CN207417124U - A kind of electronic vertical fin for folding wings unmanned plane - Google Patents
A kind of electronic vertical fin for folding wings unmanned plane Download PDFInfo
- Publication number
- CN207417124U CN207417124U CN201721543808.XU CN201721543808U CN207417124U CN 207417124 U CN207417124 U CN 207417124U CN 201721543808 U CN201721543808 U CN 201721543808U CN 207417124 U CN207417124 U CN 207417124U
- Authority
- CN
- China
- Prior art keywords
- rocking arm
- vertical fin
- steering engine
- fixed frame
- connecting rod
- 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.)
- Active
Links
Landscapes
- Toys (AREA)
Abstract
The utility model discloses a kind of electronic vertical fins for folding wings unmanned plane, a kind of electronic vertical fin for folding wings unmanned plane, including fixed frame, the front of the fixed frame is equipped with steering engine, and the steering engine is connected by rivet with fixed frame, and the front of the steering engine is equipped with rocking arm, the top of the rocking arm is equipped with connecting rod, the connecting rod is connected by screw with rocking arm, and the front of the connecting rod is equipped with rocking arm, and the upper and lower ends of the rocking arm are equipped with card slot.This is used for the electronic vertical fin of folding wings unmanned plane, pass through the cooperation of steering engine and rocking arm, steering engine drives rocking arm to provide ability source for device, and by the cooperation of block and anti-rotating hole, vertical fin is fixed in shaft, prevent vertical fin from surrounding bar rotation, also make the effect that shaft drives vertical fin to rotate more preferable, by the cooperation of fixed frame and rivet, steering engine is fixed on fixed frame by rivet, steering engine is made more to stablize at work, aerofoil is realized and is smoothly unfolded and can control.
Description
Technical field
The utility model is related to unmanned air vehicle technique fields, are specially a kind of electronic vertical fin for folding wings unmanned plane.
Background technology
Folding wings unmanned plane main advantage is small, saving space, easy to carry and transport, the mesh of the utility model
Be to provide a kind of small, Automatic-expanding and the mechanism of vertical fin can be folded.
Utility model content
The purpose of this utility model is to provide a kind of electronic vertical fin for folding wings unmanned plane, to solve above-mentioned background
The problem of being proposed in technology.
To achieve the above object, the utility model provides following technical solution：It is a kind of to be used for the electronic of folding wings unmanned plane
Vertical fin, including fixed frame, the front of the fixed frame is equipped with steering engine, and the steering engine is connected by rivet with fixed frame, the rudder
The front of machine is equipped with rocking arm, and the top of the rocking arm is equipped with connecting rod, and the connecting rod is connected by screw with rocking arm, the company
The front of bar is equipped with rocking arm, and the upper and lower ends of the rocking arm are equipped with card slot, and the rocking arm is connected by shaft with connecting rod, institute
The front for stating shaft is equipped with vertical fin, and anti-rotating hole is equipped on the left of the bottom of the vertical fin, and the front of the vertical fin is equipped with block, institute
Shaft is stated through anti-rotating hole with block to be connected.
Compared with prior art, the beneficial effects of the utility model are：This is used for the electronic vertical fin of folding wings unmanned plane, leads to
The cooperation of steering engine and rocking arm is crossed, steering engine drives rocking arm to provide ability source for device, by the cooperation of block and anti-rotating hole, will hang down
Tail is fixed in shaft, prevents vertical fin from, around bar rotation, also making the effect that shaft drives vertical fin to rotate more preferable, passing through fixed frame
With the cooperation of rivet, steering engine is fixed on fixed frame by rivet, and steering engine is made more to stablize at work, it is stable to realize aerofoil
It is unfolded and can controls, it is easy to operate.
Description of the drawings
Fig. 1 is the utility model structure diagram；
Fig. 2 is the vertical fin structure diagram of the utility model；
Fig. 3 is the utility model structure left hand view；
Fig. 4 is the rocker structure schematic diagram of the utility model；
Fig. 5 is the anti-rotating hole structure diagram of the utility model.
In figure：1st, fixed frame, 2, steering engine, 3, rocking arm, 4, connecting rod, 5, screw, 6, vertical fin, 7, shaft, 8, rocking arm, 9, gear
Block, 10, rivet, 11, card slot, 12, anti-rotating hole.
Specific embodiment
The following is a combination of the drawings in the embodiments of the present utility model, and the technical scheme in the embodiment of the utility model is carried out
It clearly and completely describes, it is clear that the described embodiments are only a part of the embodiments of the utility model rather than whole
Embodiment.Based on the embodiment in the utility model, those of ordinary skill in the art are without making creative work
All other embodiments obtained shall fall within the protection scope of the present invention.
- 5 are please referred to Fig.1, the utility model provides a kind of technical solution：It is a kind of to hang down for the electronic of folding wings unmanned plane
Tail, including fixed frame 1, the front of fixed frame 1 is equipped with steering engine 2, and steering engine 2, pressurized strut, compressed gas can be used in this mechanism rotation process
Body etc. is used as power source, and easy to operate, highly practical, steering engine 2 is connected by rivet 10 with fixed frame 1, the front installation of steering engine 2
There is rocking arm 3, the top of rocking arm 3 is equipped with connecting rod 4, and connecting rod 4 is connected by screw 5 with rocking arm 3, when aerofoil needs expansion, connects
The external power supply of logical steering engine 2, steering engine 2 are started to work, and steering engine 2 drives connecting rod 4,4 drive shaft 7 of connecting rod and band by rocking arm 3
Shake arm 8 to rotate, rocking arm 8 is fixedly connected by screw 5 with shaft 7, and shaft 7 is connected through anti-rotating hole 12 with vertical fin 6, in shaft
7 drive vertical fin 6 to be steadily unfolded while rotation, and the front of connecting rod 4 is equipped with rocking arm 8, and the upper and lower ends of rocking arm 8 are equipped with card slot
11, make easier for installation, rocking arm 8 is connected by shaft 7 with connecting rod 4, and the front of shaft 7 is equipped with vertical fin 6, the bottom of vertical fin 6
End left side is equipped with anti-rotating hole 12, and the front of vertical fin 6 is equipped with block 9, and shaft 7 is connected through anti-rotating hole 12 with block 9, anti-rotating hole 12
Effect be the fixed effect increased between vertical fin 6 and shaft 7, enable shaft 7 that vertical fin 6 to be driven to rotate together.
When aerofoil needs expansion, the external power supply of steering engine 2 is connected, steering engine 2 is started to work, and steering engine 2 is driven by rocking arm 3
Connecting rod 4,4 drive shaft 7 of connecting rod and drives rocking arm 8 to rotate, and rocking arm 8 is fixedly connected by screw 5 with shaft 7, and shaft 7 passes through
Anti-rotating hole 12 is connected with vertical fin 6, while shaft 7 rotates vertical fin 6 is driven steadily to be unfolded.
In the description of the utility model, it is to be understood that term " coaxial ", " bottom ", " one end ", " top ", " in
Portion ", " other end ", " on ", " one side ", " top ", " interior ", " forepart ", " center ", the orientation of the instructions such as " both ends " or position close
Be for based on orientation shown in the drawings or position relationship, be for only for ease of description the utility model and simplify description rather than
Indicate or imply that signified device or element there must be specific orientation, with specific azimuth configuration and operation, therefore cannot
It is interpreted as the limitation to the utility model.
In the utility model, unless otherwise clearly defined and limited, term " installation ", " setting ", " connection ", " Gu
It is fixed ", the terms such as " being screwed on " should be interpreted broadly, for example, it may be being fixedly connected or being detachably connected or integral；
Can be mechanical connection or electrical connection；It can be directly connected, can also be indirectly connected by intermediary, it can be with
It is the interaction relationship of connection inside two elements or two elements, unless otherwise restricted clearly, for this field
For those of ordinary skill, concrete meaning of the above-mentioned term in the utility model can be understood as the case may be.
While there has been shown and described that the embodiment of the utility model, for the ordinary skill in the art,
It is appreciated that in the case where not departing from the principle of the utility model and spirit can these embodiments be carried out with a variety of variations, repaiied
Change, replace and modification, the scope of the utility model are defined by the appended claims and the equivalents thereof.
Claims (1)
1. a kind of electronic vertical fin for folding wings unmanned plane, including fixed frame (1), it is characterised in that：The fixed frame (1)
Front is equipped with steering engine (2), and the steering engine (2) is connected by rivet (10) with fixed frame (1), the front installation of the steering engine (2)
There is rocking arm (3), the top of the rocking arm (3) is equipped with connecting rod (4), and the connecting rod (4) is connected by screw (5) with rocking arm (3),
The front of the connecting rod (4) is equipped with rocking arm (8), and the upper and lower ends of the rocking arm (8) are equipped with card slot (11), the rocking arm
(8) it is connected by shaft (7) with connecting rod (4), the front of the shaft (7) is equipped with vertical fin (6), the bottom of the vertical fin (6)
Left side is equipped with anti-rotating hole (12), and the front of the vertical fin (6) is equipped with block (9), and the shaft (7) is through anti-rotating hole (12) and gear
Block (9) is connected.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721543808.XU CN207417124U (en) | 2017-11-17 | 2017-11-17 | A kind of electronic vertical fin for folding wings unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721543808.XU CN207417124U (en) | 2017-11-17 | 2017-11-17 | A kind of electronic vertical fin for folding wings unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207417124U true CN207417124U (en) | 2018-05-29 |
Family
ID=62302662
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721543808.XU Active CN207417124U (en) | 2017-11-17 | 2017-11-17 | A kind of electronic vertical fin for folding wings unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207417124U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112572768A (en) * | 2020-12-18 | 2021-03-30 | 中国电子科技集团公司第三十八研究所 | Control mechanism of full-motion vertical fin of unmanned aerial vehicle |
| CN113830279A (en) * | 2021-11-09 | 2021-12-24 | 中国电子科技集团公司第三十八研究所 | Propeller electric propulsion device for adjusting posture of airship |
| CN117775339A (en) * | 2024-02-28 | 2024-03-29 | 成都金支点科技有限公司 | Servo control mechanism and unmanned aerial vehicle of collapsible rudder |
-
2017
- 2017-11-17 CN CN201721543808.XU patent/CN207417124U/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112572768A (en) * | 2020-12-18 | 2021-03-30 | 中国电子科技集团公司第三十八研究所 | Control mechanism of full-motion vertical fin of unmanned aerial vehicle |
| CN113830279A (en) * | 2021-11-09 | 2021-12-24 | 中国电子科技集团公司第三十八研究所 | Propeller electric propulsion device for adjusting posture of airship |
| CN117775339A (en) * | 2024-02-28 | 2024-03-29 | 成都金支点科技有限公司 | Servo control mechanism and unmanned aerial vehicle of collapsible rudder |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN207417124U (en) | A kind of electronic vertical fin for folding wings unmanned plane | |
| JP3141209U (en) | Helicopter model | |
| CN105151278B (en) | A kind of rudder face differential driving mechanism suitable for unmanned plane | |
| CN110065630B (en) | Bionic flapping wing flying robot | |
| CN107108012A (en) | The horn and unmanned vehicle of connection component, unmanned vehicle | |
| CN104791275B (en) | For the oscillating mechanism of electric fan and the electric fan with it | |
| CN205859553U (en) | A kind of hand-held regulator of multifunctional split-type electronic gyroscope | |
| CN107161339A (en) | One kind is fluttered the bionical bird of twisted coupling | |
| CN207417122U (en) | A kind of Double-spring unmanned plane wing-folding unfolding mechanism | |
| CN206606158U (en) | A kind of full passive blade formula variable air inlet grid | |
| CN207417115U (en) | A kind of wheeled unmanned plane wing electric foldable unfolding mechanism of bidentate | |
| CN205113712U (en) | Two degree of freedom flapping wing aircraft | |
| CN207417121U (en) | A kind of compressed spring type unmanned plane wing-folding unfolding mechanism | |
| CN204297076U (en) | A kind of six axle aircraft | |
| CN204783766U (en) | Automatic electric fan of shaking head from top to bottom | |
| CN204982303U (en) | Sewing machine's differential adjustment mechanism that compares | |
| CN208111420U (en) | QFP device encapsulation structure | |
| CN207417123U (en) | A kind of electronic front wing for folding wings unmanned plane | |
| CN205047476U (en) | Fan oscillating mechanism and complex of using it electric fan of shaking head | |
| CN109351612A (en) | A kind of screen stencil sheet being easy to change aperture | |
| CN209243333U (en) | A kind of sewing machine | |
| CN208190819U (en) | A kind of semiconductor manufacturing plant environmental monitoring system | |
| CN210240077U (en) | Knob stepless speed regulating fan | |
| CN209719896U (en) | A kind of aircraft | |
| CN207385839U (en) | Parallel operation is shaken in primary coat |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |