CN204210731U - Autogyro - Google Patents
Autogyro Download PDFInfo
- Publication number
- CN204210731U CN204210731U CN201420002191.0U CN201420002191U CN204210731U CN 204210731 U CN204210731 U CN 204210731U CN 201420002191 U CN201420002191 U CN 201420002191U CN 204210731 U CN204210731 U CN 204210731U
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- China
- Prior art keywords
- rotor
- driving engine
- screw propeller
- autogyro
- joystick
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Abstract
The utility model relates to a kind of autogyro, comprises frame, fuselage, driving engine, rotor, screw propeller, tail vane, joystick, instrument, alighting gear, frame upper end connects rotor, and driving engine is between tail vane seat storehouse, be provided with instrument and joystick in passenger cabin, driving engine is connected with screw propeller, is provided with alighting gear below frame, described rotor is for be made up of two blades, and blade is fixed on frame upper end by oar axle.The beneficial effects of the utility model are, safety is high, landing apart from short, stability is high, wind resistance has higher cost performance by force, simultaneously.
Description
Technical field
The utility model relates to field of aviation flight, particularly relates to a kind of autogyro.
Background technology
Autogyro be a kind of using autorotating rotor as lifting surface, screw propeller is as the rotor class aircraft of onward impulse.Autogyro is actually a kind of aircraft between helicopter and fixed wing aircraft, its removing rotor outside, also with a secondary screw propeller to provide the power of advance.The maximum difference of autogyro and helicopter is, the rotor of autogyro is not connected with engine driving system, driving engine just drives screw propeller to provide forward thrust for aircraft, but in the process of cyclogyro flight, blows the raw lift of rotor wing rotation movable property by front air-flow.And the rotor of helicopter is connected with engine driving system, can lift be produced, the power of flight can be provided again.Because the rotor of autogyro is rotation type, the moment of torsion be delivered on fuselage is very little, and therefore autogyro is without the need to the such tail-rotor of helicopter, but generally tail vane is housed, to control flight attitude.
Utility model content
The purpose of this utility model is to overcome above-mentioned deficiency, and provide a kind of good stability, operating safety factor is high, has the autogyro compared with high performance-price ratio.
To achieve these goals, the technical solution adopted in the utility model is: a kind of autogyro, comprises frame, fuselage, driving engine, rotor, screw propeller, tail vane, joystick, instrument, alighting gear, frame upper end connects rotor, driving engine is between tail vane seat storehouse, and be provided with instrument and joystick in passenger cabin, driving engine is connected with screw propeller, be provided with alighting gear below frame, described rotor is for be made up of two blades, and blade is fixed on frame upper end by oar axle.
Described screw propeller is connected with driving engine by horizontal drive power-transfer clutch.
The rotor face of described rotor is for tilting backwards setting.
The blade of described rotor is that oar is turned round in aerodynamic force change.
The beneficial effects of the utility model are:
1, safety is high
2, landing is apart from short
3, stability is high, and wind resistance is strong
4, there is higher cost performance.
Accompanying drawing explanation
Fig. 1 is structural representation of the present utility model;
In figure, 1 is frame; 2 is fuselage; 3 is driving engine; 4 is rotor; 5 is screw propeller; 6 is tail vane; 7 is joystick; 8 is instrument; 9 is alighting gear.
Detailed description of the invention
Below in conjunction with accompanying drawing, the utility model will be further described.
A kind of autogyro, comprises frame, fuselage, driving engine, rotor, screw propeller, tail vane, joystick, instrument, alighting gear, frame upper end connects rotor, and driving engine is between tail vane seat storehouse, be provided with instrument and joystick in passenger cabin, driving engine is connected with screw propeller, is provided with alighting gear below frame, described rotor is for be made up of two blades, and blade is fixed on frame upper end by oar axle.
Described screw propeller is connected with driving engine by horizontal drive power-transfer clutch.
The rotor face of described rotor is for tilting backwards setting.
The blade of described rotor is that oar is turned round in aerodynamic force change.
Specifically, the utility model can realize following effect:
1, safety is high
Power due to the rotor wing rotation of autogyro be by before aircraft so that obtain.Just in case driving engine aloft parking screw propeller has not turned, now cyclogyro is because have the state flown before inertia continues maintenance, and because gravity is while highly declining, also just having had relative wind from bottom to top, rotor relies on potential energy be the kinetic energy of rotor wing rotation thus produce lift.Like this, revolving Ji machine just can with the landing of gliding of the manoeuvring safety of aviator ground.
2, landing is apart from short
Autogyro has individual distinguishing feature, and the distance of landing run being exactly it is shorter than takeoff distance widely, even handles well can not to slide to run to land on the spot.
3, stability is high, and wind resistance is strong
The cyclogyro flight training handbook of the U.S. is said: " stability of cyclogyro is the highest in all aerocrafts ".It can regulate automatically, makes fuselage have good pitching stability, roll stability and speed stability.
