CN206424569U - A kind of adjustable canard of model plane - Google Patents
A kind of adjustable canard of model plane Download PDFInfo
- Publication number
- CN206424569U CN206424569U CN201621463435.0U CN201621463435U CN206424569U CN 206424569 U CN206424569 U CN 206424569U CN 201621463435 U CN201621463435 U CN 201621463435U CN 206424569 U CN206424569 U CN 206424569U
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- China
- Prior art keywords
- canard
- model
- rotating shaft
- adjustable
- model plane
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Abstract
The utility model discloses a kind of adjustable canard of model plane, including canard main body, it is characterized in that, rotating shaft is fixed with described canard main body, rotating shaft passes through body by bearing arrangement in frame, it is set with rotating shaft in driven gear, frame and is provided with motor, the driving gear engaged with driven gear is provided with motor.The adjustable canard of model plane described in the utility model is simple in construction, and easy to implement, cost is low, and Reliability of Microprocessor is good, can dynamically adjust the canard angle of pitch to simulate the various state of flights of aircraft, practicality and teaching are good.
Description
Technical field
The utility model is related to model plane technical field, more particularly to a kind of model plane adjustable canard.
Background technology
Model from structural form for have dynamic and static two kinds, static model is exactly no power set, is moved
States model, which is primarily referred to as model, has controllability, not only there is mechanical actuation device, and the function of also having electronic telecontrol having,
So with stronger enjoying nature and teaching.Traditional large-scale model plane are usually static, simply simply imitate type, it is impossible to drill
Show action, it is impossible to which the motion principle and rule of internal structure, object from the original is shown.The canard of aircraft except with
It is outer to produce vortex, also by adjusting the problem of angle of pitch improves stability rapid drawdown during transonic speed, match somebody with somebody while can also reduce
Flat resistance, be conducive to supersonic speed air battle, during landing, also deflectable one of canard very big negative angle plays flap, tradition
The canard of model plane is all static fixed component, it is impossible to show the working condition of canard, practicality and teaching are poor.
Utility model content
Technical problem to be solved in the utility model and propose technical assignment be prior art is improved there is provided
A kind of adjustable canard of model plane, the adjustable canard for solving model plane traditional in current technology is static fixed component, teaching compared with
Poor the problem of.
To solve above technical problem, the technical solution of the utility model is：
A kind of adjustable canard of model plane, including canard main body, it is characterised in that be fixed with and turn in described canard main body
Axle, rotating shaft passes through body in frame, to be set with rotating shaft in driven gear, frame by bearing arrangement and be provided with motor, electricity
The driving gear engaged with driven gear is provided with machine.The adjustable canard of model plane described in the utility model is driven by motor
Canard main body is together rotated with rotating shaft, realizes the angle of pitch regulation of canard main body, simple in construction, easy to implement, cost is low, moves
Make reliability high, service life is long, dynamic displaying canard working condition can be explained more accurately to audience, real
It is good with property and teaching.
Further, the diameter of described driven gear is more than driving gear, and playing is more than the output torque of driven pulley
The effect of motor, it is to avoid canard body rotation is too fast, ensures the work of the long-acting stabilization of canard main body.
Further, described canard main body is formed by the riveting of sheet metal part, and lightweight, intensity is high, low manufacture cost.
Further, it is provided with described rotating shaft in the alignment pin perpendicular to rotating shaft axial direction, frame and is provided with limited block,
Limited block is located in the circumferential paths that alignment pin rotates, and the maximum rotational angle of canard main body is limited with limited block, it is to avoid duck
There is the impaired working condition for not meeting real aircraft either in wing main body inordinate rotation.
Further, described limited block is block rubber, and reduction alignment pin touches noise during limited block, reduced simultaneously
Abrasion, increases the service life.
Compared with prior art, the utility model advantage is：
The adjustable canard of model plane described in the utility model is simple in construction, and easy to implement, cost is low, and Reliability of Microprocessor is good,
The canard angle of pitch can dynamically be adjusted to simulate the various state of flights of aircraft, practicality and teaching are good.
Brief description of the drawings
Fig. 1 is structural representation of the present utility model；
Fig. 2 is the structural representation of rotating shaft cross-wise direction.
Embodiment
Below in conjunction with the accompanying drawing in the utility model embodiment, the technical scheme in the utility model embodiment is carried out
Clearly and completely describe, it is clear that described embodiment is only a part of embodiment of the utility model, rather than whole
Embodiment.Based on the embodiment in the utility model, those of ordinary skill in the art are not under the premise of creative work is made
The every other embodiment obtained, belongs to the scope of the utility model protection.
A kind of adjustable canard of model plane disclosed in the utility model embodiment, can dynamically show the working condition of canard,
Bandwagon effect is good, simple and stable structure, and it is convenient to realize, practicality and teaching are good.
As depicted in figs. 1 and 2, a kind of adjustable canard of model plane, including canard main body 1, canard main body 1 is by sheet metal part
Riveting is formed, and rotating shaft 2 is fixed with wing main body 1, and rotating shaft 2 passes through body by bearing arrangement in frame 3, is set with rotating shaft 2
Have and device driving gear 6, the diameter of driven gear 4 are provided with motor 5, the output shaft of motor 5 in driven gear 4, frame 3
More than driving gear 6, driving gear 6 and the engaged transmission of driven gear 4 play a part of deceleration so that canard main body 1 can be with
Relatively slow speed rotation.
It is provided with rotating shaft 2 in the alignment pin 7 perpendicular to the axial direction of rotating shaft 2, frame 3 and is provided with limited block 8, limited block 8
In in the circumferential paths that alignment pin 7 rotates, limited block 8 is block rubber, and limited block 8 is provided with two, and one is located at canard
On the position of the maximum elevation of main body 1, another is located on the position of the maximum depression of canard main body 1, effectively limits canard main body 1
The anglec of rotation, it is to avoid the excessively rotation of canard main body 1 does not meet the working condition of actual airplane, it is ensured that the reliability of canard action.
It the above is only preferred embodiment of the present utility model, it is noted that above-mentioned preferred embodiment should not be regarded
For to limitation of the present utility model, protection domain of the present utility model should be defined by claim limited range.For
For those skilled in the art, do not departing from spirit and scope of the present utility model, can also make some
Improvements and modifications, these improvements and modifications also should be regarded as protection domain of the present utility model.
Claims (5)
1. a kind of adjustable canard of model plane, including canard main body (1), it is characterised in that be fixed with described canard main body (1)
Rotating shaft (2), rotating shaft (2) passes through body that in frame (3), driven gear (4), machine are set with rotating shaft (2) by bearing arrangement
The driving gear (6) for being provided with and being engaged with driven gear (4) on motor (5), motor (5) is provided with frame (3).
2. the adjustable canard of model plane according to claim 1, it is characterised in that the diameter of described driven gear (4) is big
In driving gear (6).
3. the adjustable canard of model plane according to claim 1, it is characterised in that described canard main body (1) is by metal metal plate
Golden part riveting is formed.
4. the adjustable canard of model plane according to claim 1, it is characterised in that be provided with described rotating shaft (2) vertical
Limited block (8) is provided with alignment pin (7) in rotating shaft (2) axial direction, frame (3), limited block (8) rotates positioned at alignment pin (7)
Circumferential paths on.
5. the adjustable canard of model plane according to claim 4, it is characterised in that described limited block (8) is block rubber.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621463435.0U CN206424569U (en) | 2016-12-29 | 2016-12-29 | A kind of adjustable canard of model plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621463435.0U CN206424569U (en) | 2016-12-29 | 2016-12-29 | A kind of adjustable canard of model plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206424569U true CN206424569U (en) | 2017-08-22 |
Family
ID=59584440
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621463435.0U Expired - Fee Related CN206424569U (en) | 2016-12-29 | 2016-12-29 | A kind of adjustable canard of model plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206424569U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108257455A (en) * | 2018-03-13 | 2018-07-06 | 桐乡市乌镇鼎丰旅游咨询工作室 | A kind of education and instruction stent |
| CN110090457A (en) * | 2019-05-30 | 2019-08-06 | 成都航空职业技术学院 | A kind of Three-wing-surface adjustable hand throwing aircraft |
| CN114261515A (en) * | 2022-01-18 | 2022-04-01 | 山西汾西重工有限责任公司 | Duck wing locking device and glider |
-
2016
- 2016-12-29 CN CN201621463435.0U patent/CN206424569U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108257455A (en) * | 2018-03-13 | 2018-07-06 | 桐乡市乌镇鼎丰旅游咨询工作室 | A kind of education and instruction stent |
| CN110090457A (en) * | 2019-05-30 | 2019-08-06 | 成都航空职业技术学院 | A kind of Three-wing-surface adjustable hand throwing aircraft |
| CN114261515A (en) * | 2022-01-18 | 2022-04-01 | 山西汾西重工有限责任公司 | Duck wing locking device and glider |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| 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: 20170822 Termination date: 20201229 |