CN204623843U - A kind of wind ball cylinder wing aircraft - Google Patents
A kind of wind ball cylinder wing aircraft Download PDFInfo
- Publication number
- CN204623843U CN204623843U CN201520294184.7U CN201520294184U CN204623843U CN 204623843 U CN204623843 U CN 204623843U CN 201520294184 U CN201520294184 U CN 201520294184U CN 204623843 U CN204623843 U CN 204623843U
- Authority
- CN
- China
- Prior art keywords
- wing
- electrical motor
- clutch
- fuselage
- wind ball
- 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.)
- Expired - Fee Related
Links
Landscapes
- Wind Motors (AREA)
Abstract
A kind of wind ball cylinder wing aircraft, belongs to aviation aircraft technical field.Comprise fuselage, engine installation, left wing, right flank, empennage and alighting gear.Engine installation comprises energy supplyystem and propelling unit or chest expander.Left wing and right flank structure and measure-alike and be symmetrically arranged in the left and right sides of the longitudinal plane of symmetry of fuselage.Left wing comprises left electrical motor, left clutch, left wing's axle, roll left a wing and left wind ball.Right flank comprises right electrical motor, right clutch, right flank axle, the right cylinder wing and right wind ball.Under the effect of front incoming flow, Zuo Fengqiu and You Feng club rotates, and turns right on the left of fuselage, and the dynamic wing clockwise direction that rolls left of left wind spherical zone rotates; Right wind spherical zone moves the right cylinder wing and also does clockwise direction rotation.Under the combined action of the circulation of roll left a wing and the right cylinder wing of front incoming flow and rotation, roll left a wing and the right cylinder wing produce lift upwards, thus this aircraft can aloft be flown.This invention aircraft can short take-off and landing (STOL), and flight maneuver is flexible.
Description
Technical field
A kind of wind ball cylinder wing aircraft, belongs to aviation aircraft technical field, particularly relates to a kind of cylinder wing aircraft.
Background technology
Traditional aircraft wing is fixing, and the scope that its lift size is adjustable is little, more difficultly realizes short take-off and landing, and the alerting ability of aircraft is poor.
Summary of the invention
The object of the invention is the above-mentioned deficiency overcoming traditional fixed wing aircraft, invention is a kind of can short take-off and landing, flight maneuver wind ball cylinder wing aircraft flexibly.
A kind of wind ball cylinder wing aircraft, comprises fuselage, engine installation, left wing, right flank, empennage and alighting gear.Maneuvering system and airborne equipment is furnished with in fuselage.Bikini wheel undercarriage after alighting gear adopts.Engine installation comprises energy supplyystem and propelling unit or chest expander.When adopting chest expander to make active force, chest expander is installed on the front end of fuselage; The mode that chest expander adopts piston engine to add the mode of screw propeller or electrical motor to add screw propeller, piston engine fuel oil provides the energy; Adopt the lithium battery power supply using convenient charging during electrical motor.When adopting propelling unit to make active force, propelling unit is installed on above the postmedian of fuselage, and propelling unit adopts turbojet engine or fanjet, makes the energy with fuel oil.Left wing and right flank structure and measure-alike and be symmetrically arranged in the left and right sides of the longitudinal plane of symmetry of fuselage.Left wing comprises left electrical motor, left clutch, left wing's axle, roll left a wing and left wind ball.Right flank comprises right electrical motor, right clutch, right flank axle, the right cylinder wing and right wind ball.Zuo Fengqiu is identical with right wind spherical structure and be arranged symmetrically with, and Zuo Fengqiu is fixed on the left end of a wing that rolls left with a wing that rolls left, and right wind ball and the right cylinder wing are fixed on the right-hand member of the right cylinder wing.The right-hand member of a wing of rolling left is connected with left clutch by left wing's axle, and left wing's axle is arranged on the left side wall of fuselage by bearing; The left end of the right cylinder wing is connected with right clutch by right flank axle, and right flank axle is arranged on the right side wall of fuselage by bearing.Left electrical motor, left clutch, right electrical motor and right clutch are arranged in fuselage.Along with this wind ball cylinder wing aircraft moves ahead, under the effect of front incoming flow, Zuo Fengqiu and You Feng club rotates, and its rotation direction is: eye right from the left side of fuselage, and Zuo Fengqiu and right wind ball are all rotated in a clockwise direction.The dynamic wing clockwise direction that rolls left of left wind spherical zone rotates; Right wind spherical zone moves the right cylinder wing and also does clockwise direction rotation.Under the combined action of the circulation of roll left a wing and the right cylinder wing of front incoming flow and rotation, roll left a wing and the right cylinder wing produce lift upwards, thus this aircraft can aloft be flown.The power of electrical motor and right electrical motor of keeping left during landing drives and to roll left a wing and right cylinder wing clickwise.Connect left electrical motor identical with the right clutch structure connecting right electrical motor and right flank axle with the left clutch of left wing axle, they are free-wheel clutch, when one end be connected with left electrical motor of left clutch is fixed, one end be connected with left wing axle of left clutch can and be merely able to make clickwise; In like manner, when one end be connected with right electrical motor of right clutch is fixed, one end be connected with right flank axle of right clutch can and be merely able to make clickwise.
The left wing of a kind of wind of the present invention ball cylinder wing aircraft and the mode of operation of right flank comprise: mainly keep left when this is taken off and lands electrical motor and right electrical motor drive roll left a wing and the right cylinder wing to rotate respectively; When cruising, main incoming flow on the front blows Zuo Fengqiu and right wind ball and rotates and drive roll left a wing and the right cylinder wing to rotate respectively.Namely the horizontal rolling in the left and right of this aircraft is sidewindered and mainly to be realized by the roll left velocity of rotation of a wing and the right cylinder wing of the left electrical motor of control and right direct motor drive, look forward from tail, when left electrical motor is faster than right electrical motor, the lift of left wing is greater than the lift of right flank, this aircraft cw sidewinders, and namely sidewinders to the right; When right electrical motor is faster than left electrical motor, the lift of right flank is greater than the lift of left wing, and this aircraft conter clockwise sidewinders, and namely sidewinders left.
Empennage comprises tailplane and vertical tail, and tailplane is made up of the fixed part of leading portion and horizontal stabilizer and back segment moving part and elevating rudder, and vertical tail is made up of the fixed part of leading portion and fixed fin and back segment moving part and yaw rudder.Elevating rudder can deflect up and down under the manipulation of maneuvering system, upward deflects and this aircraft can be made to come back, realize facing upward; The change of team of elevating rudder downward bias makes this aircraft bow, and realizes nutation.Yaw rudder is deflection under the manipulation of maneuvering system, and this aircraft can be made to go off course to the left or to the right.
This invention aircraft can short take-off and landing (STOL), and flight maneuver is flexible.
Accompanying drawing explanation
Fig. 1 is the schematic top plan view of a kind of wind ball of the present invention cylinder wing aircraft.
In figure, 1-fuselage; 2-chest expander; 3-left wing, the left electrical motor of 31-, 32-left clutch, 33-left wing axle, 34-rolls left a wing, the left wind ball of 35-; 4-right flank, the right electrical motor of 41-, 42-right clutch, 43-right flank axle, the right cylinder wing of 44-, the right wind ball of 45-; 5-tailplane, 51-horizontal stabilizer, 52-elevating rudder; 6-vertical tail, 61-fixed fin, 62-yaw rudder; 7-alighting gear.
Detailed description of the invention
Now 1 couple of the present invention is illustrated by reference to the accompanying drawings: a kind of wind ball cylinder wing aircraft, comprises fuselage 1, engine installation, left wing 3, right flank 4, empennage and alighting gear 7.Maneuvering system and airborne equipment is furnished with in fuselage 1.Alighting gear 7 adopts rear bikini wheel undercarriage.Engine installation comprises energy supplyystem and chest expander 2.Chest expander 2 is installed on the front end of fuselage 1, and chest expander 2 adopts piston engine to add the mode of screw propeller, provides the energy with fuel oil.Left wing 3 and right flank 4 structure and measure-alike and be symmetrically arranged in the left and right sides of the longitudinal plane of symmetry of fuselage 1.Left wing 3 comprises left electrical motor 31, left clutch 32, left wing's axle 33, roll left a wing 34 and left wind ball 35.Right flank 4 comprises right electrical motor 41, right clutch 42, right flank axle 43, the right cylinder wing 44 and right wind ball 45.Left electrical motor 31 is identical with right electrical motor 41 structure and parameter, adopts the lithium battery power supply of convenient charging.Left wind ball 35 is identical with right wind ball 45 structure and be arranged symmetrically with, and left wind ball 35 and the wing 34 that rolls left are fixed on the left end of the wing 34 that rolls left, and right wind ball 45 and the right cylinder wing 44 are fixed on the right-hand member of the right cylinder wing 44.The right-hand member of a wing 34 of rolling left is connected with left clutch 32 by left wing's axle 33, and left wing's axle 33 is arranged on the left side wall of fuselage 1 by bearing; The left end of the right cylinder wing 44 is connected with right clutch 42 by right flank axle 43, and right flank axle 43 is arranged on the right side wall of fuselage 1 by bearing.Left electrical motor 31, left clutch 32, right electrical motor 41 and right clutch 42 are arranged in fuselage 1.Along with this wind ball cylinder wing aircraft moves ahead, under the effect of front incoming flow, left wind ball 35 and right wind ball 45 can rotate, and its rotation direction is: eye right from the left side of fuselage 1, and left wind ball 35 and right wind ball 45 are all rotated in a clockwise direction.Left wind ball 35 drives a wing 34 clockwise direction that rolls left to rotate; Right wind ball 45 drives the right cylinder wing 44 also to do clockwise direction rotation.Under the combined action of the circulation of roll left a wing 34 and the right cylinder wing 44 of front incoming flow and rotation, roll left a wing 34 and the right cylinder wing 44 produce lift upwards, thus this aircraft can aloft be flown.The power of electrical motor 31 and right electrical motor 41 of keeping left during landing drives and to roll left a wing 34 and the right cylinder wing 44 clickwise.The left clutch 32 connecting left electrical motor 31 and left wing axle 33 is with to connect right electrical motor 41 identical with right clutch 42 structure of right flank axle 43, they are free-wheel clutch, when one end be connected with left electrical motor 31 of left clutch 32 is fixed, one end be connected with left wing axle 33 of left clutch 31 can and be merely able to make clickwise; In like manner, when one end be connected with right electrical motor 41 of right clutch 42 is fixed, one end be connected with right flank axle 43 of right clutch 42 can and be merely able to make clickwise.
The left wing 3 of a kind of wind of the present invention ball cylinder wing aircraft and the mode of operation of right flank 4 comprise: mainly keep left when this is taken off and lands electrical motor 31 and right electrical motor 41 drive roll left a wing 34 and the right cylinder wing 44 to rotate respectively; When cruising, main incoming flow on the front blows left wind ball 35 and right wind ball 45 and rotates and drive roll left a wing 34 and the right cylinder wing 44 to rotate respectively.Namely the horizontal rolling in left and right of this aircraft is sidewindered and is mainly driven the velocity of rotation of roll left a wing 34 and the right cylinder wing 44 to realize by the left electrical motor 31 of control and right electrical motor 41, look forward from tail, when left electrical motor 31 is faster than right electrical motor 41, the lift of left wing 3 is greater than the lift of right flank 4, this aircraft cw sidewinders, and namely sidewinders to the right; When right electrical motor 41 is faster than left electrical motor 31, the lift of right flank 4 is greater than the lift of left wing 3, and this aircraft conter clockwise sidewinders, and namely sidewinders left.
Empennage comprises tailplane 5 and vertical tail 6, tailplane 5 is made up of the fixed part of leading portion and horizontal stabilizer 51 and back segment moving part and elevating rudder 52, and vertical tail 6 is made up of the fixed part of leading portion and fixed fin 61 and back segment moving part and yaw rudder 62.Elevating rudder 52 can deflect up and down under the manipulation of maneuvering system, upward deflects and this aircraft can be made to come back, realize facing upward; The change of team of elevating rudder 52 downward bias makes this aircraft bow, and realizes nutation.Yaw rudder 62 is deflection under the manipulation of maneuvering system, and this aircraft can be made to go off course to the left or to the right.
Claims (5)
1. a wind ball cylinder wing aircraft, comprises fuselage (1), engine installation, left wing (3), right flank (4), empennage and alighting gear (7), it is characterized in that: fuselage is furnished with maneuvering system and airborne equipment in (1); Engine installation comprises energy supplyystem and propelling unit or chest expander (2); Left wing (3) and right flank (4) structure and measure-alike and be symmetrically arranged in the left and right sides of fuselage (1) longitudinal plane of symmetry; Left wing (3) comprises left electrical motor (31), left clutch (32), left wing's axle (33), roll left a wing (34) and left wind ball (35); Right flank (4) comprises right electrical motor (41), right clutch (42), right flank axle (43), the right cylinder wing (44) and right wind ball (45); Left electrical motor (31) is identical with right electrical motor (41) structure and parameter; Zuo Fengqiu (35) is identical with right wind ball (45) structure and be arranged symmetrically with, and Zuo Fengqiu (35) is fixed on the left end of a wing (34) of rolling left with the wing (34) that rolls left, and right wind ball (45) and the right cylinder wing (44) are fixed on the right-hand member of the right cylinder wing (44); The right-hand member of a wing (34) of rolling left is connected with left clutch (32) by left wing's axle (33), and left wing's axle (33) is arranged on by bearing on the left side wall of fuselage (1); The left end of the right cylinder wing (44) is connected with right clutch (42) by right flank axle (43), and right flank axle (43) is arranged on by bearing on the right side wall of fuselage (1); Left electrical motor (31), left clutch (32), right electrical motor (41) and right clutch (42) are arranged in fuselage (1); Connect left electrical motor (31) identical with right clutch (42) structure connecting right electrical motor (41) and right flank axle (43) with the left clutch (32) of left wing's axle (33), they are free-wheel clutch.
2. a kind of wind ball cylinder wing aircraft according to claim 1, is characterized in that: bikini wheel undercarriage after alighting gear (7) adopts.
3. a kind of wind ball cylinder wing aircraft according to claim 1, is characterized in that: chest expander (2) is installed on the front end of fuselage (1); The mode that chest expander (2) adopts piston engine to add the mode of screw propeller or electrical motor to add screw propeller, piston engine fuel oil provides the energy; Adopt the lithium battery power supply using convenient charging during electrical motor.
4. a kind of wind ball cylinder wing aircraft according to claim 1, is characterized in that: propelling unit is installed on above the postmedian of fuselage (1), and propelling unit adopts turbojet engine or fanjet, makes the energy with fuel oil.
5. a kind of wind ball cylinder wing aircraft according to claim 1, is characterized in that: left electrical motor (31) and right electrical motor (41) adopt the lithium battery power supply of convenient charging.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520294184.7U CN204623843U (en) | 2015-05-08 | 2015-05-08 | A kind of wind ball cylinder wing aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520294184.7U CN204623843U (en) | 2015-05-08 | 2015-05-08 | A kind of wind ball cylinder wing aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204623843U true CN204623843U (en) | 2015-09-09 |
Family
ID=54042896
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520294184.7U Expired - Fee Related CN204623843U (en) | 2015-05-08 | 2015-05-08 | A kind of wind ball cylinder wing aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204623843U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104787336A (en) * | 2015-05-08 | 2015-07-22 | 佛山市神风航空科技有限公司 | Wind-ball roller-wing aircraft |
-
2015
- 2015-05-08 CN CN201520294184.7U patent/CN204623843U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104787336A (en) * | 2015-05-08 | 2015-07-22 | 佛山市神风航空科技有限公司 | Wind-ball roller-wing aircraft |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN102133926B (en) | Tailstock type vertical take-off and landing unmanned aerial vehicle | |
| CN202754143U (en) | Rotating engine vertical take-off and landing aircraft | |
| CN101353084A (en) | Light aerobat capable of landing or taking-off vertically | |
| CN110077588A (en) | It is a kind of can the sea, land and air latent four of VTOL dwell aircraft | |
| CN105083550A (en) | Fixed-wing aircraft realizing vertical take-off and landing | |
| CN202481309U (en) | Vector power vertical take-off and landing aircraft and vector power system thereof | |
| CN205022861U (en) | VTOL fixed wing aircraft | |
| CN205022862U (en) | Power device and fixed wing aircraft with mechanism of verting | |
| CN202896880U (en) | Spherical micro unmanned aerial vehicle | |
| CN104443353A (en) | Wing-changeable airplane | |
| CN106005371B (en) | Difference directly drives dynamic three rudder face unmanned planes entirely | |
| CN104875875A (en) | Air wing type airflow directional load transportation air vehicle | |
| CN102849210A (en) | Spherical small unmanned aircraft | |
| CN204642148U (en) | A kind of leading edge of a wing is equipped with the aircraft that wind ball drives wind wheel | |
| CN204623843U (en) | A kind of wind ball cylinder wing aircraft | |
| CN205131643U (en) | Front and back wing multiaxis aircraft | |
| CN210416978U (en) | Novel vertical take-off and landing aircraft | |
| CN104760684A (en) | Airplane provided with wind-ball-driving wind wheels on main lift force front edges | |
| CN204473119U (en) | Lightweight unmanned plane | |
| CN104787305A (en) | Aircraft with wind ball driven wind wheels at wing leading edges | |
| CN204606200U (en) | A kind of leading edge of a wing drives the aircraft of wind wheel with wind ball | |
| CN202526908U (en) | Double-leaf propeller of model plane | |
| CN202481307U (en) | Four-propeller aircraft taking off and landing vertically | |
| CN204674321U (en) | Light-weight vertical landing hovercar | |
| CN104773282A (en) | Aircraft with leading edge provided with wind balls for driving wind wheels |
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: 20220419 Address after: 528400 floor shop 6, erheng street, Changshou street, Yongning, Xiaolan Town, Zhongshan City, Guangdong Province Patentee after: Guangdong Yiyuan Ecological Garden Co.,Ltd. Address before: 528500 room 402, Fu Wan Jiangwan Road, Hecheng street, Gaoming District, Foshan, Guangdong, China, 78 Patentee before: FOSHAN SHENFENG AVIATION TECHNOLOGY Co.,Ltd. |
|
| TR01 | Transfer of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20150909 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |