehicle comprises combustion engine, gauge panel and electrical motor, combustion engine, Hydraulic Pump is connected with jack, combustion engine, gauge panel and electrical motor are connected in aircraft, combustion engine is connected with change speed gear box, change speed gear box is connected by gear with main runner, jack is fixed on air baffle and work chassis, on roller frame, main runner and strut bar bearing fit, main runner lower end is fixedly connected with runner, strut bar is positioned in the middle of aircraft, the upper and lower two ends of strut bar are connected with respectively a bearing circle, electrical motor is connected by connecting rod with bearing circle, in the middle of strut bar, be connected with expansion link and base, base can make aircraft steadily land, insert in force changer expansion link outer end, insert in force changer up-and-down rod one end, the up-and-down rod other end is connected with roller frame by spring, in the middle of shark's fin inwall, be connected with track, between track and force changer, be connected rail wheel, shark's fin outer wall is connected with rotating disk, shark's fin inwall top and bottom are fixedly linked with runner respectively, air baffle is connected between track protective case and roller frame, electrical motor is contained under chassis and is connected with gear, gear is fixed on jack, the device eyes of flying up to heaven are housed on jack, strut bar and base are fixedly connected on bearing, electrical motor connection work chassis and gear, gear is connected in the middle of jack, base is connected on strut bar and is fixed in the middle of bearing, bearing is fixed on expansion link work chassis.
The present invention forms approximate ellipsoidal device body by bearing circle, shark's fin, and combustion engine, by change speed gear box and the rotation of driven by rotating wheel shark's fin, utilizes electrical motor to drive bearing circle that aircraft is turned to, and turns to conveniently, flexibly.Simple in structure, cost is low, easily manufactures.Without runway, fall to normal price, can be used for the delivery of patrol, individual or collective's sightseeing tour.
Brief description of the drawings
Fig. 1 is the structural representation of one embodiment of the invention.
1. springs in figure, 2. roller frame, 3. support roller, 4. change speed gear box, 5. combustion engine, 6. electrical motor, 7. strut bar, 8. operations chair, 9. bearing circle, 10. connecting rod, 11. gauge panels, 12. runners, 13. air baffles, 14. rotating disks, 15. shark's fins, 16. force changers, 17. tracks, 18. rail wheels, 19. push rods, 20. up-and-down rods, 21. main runners, 22. driven gears, 23. driving gears, 24. corner blocks, 25. track protective cases, 26. expansion links, 27. aircraft eyes, 28. jacks, 29. bearings, 30. bases, 31. work chassis, 32. gears, 33. electric wires, 34. hydraulic oil pipes, 35. Hydraulic Pumps.
Detailed description of the invention
In Fig. 1, combustion engine 5, Hydraulic Pump 35 and jack 28 are connected, and combustion engine 5, gauge panel 11 and electrical motor 6 are connected in aircraft.Combustion engine 5 is connected with change speed gear box 4, and change speed gear box 4 is connected with driven gear 22 by driving gear 23 with main runner 21.Jack 28 is fixed on air baffle 13 and works on chassis 31, roller frame 2, main runner 21 tops and strut bar 7 bearing fits, and main runner 21 lower ends are fixedly connected with runner 12.Strut bar 7 is positioned in the middle of aircraft, and strut bar is connected with respectively a bearing circle 9 in two ends Shang Xia 7, and electrical motor 6 is connected by connecting rod 10 with bearing circle 9.In the middle of strut bar 7, be connected with expansion link 26 and base 30, base 30 can make aircraft steadily land, insert in force changer 16 expansion link 26 outer ends, insert in force changer 16 up-and-down rod 20 one end, up-and-down rod 20 other ends are connected with roller frame 2 by spring 1, in the middle of shark's fin 15 inwalls, are connected with track 17, are connected rail wheel 18 between track 17 and force changer 16, shark's fin 15 outer walls are connected with rotating disk 14, and shark's fin 15 inwall top and bottom are fixedly linked with runner 12 respectively.Air baffle 13 is connected between track protective case 25 and roller frame 2, and electrical motor 6 is contained in work chassis and is connected with gear 32 for 31 times, and gear 32 is fixed on jack 28, and the device eyes 27 of flying up to heaven are housed on jack 28.Strut bar 7 and base 30 are fixedly connected on bearing 29.
Electrical motor 6 connects work chassis 31 and gear 32, and gear 32 is connected in the middle of jack 28.Base 30 is connected on strut bar 7 and is fixed in the middle of bearing 29, and bearing 29 is fixed on expansion link 26 and works on chassis 31
Hydraulic Pump 35 works jack 28 by hydraulic oil pipe 34, and aircraft eyes 27 are stretched.
When use, expansion link inserts in force changer 16 for 26 times, by force changer 16, the roller frame 2 that up-and-down rod 20 connects is matched with runner 21, and rail wheel 18 matches with track 17.Combustion engine 5 drives main runner 21, runner 12, shark's fin 15, track 17 to rotate together with rotating disk 14 by change speed gear box 4.When rotation, air is entered by shark's fin 15 cavity lower ends, discharges from shark's fin 15 cavity upper ends, produces raising force.Electrical motor 6 regulates the angle of bearing circle 9 to realize by connecting rod 10 and turns to.Air baffle 13 surrounds operator's compartment, and operations chair 8 and gauge panel 11 are connected in operator's compartment.Electrical motor 6 is fixed on driven gear 32 on work chassis 31 stretches out outside aircraft body jack 28.Bearing 29 is fixed on work chassis 31 and on expansion link 26, is connected strut bar 7 and base 30, makes the steady land of aircraft.
Claims (1)
1. an elliptic aerial vehicle, this elliptic aerial vehicle comprises combustion engine, gauge panel and electrical motor, combustion engine, gauge panel and electrical motor are connected in aircraft, it is characterized in that: combustion engine, gauge panel and electrical motor are connected in aircraft, combustion engine is connected with change speed gear box, change speed gear box is connected by gear with main runner, jack is fixed on air baffle and work chassis, on roller frame, main runner and strut bar bearing fit, main runner lower end is fixedly connected with runner, strut bar is positioned in the middle of aircraft, the upper and lower two ends of strut bar are connected with respectively a bearing circle, electrical motor is connected by connecting rod with bearing circle, in the middle of strut bar, be connected with expansion link and base, base can make aircraft steadily land, insert in force changer expansion link outer end, insert in force changer up-and-down rod one end, the up-and-down rod other end is connected with roller frame by spring, in the middle of shark's fin inwall, be connected with track, between track and force changer, be connected rail wheel, shark's fin outer wall is connected with rotating disk, shark's fin inwall top and bottom are fixedly linked with runner respectively, air baffle is connected between track protective case and roller frame, electrical motor is contained under chassis and is connected with gear, gear is fixed on jack, the device eyes of flying up to heaven are housed on jack, strut bar and base are fixedly connected on bearing, electrical motor connection work chassis and gear, gear is connected in the middle of jack, base is connected on strut bar and is fixed in the middle of bearing, bearing is fixed on expansion link work chassis.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410071209.7A CN103832587B (en) | 2014-03-01 | 2014-03-01 | Elliptic aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410071209.7A CN103832587B (en) | 2014-03-01 | 2014-03-01 | Elliptic aerial vehicle |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN103832587A true CN103832587A (en) | 2014-06-04 |
| CN103832587B CN103832587B (en) | 2016-09-07 |
Family
ID=50796553
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410071209.7A Expired - Fee Related CN103832587B (en) | 2014-03-01 | 2014-03-01 | Elliptic aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN103832587B (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108341045A (en) * | 2018-03-29 | 2018-07-31 | 南京工业职业技术学院 | Unmanned plane falling protecting device |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201161713Y (en) * | 2008-02-05 | 2008-12-10 | 焦洪亮 | Elliptic aerial vehicle |
| CN101746507A (en) * | 2008-12-12 | 2010-06-23 | 霍尼韦尔国际公司 | Hybrid power for ducted fan unmanned aerial systems |
| GB2502167A (en) * | 2012-02-08 | 2013-11-20 | Gary Sewell | Chassis mounted vortex generator for attraction towards surfaces |
-
2014
- 2014-03-01 CN CN201410071209.7A patent/CN103832587B/en not_active Expired - Fee Related
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201161713Y (en) * | 2008-02-05 | 2008-12-10 | 焦洪亮 | Elliptic aerial vehicle |
| CN101746507A (en) * | 2008-12-12 | 2010-06-23 | 霍尼韦尔国际公司 | Hybrid power for ducted fan unmanned aerial systems |
| GB2502167A (en) * | 2012-02-08 | 2013-11-20 | Gary Sewell | Chassis mounted vortex generator for attraction towards surfaces |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108341045A (en) * | 2018-03-29 | 2018-07-31 | 南京工业职业技术学院 | Unmanned plane falling protecting device |
| CN108341045B (en) * | 2018-03-29 | 2024-04-09 | 南京工业职业技术学院 | Unmanned aerial vehicle protection device that falls |
Also Published As
| Publication number | Publication date |
|---|---|
| CN103832587B (en) | 2016-09-07 |
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| C14 | Grant of patent or utility model | ||
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| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160907 Termination date: 20180301 |
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| CF01 | Termination of patent right due to non-payment of annual fee |