CN205971807U - Plunder wing angle adjusting device - Google Patents
Plunder wing angle adjusting device Download PDFInfo
- Publication number
- CN205971807U CN205971807U CN201620766008.3U CN201620766008U CN205971807U CN 205971807 U CN205971807 U CN 205971807U CN 201620766008 U CN201620766008 U CN 201620766008U CN 205971807 U CN205971807 U CN 205971807U
- Authority
- CN
- China
- Prior art keywords
- wing
- wing plate
- steering wheel
- bedplate
- seat board
- 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
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Abstract
The utility model discloses the institute is a plunder wing angle adjusting device, it has left wing's board, right wing plate, steering wheel and bedplate, left wing's board and right wing plate install to rotate upward at the bedplate symmetrically and move, the steering wheel is installed by the bedplate, left wing's board and right wing plate pass through zola's pole and the transmission is connected with the steering wheel rocking arm to right pull rod, the steering wheel is controlled by flight controller, the steering wheel is servo steering wheel, flight controller includes the remote controller, part such as remote control receiver and battery, the bedplate comprises last bedplate and lower bedplate, left wing's board and right wing plate pass through the rotation axis and install at last bedplate under and between the bedplate, the bedplate installation is fixed on the fuselage, the back and forth movement of zola's pole and right pull rod is the symmetry and removes, the push -and -pull pterygoid lamina is for the angle symmetry change of fuselage axis. The utility model discloses can conveniently adjust the angle that the wing and fuselage were plunderred to the aircraft at the flight in -process, satisfy people to flight weight and flying speed to and degree of having a smooth flight requirement.
Description
Technical field
This utility model is a kind of model plane accessory, and specifically one kind plunders wing angle regulator.
Background technology
The wing of fixed wing airplane is explored and is never stopped.Due to scientific and technical backward and theoretical knowledge restriction, flight
The research of device fails to obtain good development.In recent years, with the progress that science and technology is theoretical, wing angular transformation technology is being plunderred in the U.S.
Aspect obtains important breakthrough, holds a safe lead countries in the world already, becomes and successfully develops the country plunderring wing convertible aircraft in the world.Beautiful
The famous tiltrotor masterpiece of state has f14 fighter plane.
The technical elements of wing angular transformation are being plunderred in China, at present also in the primary stage of development.Due to starting late, core
Heart technology is not also grasped, and also needs to continue to grope and study for reference.In the face of core technology breaks through this difficult problem, we not only need inverse
To research and development, with greater need for innovation.
Content of the invention
The purpose of this utility model is exactly to propose one kind to plunder wing angle regulator, and this device can be square in flight course
Just adjust the angle that aircraft plunders the wing and fuselage, meet people to flying weight and flight speed demand, make flight more steady.
This utility model proposed this plunder wing angle regulator, it has left wing plate, right wing plate, steering wheel and seat board,
It is characterized in that left wing plate and right wing plate are symmetrically mounted at rotating on seat board, steering wheel is arranged on by seat board, left wing plate and right flank
Plate passes through left lever and right pull bar is connected transmission with steering wheel rocking arm, and steering wheel is controlled by flight controller.
Described steering wheel is Servo-controller.
Flight controller includes remote control, the part such as remote-control receiver and battery.
Described seat board is made up of upper base plate and lower seat board, left wing plate and right wing plate by rotary shaft be arranged on upper base plate and under
Between seat board, seat board is fixed on fuselage.
Left lever and right pull bar move back and forth as symmetrically moving, push-and-pull left wing plate and right wing plate are with respect in fuselage simultaneously
The angle symmetrical of axis changes.
Angle change scope between steering wheel push-and-pull left wing plate and right wing plate and fuselage axis be 30-120 degree, left wing plate and
It is the flat wing angle when right wing plate is vertical with fuselage axis, during less than 90 degree, when that is, left wing plate and right wing plate turn backwards, plunder the wing for little
Angle or claim swept-back wing, more than 90 degree, that is, left wing plate and right wing plate forward when be to plunder wing angle or buzzard-type wing greatly.
For sake of convenience, left wing plate and right wing plate are referred to as wing plate by this utility model.Pull bar is referred to as by left lever and right pull bar.
This utility model, as an integrated package of aeromodelling aerocraft, is capable of freely converting of wing angle, full
The different flight of foot needs.Be easy to during wing vertical take off, wing forward when be easy to low cruise or heavy－duty navigation, wing court
It is easy to high band cruise when afterwards.The change of wing angle is realized by remote control by manipulator completely, in allowed band, angle
Can also stepless changing.
