CN2902392Y - Front and back direction changing control component element of model airplane - Google Patents
Front and back direction changing control component element of model airplane Download PDFInfo
- Publication number
- CN2902392Y CN2902392Y CN 200620057830 CN200620057830U CN2902392Y CN 2902392 Y CN2902392 Y CN 2902392Y CN 200620057830 CN200620057830 CN 200620057830 CN 200620057830 U CN200620057830 U CN 200620057830U CN 2902392 Y CN2902392 Y CN 2902392Y
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- CN
- China
- Prior art keywords
- turning
- control component
- model
- turn
- connecting rod
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- Expired - Lifetime
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Abstract
The utility model provides a fore-and-aft steering control assembly for a model airplane and the utility model consists of a steering engine, a steering control unit and a connection rod. The steering engine is connected with the steering control unit by the connection rod. The fore-and-aft steering control assembly of the utility model is novel, simple in structure and easy to steer the model airplane. The fore-and-aft steering of the model airplane can be easily controlled and is very sensitive. The utility model can efficiently control the model airplane to move forward or backward.
Description
Technical field
The utility model relates to the model plane field, refers to that especially a kind of front and back of model plane turn to Control Component.
Background technology
Turn to control assembly various before and after the general aeromodelling airplane, particularly have the aeromodelling airplane of 3D function, front and back turn to the control and regulation structure complicated, and wayward when turning to before and after regulating the control aeromodelling airplane, front and back turn to insensitive.
Summary of the invention
Based on the deficiencies in the prior art, main purpose of the present utility model is to provide a kind of model plane front and back simple in structure, that front and back turn to sensitivity to turn to Control Component.
In order to achieve the above object, the utility model provides a kind of front and back of model plane to turn to Control Component, comprises steering wheel, turning control cell and connecting rod, and described steering wheel connects turning control cell with connecting rod.
Described turning control cell comprises turning-bar, pull bar and pitch, and described turning-bar connects pitch with pull bar.The pull bar lower end is fixed in described turning-bar front and back end.The front and back linking arm socket pull bar upper end of described pitch.Described turning-bar is fixed on the mainboard frame.
Described connecting rod comprises fork and connecting rod, and described fork two ends are socket steering wheel and connecting rod respectively.
Described connecting rod further comprises another fork, and described another fork two ends are socket turning-bar and connecting rod respectively.
Compared with prior art, turn to Control Component simple in structure before and after the utility model, turn to regulative mode simple, novel before and after the model plane.Be easy to control when turning to before and after the aeromodelling airplane, turn to sensitivity.Can effectively control aeromodelling airplane is reached advance, the purpose of turning backward.
For making the utility model easier to understand, the front and back of further setting forth a kind of model plane of the utility model below in conjunction with accompanying drawing turn to the specific embodiment of Control Component.
Description of drawings
Fig. 1 is for turning to the structural representation of Control Component before and after the utility model model plane.
Fig. 2 is for turning to the decomposition texture schematic diagram of Control Component before and after the utility model model plane.
The specific embodiment
Below in conjunction with accompanying drawing, the utility model is further described.
Turn to Control Component to be installed in the fuselage main body of model plane before and after the utility model, the front and back that constitute model plane turn to regulating part.It comprises steering wheel 1, turning control cell 2 and connecting rod 3, and described steering wheel 1 connects turning control cell 2 with connecting rod 3.Drive the work of turning control cell 2 by steering wheel 1.
Turning control cell 2 comprises turning-bar 21, pull bar 22,23 and pitch 24, and described turning-bar 21 connects pitch 24 with pull bar 22,23.Turning-bar 21 middle parts are run through with main shaft 4, and it is fixed in fuselage mainboard frame upper end.Pull bar 22,23 lower ends are fixed in pin 25,26 respectively in turning-bar 21 front and back ends, and the front and back linking arm of pitch 24 is socket pull bar 22,23 upper ends respectively.
Connecting rod 3 comprises fork 31, fork 32 and connecting rod 33, fork 31 1 ends are fixed on the steering wheel 1 with screw 34, the other end is with the fixing aluminium ball 36 of screw 35, connect connecting rod 33 by aluminium ball 36 again, connecting rod 33 other ends connect fork 32 with aluminium ball 37 and screw 38 equally, fork 32 other ends are fixed in turning-bar 21 middle parts expenditure part with screw 39, then steering wheel 1 and turning control cell 2 linked up, and by turning to before and after the steering wheel 1 drive turning control cell 2 control model plane.
Working method: during startup, driven by motor steering wheel 1 rotates, and then by fork 31, connecting rod 33 and 21 rotations of fork 32 drive turning-bars, turning-bar 21 rotates by pull bar 22,23 pulling pitches 24, drive with pitch 24 again and go up the screw angle and change, then can effectively control the purpose that aeromodelling airplane is reached advance, retreat.
Above disclosed only for turning to the preferred embodiment of Control Component behind the utility model model plane, can not limit the utility model interest field with this, therefore the equivalent variations of being done according to the utility model claim still belongs to the scope that the utility model is contained.
Claims (7)
1. the front and back of model plane turn to Control Component, it is characterized in that: comprise steering wheel, turning control cell and connecting rod, described steering wheel connects turning control cell with connecting rod.
2. the front and back of model plane as claimed in claim 1 turn to Control Component, it is characterized in that: described turning control cell comprises turning-bar, pull bar and pitch, and described turning-bar connects pitch with pull bar.
3. the front and back of model plane as claimed in claim 2 turn to Control Component, it is characterized in that: the pull bar lower end is fixed in described turning-bar front and back end.
4. the front and back of model plane as claimed in claim 2 turn to Control Component, it is characterized in that: the front and back linking arm socket pull bar upper end of described pitch.
5. the front and back of model plane as claimed in claim 2 turn to Control Component, it is characterized in that: described turning-bar is fixed on the mainboard frame.
6. the front and back of model plane as claimed in claim 1 turn to Control Component, it is characterized in that: described connecting rod comprises fork and connecting rod, and described fork two ends are socket steering wheel and connecting rod respectively.
7. the front and back of model plane as claimed in claim 6 turn to Control Component, it is characterized in that: described connecting rod further comprises another fork, and described another fork two ends are socket turning-bar and connecting rod respectively.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 200620057830 CN2902392Y (en) | 2006-04-17 | 2006-04-17 | Front and back direction changing control component element of model airplane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 200620057830 CN2902392Y (en) | 2006-04-17 | 2006-04-17 | Front and back direction changing control component element of model airplane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN2902392Y true CN2902392Y (en) | 2007-05-23 |
Family
ID=38077794
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 200620057830 Expired - Lifetime CN2902392Y (en) | 2006-04-17 | 2006-04-17 | Front and back direction changing control component element of model airplane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN2902392Y (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106693394A (en) * | 2015-11-15 | 2017-05-24 | 许美兰 | Model airplane azimuth control system |
| CN113101679A (en) * | 2021-04-17 | 2021-07-13 | 西北工业大学 | Three-load separating device of model rocket |
-
2006
- 2006-04-17 CN CN 200620057830 patent/CN2902392Y/en not_active Expired - Lifetime
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106693394A (en) * | 2015-11-15 | 2017-05-24 | 许美兰 | Model airplane azimuth control system |
| CN113101679A (en) * | 2021-04-17 | 2021-07-13 | 西北工业大学 | Three-load separating device of model rocket |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CX01 | Expiry of patent term |
Granted publication date: 20070523 |
|
| EXPY | Termination of patent right or utility model |