CN206273682U - Unmanned aerial vehicle angle adjustable stabilizing control system - Google Patents
Unmanned aerial vehicle angle adjustable stabilizing control system Download PDFInfo
- Publication number
- CN206273682U CN206273682U CN201621106644.XU CN201621106644U CN206273682U CN 206273682 U CN206273682 U CN 206273682U CN 201621106644 U CN201621106644 U CN 201621106644U CN 206273682 U CN206273682 U CN 206273682U
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- vertical bar
- swivel plate
- power mechanism
- motor
- control system
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Abstract
The utility model discloses a kind of unmanned aerial vehicle angle adjustable stabilizing control system, including unmanned plane main body, vertical bar, swivel plate, two filming apparatus, first revolving power mechanism and the second revolving power mechanism, unmanned plane main body includes center mainboard, center mainboard has the first through hole passed through for vertical bar, the second through hole passed through for vertical bar is offered on swivel plate, the two ends of swivel plate are pivotally connected with center mainboard respectively, vertical bar passes through first through hole and the second through hole and is pivotally connected with swivel plate, the rotation direction of swivel plate is mutually perpendicular to the rotation direction of vertical bar, first revolving power mechanism drives with vertical bar and is connected, second revolving power mechanism drives with swivel plate and is connected, two ends of two filming apparatus respectively with vertical bar are affixed.By this unmanned aerial vehicle angle adjustable stabilizing control system so that filming apparatus are more stablized during shooting, and the image or video of shooting become apparent from.
Description
Technical field
The utility model is related to unmanned plane, more particularly to unmanned aerial vehicle angle adjustable stabilizing control system.
Background technology
Unmanned plane is the not manned vehicle manipulated by radio robot or airborne computer stored program controlled,
Generally filming apparatus are arranged on unmanned plane personage and scenery are shot.
In the prior art, filming apparatus are affixed frames by a straight-bar directly with unmanned plane, are clapped in unmanned plane during flying
During taking the photograph, if unmanned plane is subject to external force to act on run-off the straight, filming apparatus can also incline with the inclination of unmanned plane
Tiltedly, filming apparatus are caused to be susceptible to rock in shooting process, unstable, the fogging image of shooting.
Utility model content
In order to overcome the deficiencies in the prior art, the purpose of this utility model is to provide unmanned aerial vehicle angle adjustable stabilization to control
System processed, filming apparatus are more stablized during shooting, and the image or video of shooting become apparent from.
The purpose of this utility model is realized using following technical scheme：
Unmanned aerial vehicle angle adjustable stabilizing control system, including unmanned plane main body, vertical bar, swivel plate, two filming apparatus,
First revolving power mechanism and the second revolving power mechanism, unmanned plane main body include center mainboard, and center mainboard has for vertical
The first through hole that bar is passed through, offers the second through hole passed through for vertical bar on swivel plate, the two ends of swivel plate respectively with center
Mainboard is pivotally connected, and vertical bar passes through first through hole and the second through hole and pivotally connects with swivel plate
Connect, the rotation direction of swivel plate is mutually perpendicular to the rotation direction of vertical bar, the first revolving power mechanism is installed on swivel plate simultaneously
Driven with vertical bar and be connected, the second revolving power mechanism is installed on center mainboard and is driven with swivel plate and is connected, two filming apparatus
Two ends respectively with vertical bar are affixed.
Preferably, swivel plate is arranged in first through hole, and the two ends of swivel plate are respectively with the inwall of first through hole can turn
Dynamic mode is connected.
Preferably, this unmanned aerial vehicle angle adjustable stabilizing control system also includes a quadra, and the quadra is installed
In the upper surface of center mainboard, swivel plate be arranged in quadra and swivel plate two ends respectively with the inwall of quadra
Pivotally connect.
Preferably, the shock absorbing apparatus for damping are provided between quadra and center mainboard.
Preferably, shock absorbing apparatus are spring or antivibration pad.
Preferably, the first revolving power mechanism and the second revolving power mechanism are respectively the first motor and the second motor, the
The output shaft of one motor is affixed with vertical bar, and the output shaft of the second motor is affixed with swivel plate.
Preferably, the 3rd revolving power mechanism is installed, the 3rd revolving power mechanism is the 3rd motor in vertical bar, the
Three motors have upper output shaft and lower output shaft, and being set with the vertical bar above the 3rd motor can the rotation of opposed vertical bar
The first main shaft, the upper end of the first main shaft with positioned at vertical bar upper end filming apparatus it is affixed, the lower end of the first main shaft and the 3rd
The upper output shaft of motor is affixed, be set with the vertical bar below the 3rd motor can opposed vertical bar rotate the second main shaft,
The lower end of the second main shaft is affixed with the filming apparatus for being located at vertical bar lower end, the lower output of the upper end of the second main shaft and the 3rd motor
Axle is affixed.
Compared to existing technology, the beneficial effects of the utility model are：It is hinged and rotates with swivel plate by vertical bar
Ban Yu centers mainboard is hinged, it is ensured that vertical bar will not be rocked with unmanned plane main body is rocked so that whole shooting process is more
Stabilization, the image of shooting becomes apparent from；In addition, when vertical bar is subject to external force to act on run-off the straight, by the first rotary power
Mechanism, the second revolving power mechanism correspond to order about vertical bar and swivel plate rotation respectively so that vertical bar returns back to original position, prevents
Vertical bar causes the image for shooting or video unintelligible because external force effect shifts.
Brief description of the drawings
Fig. 1 is the structural representation of the utility model unmanned aerial vehicle angle adjustable stabilizing control system；
Fig. 2 is the partial enlarged drawing of A in Fig. 1.
In figure：1st, unmanned plane main body；2nd, center mainboard；3rd, vertical bar；4th, swivel plate；5th, filming apparatus；6th, the first rotation
Actuating unit；7th, the second revolving power mechanism；8th, the second through hole；9th, quadra；10th, shock absorbing apparatus；11st, the 3rd rotary power
Mechanism.
Specific embodiment
Below, with reference to accompanying drawing and specific embodiment, the utility model is described further：
As depicted in figs. 1 and 2, unmanned aerial vehicle angle adjustable stabilizing control system, including unmanned plane main body 1, vertical bar 3,
Swivel plate 4, two filming apparatus 5, the first revolving power mechanism 6 and the second revolving power mechanism 7, unmanned plane main body 1 include center
Mainboard 2, center mainboard 2 has the first through hole (figure is not marked) passed through for vertical bar 3, is offered on swivel plate 4 for vertical bar 3
The second through hole 8 for passing through, the two ends of swivel plate 4 are pivotally connected with center mainboard 2 respectively, and vertical bar 3 is through the
One through hole and the second through hole 8 are simultaneously pivotally connected with swivel plate 4, the rotation direction of swivel plate 4 and turning for vertical bar 3
Dynamic direction is mutually perpendicular to, and the first revolving power mechanism 6 is installed on swivel plate 4 and is driven with vertical bar 3 and is connected, the second rotary power
Mechanism 7 is installed on center mainboard 2 and is driven with swivel plate 4 and is connected, and two ends of two filming apparatus 5 respectively with vertical bar 3 are affixed.
As depicted in figs. 1 and 2, unmanned plane revolves during flight shoots when unmanned plane main body 1 is subject to external force to act on edge
During 4 two ends line direction run-off the straight of flap, because vertical bar 3 is pivotally connected with swivel plate 4, swivel plate 4 exists
With center mainboard 2 it is inclined during, swivel plate 4 is relatively rotated with vertical bar 3, and vertical bar 3 remains perpendicular because of self gravitation
Directly, will not the run-off the straight with the inclination of center mainboard 2, it is ensured that the stability in shooting process of filming apparatus 5, when nobody
When machine receives external force effect along perpendicular to the direction run-off the straight of the two ends line of swivel plate 4, due to the two ends and center of swivel plate
Mainboard 2 is pivotally connected, and during inclined, swivel plate 4 is rotated against center mainboard 2 with center mainboard 2, rotation
Flap 4 will not the run-off the straight with the inclination of center mainboard 2 so that vertical bar 3 remains vertical, further ensures shooting
In stability, therefore by said structure, no matter how unmanned plane inclines, by the rotation relative with vertical bar 3 of swivel plate 4
Turn and swivel plate 4 is rotated against with center mainboard 2, may be such that vertical bar 3 can remain vertical state, shooting process is steady
It is fixed, will not shake, the image of shooting becomes apparent from；In addition, when vertical bar 3 is subject to external force effect to deviate vertical direction,
Signal is passed to the first revolving power mechanism 6 and the second revolving power mechanism 7 by the sensor in vertical bar 3 by mainboard, the
One revolving power mechanism 6 and the second revolving power mechanism 7 correspond to order about vertical bar 3 and swivel plate 4 rotates respectively so that vertical bar
3 return back to original position, prevent vertical bar 3 from causing the image for shooting or video unintelligible because external force effect shifts, above institute
The sensor and mainboard stated all are control devices commonly used in the prior art, at the same time it can also give perpendicular according to actually used situation
Straight-bar 3 sets movement track, and this action track passes to the first revolving power mechanism 6 and the second rotating power machine by the mainboard
Structure 7, the first revolving power mechanism 6 and the second revolving power mechanism 7 control vertical bar 3 and swivel plate 4 by the action of setting respectively
Track is moved, and more conforms to use requirement, and practicality is stronger.
A kind of preferred embodiment as the utility model, swivel plate 4 is arranged in first through hole, and the two of swivel plate 4
End is pivotally connected with the inwall of first through hole respectively.It is arranged in first through hole by by swivel plate 4, is reduced
The overall volume of unmanned plane main body 1, profile exquisiteness more attractive in appearance.
Used as the utility model another preferred embodiment, this unmanned aerial vehicle angle adjustable stabilizing control system is also wrapped
Include a quadra 9, the quadra 9 is installed on the upper surface of center mainboard 2, swivel plate 4 be arranged in quadra 9 and
Inwall of the two ends of swivel plate 4 respectively with quadra 9 is pivotally connected.It is directly installed on by by swivel plate 4
In quadra 9 so that swivel plate 4 it is easier for installation.
Because unmanned plane is to produce power to fly by the rotation of helical blade, process of the helical blade in high speed rotation
In, the vibrations of low amplitude high frequency can be produced, there are slight vibrations, side with the rotation of helical blade to prevent vertical bar 3
The shock absorbing apparatus 10 for damping are provided between shape framework 9 and center mainboard 2；Preferably, shock absorbing apparatus 10 are spring or shock-absorbing
Pad, certainly, the shock absorbing apparatus 10 are alternatively other elastic components being adapted for mount between quadra 9 and center mainboard 2.
Preferably, the first revolving power mechanism 6 and the second revolving power mechanism 7 are respectively the first motor and the second motor,
The output shaft of the first motor is affixed with vertical bar, and the output shaft of the second motor is affixed with swivel plate.
In order that obtaining vertical bar 3 more conforms to actual operation requirements, vertical bar 3 is traditionally arranged to be axis in axis structure, vertically
3rd revolving power mechanism 11 is installed, it is preferable that the 3rd revolving power mechanism 11 is the 3rd motor, the 3rd motor tool on bar 3
Have upper output shaft and lower output shaft, be set with the vertical bar 3 above the 3rd motor can the rotation of opposed vertical bar 3 first
Main shaft, the upper end of the first main shaft is affixed with filming apparatus 5 positioned at the upper end of vertical bar 3, the lower end of the first main shaft and the 3rd motor
Upper output shaft it is affixed, be set with vertical bar 3 below the 3rd motor can opposed vertical bar 3 rotate the second main shaft, the
The lower end of two main shafts is affixed with the filming apparatus 5 for being located at the lower end of vertical bar 3, the lower output of the upper end of the second main shaft and the 3rd motor
Axle is affixed, and during use, the 3rd motor 11 is realized clapping by controlling the first main shaft in vertical bar 3 and the second main shaft rotation
Device 5 is taken the photograph to task and the omnidirectional shooting of scenery.
It will be apparent to those skilled in the art that technical scheme that can be as described above and design, make other various
It is corresponding to change and deformation, and all these change and deformation should all belong to the protection of the utility model claim
Within the scope of.
Claims (7)
1. unmanned aerial vehicle angle adjustable stabilizing control system, it is characterised in that：Including unmanned plane main body, vertical bar, swivel plate, two
Filming apparatus, the first revolving power mechanism and the second revolving power mechanism, unmanned plane main body include center mainboard, center mainboard tool
There is the first through hole passed through for vertical bar, the second through hole passed through for vertical bar, the two ends point of swivel plate are offered on swivel plate
Bie Yu centers mainboard is pivotally connected, and vertical bar passes through first through hole and the second through hole and with swivel plate with rotatable
Mode connect, the rotation direction of swivel plate is mutually perpendicular to the rotation direction of vertical bar, and the first revolving power mechanism is installed on
Swivel plate is simultaneously connected with vertical bar driving, and the second revolving power mechanism is installed on center mainboard and is driven with swivel plate and is connected, and two
Two ends of the filming apparatus respectively with vertical bar are affixed.
2. unmanned aerial vehicle angle adjustable stabilizing control system according to claim 1, it is characterised in that：Swivel plate is arranged on
In first through hole, the two ends of swivel plate are pivotally connected with the inwall of first through hole respectively.
3. unmanned aerial vehicle angle adjustable stabilizing control system according to claim 1, it is characterised in that：Also include that one is square
Framework, the quadra is installed on the upper surface of center mainboard, swivel plate be arranged in quadra and swivel plate two ends
Pivotally it is connected with the inwall of quadra respectively.
4. unmanned aerial vehicle angle adjustable stabilizing control system according to claim 3, it is characterised in that：Quadra is with
The shock absorbing apparatus for damping are provided between heart mainboard.
5. unmanned aerial vehicle angle adjustable stabilizing control system according to claim 4, it is characterised in that：Shock absorbing apparatus are bullet
Spring or antivibration pad.
6. unmanned aerial vehicle angle adjustable stabilizing control system according to claim 1, it is characterised in that：First rotary power
Mechanism and the second revolving power mechanism are respectively the first motor and the second motor, and the output shaft of the first motor is affixed with vertical bar,
The output shaft of the second motor is affixed with swivel plate.
7. unmanned aerial vehicle angle adjustable stabilizing control system according to claim 1, it is characterised in that：Installed in vertical bar
There is the 3rd revolving power mechanism, the 3rd revolving power mechanism is the 3rd motor, and the 3rd motor has upper output shaft and lower output
Axle, be set with the vertical bar above the 3rd motor can opposed vertical bar rotation the first main shaft, the upper end of the first main shaft
Affixed with filming apparatus positioned at vertical bar upper end, the lower end of the first main shaft is affixed with the upper output shaft of the 3rd motor, positioned at
Be set with vertical bar below three motors can opposed vertical bar rotate the second main shaft, the lower end of the second main shaft be located at vertical bar
The filming apparatus of lower end are affixed, and the upper end of the second main shaft is affixed with the lower output shaft of the 3rd motor.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621106644.XU CN206273682U (en) | 2016-10-08 | 2016-10-08 | Unmanned aerial vehicle angle adjustable stabilizing control system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621106644.XU CN206273682U (en) | 2016-10-08 | 2016-10-08 | Unmanned aerial vehicle angle adjustable stabilizing control system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206273682U true CN206273682U (en) | 2017-06-23 |
Family
ID=59062376
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621106644.XU Expired - Fee Related CN206273682U (en) | 2016-10-08 | 2016-10-08 | Unmanned aerial vehicle angle adjustable stabilizing control system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206273682U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109470909A (en) * | 2018-06-21 | 2019-03-15 | 国网浙江江山市供电有限公司 | Distribution overhead line electroscope based on unmanned plane |
| CN110077612A (en) * | 2019-05-23 | 2019-08-02 | 广州市高级技工学校(广州市技师学院、广州市高级职业技术培训学院、广州市农业干部学校) | The angle adjustable stabilizing control system that unmanned aerial vehicle is taken photo by plane |
-
2016
- 2016-10-08 CN CN201621106644.XU patent/CN206273682U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109470909A (en) * | 2018-06-21 | 2019-03-15 | 国网浙江江山市供电有限公司 | Distribution overhead line electroscope based on unmanned plane |
| CN110077612A (en) * | 2019-05-23 | 2019-08-02 | 广州市高级技工学校(广州市技师学院、广州市高级职业技术培训学院、广州市农业干部学校) | The angle adjustable stabilizing control system that unmanned aerial vehicle is taken photo by plane |
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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: 20170623 Termination date: 20171008 |