CN204642148U - A kind of leading edge of a wing is equipped with the aircraft that wind ball drives wind wheel - Google Patents
A kind of leading edge of a wing is equipped with the aircraft that wind ball drives wind wheel Download PDFInfo
- Publication number
- CN204642148U CN204642148U CN201520294192.1U CN201520294192U CN204642148U CN 204642148 U CN204642148 U CN 204642148U CN 201520294192 U CN201520294192 U CN 201520294192U CN 204642148 U CN204642148 U CN 204642148U
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- Prior art keywords
- wing
- electrical motor
- wind wheel
- clutch
- wind
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- 238000009434 installation Methods 0.000 claims abstract description 7
- 210000000038 chest Anatomy 0.000 claims description 10
- 239000000295 fuel oil Substances 0.000 claims description 5
- WHXSMMKQMYFTQS-UHFFFAOYSA-N lithium Chemical compound [Li] WHXSMMKQMYFTQS-UHFFFAOYSA-N 0.000 claims description 4
- 229910052744 lithium Inorganic materials 0.000 claims description 4
- 230000000694 effects Effects 0.000 claims description 3
- 241000271460 Crotalus cerastes Species 0.000 description 11
- 230000003028 elevating Effects 0.000 description 6
- 239000003381 stabilizer Substances 0.000 description 3
- 238000005096 rolling process Methods 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 1
Abstract
The leading edge of a wing is equipped with the aircraft that wind ball drives wind wheel, belongs to aviation aircraft technical field.Comprise fuselage, engine installation, left wing, right flank, empennage and alighting gear.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, left wind wheel, Zuo Fengqiu, left fixed-wing and port aileron.Right flank comprises right electrical motor, right clutch, right flank axle, right wind wheel, right wind ball, right fixed-wing and starboard aileron.Zuo Fengqiu and right wind ball rotate under the driving of front incoming flow or left electrical motor and right electrical motor, and front incoming flow major part is promoted to the upper surface of left wing and right flank and stream after accelerating, and the lift that left wing and right flank produce increases greatly.This invention aircraft can short take-off and landing (STOL), and flight maneuver is flexible.
Description
Technical field
The leading edge of a wing is equipped with the aircraft that wind ball drives wind wheel, belongs to aviation aircraft technical field, particularly relates to a kind of wind wheel aeroplane.
Background technology
Traditional aircraft wing is fixing, regulates the size of lift by wing flap, 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, invent a kind of can short take-off and landing, flight maneuver flexibly the leading edge of a wing wind ball be housed drive the aircraft of wind wheel.
The leading edge of a wing is equipped with the aircraft that wind ball drives wind wheel, 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, left wind wheel, Zuo Fengqiu, left fixed-wing and port aileron.Right flank comprises right electrical motor, right clutch, right flank axle, right wind wheel, right wind ball, right fixed-wing and starboard aileron.Left electrical motor is identical with parameter with right electric motor structure.Zuo Fengqiu is identical with right wind spherical structure and be arranged symmetrically with.The left end of left wing's axle is connected with Zuo Fengqiu through after the bearing be arranged on the wing tip end plate of left fixed-wing, the right-hand member of left wing's axle is connected with the output shaft of left clutch through after the bearing be installed on the left wall of fuselage, and the input shaft of left clutch is connected with the output shaft of left electrical motor.The right-hand member of right flank axle is connected with right wind ball through after the bearing be arranged on the wing tip end plate of right fixed-wing, the left end of right flank axle is connected with the output shaft of right clutch through after the bearing be installed on the right wall of fuselage, and the input shaft of right clutch is connected with the output shaft of right electrical motor.Left wind wheel is identical with right wind wheel structure, and the cross section of their blade is aerofoil profile.Left electrical motor, left clutch, right electrical motor and right clutch are arranged in fuselage.Drive the aircraft of wind wheel to move ahead along with this leading edge of a wing is equipped with wind ball, 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.Left wind spherical zone moves left wind wheel clockwise direction and rotates; Right wind spherical zone moves right wind wheel and also does clockwise direction rotation.Front incoming flow major part is promoted to the upper surface of left wing and right flank and flows after accelerating by left wind wheel and right wind wheel, and the lift making left wing and right flank produce like this increases greatly.The power of electrical motor and right electrical motor of keeping left during landing drives left wind wheel and right wind wheel clickwise, thus increases lift.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.
A kind of leading edge of a wing of the present invention is equipped with wind ball and drives the left wing of aircraft of wind wheel and the mode of operation of right flank to comprise: mainly keep left when this is taken off and lands electrical motor and right electrical motor drive left wind wheel and right wind wheel to rotate respectively; When cruising, main incoming flow on the front blows Zuo Fengqiu and right wind ball and rotates and drive left wind wheel and right wind wheel to rotate respectively.The velocity of rotation that namely the horizontal rolling in left and right of this aircraft sidewinders mainly by controlling left electrical motor and the left wind wheel of right direct motor drive and right wind wheel realizes, 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.
Port aileron and starboard aileron are used to control aircraft and sidewinder.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 that a kind of leading edge of a wing of the present invention is equipped with that wind ball drives the aircraft of wind wheel; Fig. 2 is the cross sectional drawing of the right flank be exaggerated.
In figure, 1-fuselage; 2-chest expander; 3-left wing, the left electrical motor of 31-, 32-left clutch, 33-left wing axle, the left wind wheel of 34-, the left wind ball of 35-, the left fixed-wing of 36-, the wing tip end plate of the left fixed-wing of 37-, 38-port aileron; 4-right flank, the right electrical motor of 41-, 42-right clutch, 43-right flank axle, the right wind wheel of 44-, the right wind ball of 45-, the right fixed-wing of 46-, the wing tip end plate of the right fixed-wing of 47-, 48-starboard aileron; 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 by reference to the accompanying drawings the present invention is illustrated: a kind of leading edge of a wing is equipped with the aircraft that wind ball drives wind wheel, 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, left wind wheel 34, left wind ball 35, left fixed-wing 36 and port aileron 38.Right flank 4 comprises right electrical motor 41, right clutch 42, right flank axle 43, right wind wheel 44, right wind ball 45, right fixed-wing 46 and starboard aileron 48.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, the left end of left wing's axle 33 is connected with left wind ball 35 through after the bearing be arranged on the wing tip end plate 37 of left fixed-wing, the right-hand member of left wing's axle 33 is connected with the output shaft of left clutch 32 through after the bearing be installed on the left wall of fuselage 1, and the input shaft of left clutch 32 is connected with the output shaft of left electrical motor 31.The right-hand member of right flank axle 43 is connected with right wind ball 45 through after the bearing be arranged on the wing tip end plate 47 of right fixed-wing, the left end of right flank axle 43 is connected with the output shaft of right clutch 42 through after the bearing be installed on the right wall of fuselage 1, and the input shaft of right clutch 42 is connected with the output shaft of right electrical motor 41.Left wind wheel 34 is identical with right wind wheel 44 structure, and the cross section of their blade is aerofoil profile.Left electrical motor 31, left clutch 32, right electrical motor 41 and right clutch 42 are arranged in fuselage 1.The aircraft of wind wheel is driven to move ahead along with this leading edge of a wing is equipped with wind ball, 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 left wind wheel 34 clockwise direction to rotate; Right wind ball 45 drives right wind wheel 44 also to do clockwise direction rotation.Front incoming flow major part is promoted to the upper surface of left wing 3 and right flank 4 and flows after accelerating by left wind wheel 34 and right wind wheel 44, and the lift making left wing 3 and right flank 4 produce like this increases greatly.The power of electrical motor 31 and right electrical motor 41 of keeping left during landing drives left wind wheel 34 and right wind wheel 44 clickwise, in order to increase lift.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.
A kind of leading edge of a wing of the present invention is equipped with wind ball and drives the left wing 3 of aircraft of wind wheel and the mode of operation of right flank 4 to comprise: mainly keep left when this is taken off and lands electrical motor 31 and right electrical motor 41 drive left wind wheel 34 and right wind wheel 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 left wind wheel 34 and right wind wheel 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 left wind wheel 34 and right wind wheel 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.
Port aileron 38 and starboard aileron 48 are used to control aircraft and sidewinder.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 (6)
1. the leading edge of a wing is equipped with the aircraft that wind ball drives wind wheel, and comprise fuselage (1), engine installation, left wing (3), right flank (4), empennage and alighting gear (7), fuselage is furnished with maneuvering system and airborne equipment in (1); Engine installation comprises energy supplyystem and propelling unit or chest expander, it is characterized in that: 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), left wind wheel (34), Zuo Fengqiu (35), left fixed-wing (36) and port aileron (38); Right flank (4) comprises right electrical motor (41), right clutch (42), right flank axle (43), right wind wheel (44), right wind ball (45), right fixed-wing (46) and starboard aileron (48); 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 turn right from the left side of fuselage (1), they rotate clockwise under the effect of front incoming flow; The left end of left wing's axle (33) is connected with left wind ball (35) through after the bearing be arranged on the wing tip end plate (37) of left fixed-wing, the right-hand member of left wing's axle (33) is connected with the output shaft of left clutch (32) through after the bearing be installed on fuselage (1) left wall, and the input shaft of left clutch (32) is connected with the output shaft of left electrical motor (31); The right-hand member of right flank axle (43) is connected with right wind ball (45) through after the bearing be arranged on the wing tip end plate (47) of right fixed-wing, the left end of right flank axle (43) is connected with the output shaft of right clutch (42) through after the bearing be installed on fuselage (1) right wall, and the input shaft of right clutch (42) is connected with the output shaft of right electrical motor (41); Left wind wheel (34) is identical with right wind wheel (44) structure; Left electrical motor (31), left clutch (32), right electrical motor (41) and right clutch (42) are arranged in fuselage (1); Left clutch (32) is identical with right clutch (42) structure, and they are free-wheel clutch.
2. a kind of leading edge of a wing according to claim 1 is equipped with the aircraft that wind ball drives wind wheel, it is characterized in that: bikini wheel undercarriage after alighting gear (7) adopts.
3. a kind of leading edge of a wing according to claim 1 is equipped with the aircraft that wind ball drives wind wheel, it 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 leading edge of a wing according to claim 1 is equipped with the aircraft that wind ball drives wind wheel, it 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 leading edge of a wing according to claim 1 is equipped with the aircraft that wind ball drives wind wheel, it is characterized in that: left electrical motor (31) and right electrical motor (41) adopt the lithium battery power supply of convenient charging.
6. a kind of leading edge of a wing according to claim 1 is equipped with the aircraft that wind ball drives wind wheel, it is characterized in that: the cross section of the blade of left wind wheel (34) and right wind wheel (44) is aerofoil profile.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520294192.1U CN204642148U (en) | 2015-05-08 | 2015-05-08 | A kind of leading edge of a wing is equipped with the aircraft that wind ball drives wind wheel |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520294192.1U CN204642148U (en) | 2015-05-08 | 2015-05-08 | A kind of leading edge of a wing is equipped with the aircraft that wind ball drives wind wheel |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204642148U true CN204642148U (en) | 2015-09-16 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520294192.1U Withdrawn - After Issue CN204642148U (en) | 2015-05-08 | 2015-05-08 | A kind of leading edge of a wing is equipped with the aircraft that wind ball drives wind wheel |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204642148U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108082466A (en) * | 2017-11-23 | 2018-05-29 | 北京航空航天大学 | A kind of tilting duct connection wing layout vertically taking off and landing flyer |
| CN104773282B (en) * | 2015-05-08 | 2018-07-13 | 湖南湘晨飞机工业有限公司 | A kind of aircraft of the leading edge of a wing equipped with wind ball driving wind wheel |
-
2015
- 2015-05-08 CN CN201520294192.1U patent/CN204642148U/en not_active Withdrawn - After Issue
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104773282B (en) * | 2015-05-08 | 2018-07-13 | 湖南湘晨飞机工业有限公司 | A kind of aircraft of the leading edge of a wing equipped with wind ball driving wind wheel |
| CN108082466A (en) * | 2017-11-23 | 2018-05-29 | 北京航空航天大学 | A kind of tilting duct connection wing layout vertically taking off and landing flyer |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| AV01 | Patent right actively abandoned |
Granted publication date: 20150916 Effective date of abandoning: 20180713 |
|
| AV01 | Patent right actively abandoned |