The great advantage that autogyro is different from other class aircraft is that wind loading rating is high, and when taking off, it also likes there is wind.For autogyro, wind is conducive to starting and the acceleration rotation of rotor, can shorten sliding distance of running, and when reaching enough large wind speed, general autogyro also can not need sliding race standing start.
4, there is higher cost performance
Because autogyro is simple relative to helicopter structure, do not have tail-rotor driving system, retarder, auto-bank unit and main-rotor drive system, so not only price is low, and fault rate is also low.In addition working service is simple and convenient, and required expense is also low.It is handy, safe for autogyro, feature easily, makes it will occupy a tiny space in the aerocraft family in future.
Last it is noted that obviously, above-described embodiment is only for the application's example is clearly described, and the restriction not to embodiment.For those of ordinary skill in the field, can also make other changes in different forms on the basis of the above description.Here exhaustive without the need to also giving all embodiments.And thus the apparent change of amplifying out or variation be still among the protection domain of the application's type.
Claims (1)
1. an autogyro, comprise frame, fuselage, driving engine, rotor, screw propeller, tail vane, joystick, instrument, alighting gear, it is characterized in that, frame upper end connects rotor, driving engine is between tail vane passenger cabin, instrument and joystick is provided with in passenger cabin, driving engine is connected with screw propeller, alighting gear is provided with below frame, described rotor is for be made up of two blades, blade is fixed on frame upper end by oar axle, described screw propeller is connected with driving engine by horizontal drive power-transfer clutch, the rotor face of described rotor is for tilting backwards setting, the blade of described rotor is that oar is turned round in aerodynamic force change.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420002191.0U CN204210731U (en) | 2014-01-03 | 2014-01-03 | Autogyro |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420002191.0U CN204210731U (en) | 2014-01-03 | 2014-01-03 | Autogyro |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204210731U true CN204210731U (en) | 2015-03-18 |
Family
ID=52979428
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420002191.0U Expired - Fee Related CN204210731U (en) | 2014-01-03 | 2014-01-03 | Autogyro |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204210731U (en) |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105947198A (en) * | 2016-05-03 | 2016-09-21 | 中国航天空气动力技术研究院 | Triphibian air cushion rotor craft structure |
| CN106143884A (en) * | 2015-03-19 | 2016-11-23 | 王略 | Complete manual gyroplane |
| WO2017036080A1 (en) * | 2015-09-02 | 2017-03-09 | 河南三和航空工业有限公司 | Parachute equipped autogyro and manufacturing method |
| CN107738745A (en) * | 2017-09-28 | 2018-02-27 | 宝鸡欧亚化工设备制造厂 | A kind of active brake type gyroplane |
| CN107792356A (en) * | 2017-09-28 | 2018-03-13 | 宝鸡欧亚化工设备制造厂 | One kind takes off vertically type gyroplane |
| CN109131823A (en) * | 2018-09-21 | 2019-01-04 | 湖南湘晨飞机工业有限公司 | A kind of gyroplane casing |
| CN109383788A (en) * | 2018-11-22 | 2019-02-26 | 南京航空航天大学 | A kind of cross flow fan lift-rising autogyro |
-
2014
- 2014-01-03 CN CN201420002191.0U patent/CN204210731U/en not_active Expired - Fee Related
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106143884A (en) * | 2015-03-19 | 2016-11-23 | 王略 | Complete manual gyroplane |
| CN106143884B (en) * | 2015-03-19 | 2019-09-06 | 王略 | Full manual control gyroplane |
| WO2017036080A1 (en) * | 2015-09-02 | 2017-03-09 | 河南三和航空工业有限公司 | Parachute equipped autogyro and manufacturing method |
| CN105947198A (en) * | 2016-05-03 | 2016-09-21 | 中国航天空气动力技术研究院 | Triphibian air cushion rotor craft structure |
| CN105947198B (en) * | 2016-05-03 | 2018-05-01 | 中国航天空气动力技术研究院 | One kind three is dwelt air cushion rotor craft configuration |
| CN107738745A (en) * | 2017-09-28 | 2018-02-27 | 宝鸡欧亚化工设备制造厂 | A kind of active brake type gyroplane |
| CN107792356A (en) * | 2017-09-28 | 2018-03-13 | 宝鸡欧亚化工设备制造厂 | One kind takes off vertically type gyroplane |
| CN109131823A (en) * | 2018-09-21 | 2019-01-04 | 湖南湘晨飞机工业有限公司 | A kind of gyroplane casing |
| CN109383788A (en) * | 2018-11-22 | 2019-02-26 | 南京航空航天大学 | A kind of cross flow fan lift-rising autogyro |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20180925 Address after: 471000 725, room 7, international hotel, Huayang Plaza, No. 88, Kai Xuan Road, Jianxi District, Luoyang, Henan. Patentee after: Luoyang Luo Depp blue rotor Technology Co.,Ltd. Address before: 510170 901, Longqing north 3, Liwan District, Guangzhou, Guangdong. Patentee before: Su Guibin |
|
| TR01 | Transfer of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20150318 Termination date: 20220103 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |