CN104192301B - A kind of manpower variable wing plane - Google Patents
A kind of manpower variable wing plane Download PDFInfo
- Publication number
- CN104192301B CN104192301B CN201410492981.6A CN201410492981A CN104192301B CN 104192301 B CN104192301 B CN 104192301B CN 201410492981 A CN201410492981 A CN 201410492981A CN 104192301 B CN104192301 B CN 104192301B
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- aircraft
- air accumulator
- control system
- right flank
- left wing
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Abstract
A kind of manpower variable wing plane, belongs to aeronautical technology field. Comprise fuselage, foldable propeller, movable left wing, activity right flank, empennage, undercarriage, air accumulator, control system and people's force transmission system. Pilot control control system is controlled the folding of movable left wing and activity right flank, and controls this aircraft and turn and pitching flying attitude. The table top of transmitting station and the angle of horizontal plane are between 14 ° to 46 °. Adopt gas jet mode to take off, driver opens the injection cock of air accumulator by control system, and the gas in air accumulator is ejection at a high speed to the back lower place, and under its reaction, this aircraft flies out to front upper place at a high speed. After this aircraft reaches parabola summit, driver's manipulation activities left wing and activity right flank are synchronously opened simultaneously gradually, start human-powered flight's pattern thereby then foldable propeller is rotated with pedal people force transmission system. This aircraft energy-saving high-efficiency environment-friendly and safety.
Description
Technical field
A kind of manpower variable wing plane, belongs to aeronautical technology field, relates in particular to a kind of variable wing plane.
Background technology
Traditional man-powered aircraft, flies by people's strength completely, and the distance of flight is far away not. And it is harder to take off, and runway that need to be longer.
Summary of the invention
The object of the invention is to overcome the above-mentioned deficiency of traditional man-powered aircraft, invention one is taken off without long runway, can be flown more remote manpower variable wing plane.
A kind of manpower variable wing plane, comprises fuselage, foldable propeller, movable left wing, activity right flank, empennage, undercarriage, air accumulator, control system and people's force transmission system. Driver is positioned at fuselage leading portion, and air accumulator is placed in stage casing in fuselage. Before taking off, in air accumulator, be full of gases at high pressure, gas used is air or nitrogen. Movable left wing is identical with activity right flank structure to be symmetrically arranged in the left and right sides of the symmetrical longitudinal section of fuselage, and is placed in fuselage top. Empennage comprises vertical tail and tailplane. The rudder of the fixed fin that vertical tail is fixed by front portion and rear portion activity forms; The elevator of the horizontal stabilizer that tailplane is fixed by front portion and rear portion activity form. Elevator is upper and lower deflection under the manipulation of control system, upward deflects and can make this aircraft come back, and realization is faced upward; The change of team of elevator downward bias is bowed this aircraft, realizes nutation. Rudder is deflection under the manipulation of control system, and this aircraft is gone off course to the left or to the right. Undercarriage adopts bikini wheel undercarriage. Pilot control control system is controlled the folding of movable left wing and activity right flank, and controls this aircraft and turn and pitching flying attitude. Be fixedly installed in ground for this transmitting station of taking off use. The table top of transmitting station and the angle of horizontal plane are between 14 ° to 46 °, and table top is equipped with to hold three guide piles of this wheel of aircraft landing gear.
The flying method of manpower variable wing plane of the present invention is: adopt gas jet mode to take off, this aircraft first movable left wing and activity right flank being drawn in is carried on transmitting station, and three wheels of undercarriage are placed in respectively three of transmitting station table top above guide pile. Driver opens the injection cock of air accumulator by control system, gas in air accumulator is ejection at a high speed to the back lower place, under its reaction, this aircraft flies out to front upper place at a high speed, after air accumulator internal gas pressure equates with ambient pressure, flies to front upper place because this aircraft of inertia continues to be similar to parabolical track. After this aircraft reaches parabola summit, driver's manipulation activities left wing and activity right flank are synchronously opened simultaneously gradually, start human-powered flight's pattern thereby then foldable propeller is rotated with pedal people force transmission system. Driver realizes this aircraft by manipulation empennage and turns and pitching flying attitude. Finally a more smooth land landing.
The outstanding advantages of a kind of manpower variable wing plane of this invention is: energy-saving high-efficiency environment-friendly. Owing to taking off to the procedure activation left wing of highest point and activity right flank in closing up state, resistance is little, and energy loss is little, and efficiency is high, can fly fartherly.
A kind of manpower variable wing plane of the present invention is suitable for sports and amusement activity and Aerial photography.
Brief description of the drawings
Fig. 1 is a kind of manpower variable wing plane of the present invention schematic side view when standby for takeoff on transmitting station; Fig. 2 is the folding screw of a kind of manpower variable wing plane of the present invention, left movable wing and the right movable wing schematic top plan view while drawing in; Fig. 3 is the folding screw of a kind of manpower variable wing plane of the present invention, left movable wing and the right movable wing schematic top plan view while opening.