Therefore, this utility model can easily adjust, in flight course, the angle that aircraft plunders the wing and fuselage, meets people
To flying weight and flight speed, and the requirement of degree of having a smooth flight.
Brief description
Fig. 1 is this utility model schematic perspective view.
Fig. 2 is this utility model and model plane fuselage assembled relation figure.
In Fig. 1-2, the label of each several part is as follows：
1- Servo-controller；The right pull bar of 2-；3- left lever；4- rotary shaft；5- seat board；6- wing plate.
Specific embodiment
As shown in Figure 1-2.Wing plate 6 includes left wing plate and right wing plate, with existing as the structure of mould wing and shape close,
Be installs the accessories such as the installing hole of left lever 3, right pull bar 2 and rotary shaft 4 and corresponding bearing more.
Seat board 5 includes upper base plate and lower seat board, can make antitrope, a pair of wing plate is arranged between seat board.Seat board is installed
It is fixed on model airplane machine.These are substantially identical with existing model plane, herein not multilist.
Servo-controller 1 is existing commercial goods, and its supporting with pull bar can be according to specifically needing to order to supplier.
NM assembly and label are as described above.
This wing angle regulator of plunderring of this utility model adopts lithium battery power supply, and Servo-controller converts electrical current into into moment of torsion
Output power.Take off and smoothly complete aerial mission for stabilizing it, taken off using the flat wing when taking off, aircraft is equipped with one piece simultaneously
Flight controller auxiliary operation.Using plunderring greatly wing angle when needing low cruise or during big load, speed can be reduced simultaneously
And raising stability, increase loading capacity.Need to plunder wing angle using little when improving speed, motility and operable can be improved
Property.
Claims (6)
1. one kind plunders wing angle regulator, and it has left wing plate, right wing plate, steering wheel and seat board it is characterised in that left wing plate and the right side
Wing plate is symmetrically mounted at and rotates on seat board, and steering wheel is arranged on by seat board, and left wing plate and right wing plate pass through left lever and right pull bar
It is connected transmission with steering wheel rocking arm, steering wheel is controlled by flight controller.
2. plunder wing angle regulator according to claim 1 it is characterised in that steering wheel is Servo-controller.
3. plunder wing angle regulator according to claim 1 it is characterised in that flight controller includes remote control, remote control connects
Receipts machine and battery.
4. plunder wing angle regulator according to claim 1 it is characterised in that seat board is made up of upper base plate and lower seat board, left
Wing plate and right wing plate are arranged between upper base plate and lower seat board by rotary shaft, and seat board is fixed on fuselage.
5. plunder wing angle regulator according to claim 1 it is characterised in that left lever and right pull bar move back and forth for
Symmetrically move, push-and-pull left wing plate and right wing plate change with respect to the angle symmetrical of fuselage axis.
6. plunder wing angle regulator according to claim 1 it is characterised in that steering wheel push-and-pull left wing plate and right wing plate and machine
Angle change scope between body axis is 30-120 degree.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620766008.3U CN205971807U (en) | 2016-07-21 | 2016-07-21 | Plunder wing angle adjusting device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620766008.3U CN205971807U (en) | 2016-07-21 | 2016-07-21 | Plunder wing angle adjusting device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205971807U true CN205971807U (en) | 2017-02-22 |
Family
ID=58024899
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620766008.3U Expired - Fee Related CN205971807U (en) | 2016-07-21 | 2016-07-21 | Plunder wing angle adjusting device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205971807U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107985550A (en) * | 2017-12-09 | 2018-05-04 | 佛山市神风航空科技有限公司 | One kind change wing |
| CN115743519A (en) * | 2022-10-07 | 2023-03-07 | 北京工业大学 | Variable-wing aircraft wing sweepback angle mechanism |
-
2016
- 2016-07-21 CN CN201620766008.3U patent/CN205971807U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107985550A (en) * | 2017-12-09 | 2018-05-04 | 佛山市神风航空科技有限公司 | One kind change wing |
| CN115743519A (en) * | 2022-10-07 | 2023-03-07 | 北京工业大学 | Variable-wing aircraft wing sweepback angle mechanism |
| CN115743519B (en) * | 2022-10-07 | 2024-08-20 | 北京工业大学 | Variable sweep angle mechanism for variable wing aircraft wing |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20170222 Termination date: 20180721 |