In figure, 1-fuselage, 2-foldable propeller, the movable left wing of 3-, 4-activity right flank, 5-empennage, 51-fixed fin, 52-rudder, 53-horizontal stabilizer, 54-elevator, 6-undercarriage, 7-air accumulator, 71-injection cock, 8-transmitting station, 81-guide pile, 9-ground. The direction that in Fig. 1, the direction indication of the larger arrow indication in the upper right corner a kind of manpower variable wing plane of the present invention takes off, with horizontal plane angle at 45 °.
Detailed description of the invention
Now 1 ~ 3 couple of the present invention is illustrated by reference to the accompanying drawings: a kind of manpower variable wing plane, comprises fuselage 1, foldable propeller 2, movable left wing 3, activity right flank 4, empennage 5, undercarriage 6, air accumulator 7, control system and people's force transmission system. Driver is positioned at fuselage 1 leading portion, and air accumulator 7 is placed in the interior stage casing of fuselage 1. Before taking off, in air accumulator 7, be full of high pressure nitrogen. Movable left wing 3 is identical with activity right flank 4 structures is symmetrically arranged in the left and right sides of fuselage 1 symmetrical longitudinal section, and is placed in fuselage 1 top. Empennage 5 comprises vertical tail and tailplane. The fixed fin 51 that vertical tail is fixed by front portion and the rudder 52 of rear portion activity form; The horizontal stabilizer 53 that tailplane is fixed by front portion and the elevator 54 of rear portion activity form. Elevator 54 is upper and lower deflection under the manipulation of control system, upward deflects and can make this aircraft come back, and realization is faced upward; The elevator 54 downward bias change of teams are bowed this aircraft, realize nutation. Rudder 52 is deflection under the manipulation of control system, and this aircraft is gone off course to the left or to the right. Undercarriage 6 adopts bikini wheel undercarriage. Pilot control control system is controlled the folding of movable left wing 3 and activity right flank 4, and controls this aircraft and turn and pitching flying attitude. Be fixedly installed in ground 9 for this transmitting station 8 of taking off use. The table top of transmitting station 8 and the angle of horizontal plane are 45 °, and table top is equipped with to hold three guide piles 81 of this wheel of aircraft landing gear.
The flying method of manpower variable wing plane of the present invention is: adopt gas jet mode to take off, this aircraft first movable left wing 3 and activity right flank 4 being drawn in is carried on transmitting station 8, and three wheels of undercarriage 6 are placed in respectively above three guide piles 81 of transmitting station 8 table tops. Driver opens the injection cock 71 of air accumulator 7 by control system, gas in air accumulator 7 is ejection at a high speed to the back lower place, under its reaction, this aircraft flies out to front upper place at a high speed, after air accumulator 7 internal gas pressures equate with ambient pressure, flies to front upper place because this aircraft of inertia continues to be similar to parabolical track. After this aircraft reaches parabola summit, driver's manipulation activities left wing 3 and activity right flank 4 are synchronously opened simultaneously gradually, start human-powered flight's pattern thereby then foldable propeller 2 is rotated with pedal people force transmission system. Driver realizes this aircraft by manipulation empennage 5 and turns and pitching flying attitude. Finally a more smooth land landing.
Claims (3)
1. a manpower variable wing plane, is characterized in that: comprise fuselage (1), foldable propeller (2), movable left wing (3), activity right flank (4), empennage (5), undercarriage (6), air accumulator (7), control system and people's force transmission system; Driver is positioned at fuselage (1) leading portion, and air accumulator (7) is placed in the interior stage casing of fuselage (1); Air accumulator before taking off is full of gases at high pressure in (7); In air accumulator (7), gas used is air or nitrogen; Be symmetrically arranged in the left and right sides of fuselage (1) symmetrical longitudinal section identical with activity right flank (4) structure of movable left wing (3), and be placed in fuselage (1) top; Empennage (5) comprises vertical tail and tailplane; Vertical tail is made up of fixed fin (51) and rudder (52); Tailplane is made up of horizontal stabilizer (53) and elevator (54); Elevator (54) is upper and lower deflection under the manipulation of control system, upward deflects and can make this aircraft come back, and realization is faced upward; The change of team of elevator (54) downward bias is bowed this aircraft, realizes nutation; Rudder (52) deflection under the manipulation of control system, goes off course this aircraft to the left or to the right; Undercarriage (6) adopts bikini wheel undercarriage; Pilot control control system is controlled the folding of movable left wing (3) and activity right flank (4), and controls this aircraft and turn and pitching flying attitude; Be fixedly installed in ground (9) for this transmitting station (8) of taking off use; The table top of transmitting station (8) and the angle of horizontal plane are between 14 ° to 46 °, and table top is equipped with to hold three guide piles (81) of this undercarriage (6) wheel.
2. a kind of manpower variable wing plane according to claim 1, is characterized in that: the table top of transmitting station (8) and the angle of horizontal plane are 45 °.
3. the flying method of the manpower variable wing plane as described in claim 1 ~ 2 any one, it is characterized in that: adopt gas jet mode to take off, it is upper that this aircraft first movable left wing (3) and activity right flank (4) being drawn in is carried to transmitting station (8), and three guide piles (81) that three wheels of undercarriage (6) are placed in respectively transmitting station (8) table top above; Driver opens the injection cock (71) of air accumulator (7) by control system, gas in air accumulator (7) is ejection at a high speed to the back lower place, under its reaction, this aircraft flies out to front upper place at a high speed, after air accumulator (7) internal gas pressure equates with ambient pressure, flies to front upper place because this aircraft of inertia continues to be similar to parabolical track; Thereby after this aircraft reaches parabola summit, driver's manipulation activities left wing (3) and activity right flank (4) are synchronously opened simultaneously gradually, then make foldable propeller (2) with pedal people force transmission system rotate to start human-powered flight's pattern; Driver realizes this aircraft by manipulation empennage (5) and turns and pitching flying attitude; Finally a smooth land landing.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410492981.6A CN104192301B (en) | 2014-09-24 | 2014-09-24 | A kind of manpower variable wing plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410492981.6A CN104192301B (en) | 2014-09-24 | 2014-09-24 | A kind of manpower variable wing plane |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN104192301A CN104192301A (en) | 2014-12-10 |
| CN104192301B true CN104192301B (en) | 2016-05-11 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410492981.6A Expired - Fee Related CN104192301B (en) | 2014-09-24 | 2014-09-24 | A kind of manpower variable wing plane |
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| Country | Link |
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| CN (1) | CN104192301B (en) |
Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110606192A (en) * | 2019-10-24 | 2019-12-24 | 中国航空工业集团公司沈阳飞机设计研究所 | Airplane front wheel turning control method |
| CN111717409B (en) * | 2020-06-23 | 2022-04-12 | 添津人工智能通用应用系统(天津)有限公司 | High-pressure pneumatic boosting take-off device of light unmanned aerial vehicle |
| CN113353260A (en) * | 2021-06-17 | 2021-09-07 | 淮阴工学院 | Medium-short distance emission type transportation device and method |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR435410A (en) * | 1910-10-20 | 1912-02-29 | Joseph Migliorino | Flying machine |
| US2012104A (en) * | 1934-06-14 | 1935-08-20 | Loske Frank | Aeroplane |
| FR890435A (en) * | 1941-07-04 | 1944-02-08 | Glider with a pedal device controlled by human force | |
| CN2344064Y (en) * | 1998-02-25 | 1999-10-20 | 纪乃波 | Aerodynamic toy |
| WO2011137335A1 (en) * | 2010-04-30 | 2011-11-03 | Elbit Systems Of America, Llc | Unmanned aerial vehicle based sonar buoy |
| CN103587686A (en) * | 2013-12-02 | 2014-02-19 | 哈尔滨工业大学 | Catapulted folding wing flying robot |
-
2014
- 2014-09-24 CN CN201410492981.6A patent/CN104192301B/en not_active Expired - Fee Related
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR435410A (en) * | 1910-10-20 | 1912-02-29 | Joseph Migliorino | Flying machine |
| US2012104A (en) * | 1934-06-14 | 1935-08-20 | Loske Frank | Aeroplane |
| FR890435A (en) * | 1941-07-04 | 1944-02-08 | Glider with a pedal device controlled by human force | |
| CN2344064Y (en) * | 1998-02-25 | 1999-10-20 | 纪乃波 | Aerodynamic toy |
| WO2011137335A1 (en) * | 2010-04-30 | 2011-11-03 | Elbit Systems Of America, Llc | Unmanned aerial vehicle based sonar buoy |
| CN103587686A (en) * | 2013-12-02 | 2014-02-19 | 哈尔滨工业大学 | Catapulted folding wing flying robot |
Also Published As
| Publication number | Publication date |
|---|---|
| CN104192301A (en) | 2014-12-10 |
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| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CB03 | Change of inventor or designer information |
Inventor after: Zhong Xueting Inventor before: Wang Zhicheng |
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| CB03 | Change of inventor or designer information | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20170908 Address after: 015000, No. 8, Lane 8, Heping South Road, Heping Town, Dengkou County, Inner Mongolia, Bayannaoer Patentee after: Zhong Xueting Address before: Foshan City, Guangdong province 528500 city streets Gaoming District No. 78 Jiangwan Road, room 402 Fu Wan Patentee before: Shenfeng science and technology of aviation Co., Ltd of Foshan City |
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| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160511 Termination date: 20180924 |
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| CF01 | Termination of patent right due to non-payment of annual fee |