CN106672252A - Unmanned aerial vehicle - Google Patents
Unmanned aerial vehicle Download PDFInfo
- Publication number
- CN106672252A CN106672252A CN201611117061.1A CN201611117061A CN106672252A CN 106672252 A CN106672252 A CN 106672252A CN 201611117061 A CN201611117061 A CN 201611117061A CN 106672252 A CN106672252 A CN 106672252A
- Authority
- CN
- China
- Prior art keywords
- unmanned plane
- horn
- lever arm
- stator
- drive division
- 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.)
- Pending
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
- B64D47/08—Arrangements of cameras
-
- G—PHYSICS
- G03—PHOTOGRAPHY; CINEMATOGRAPHY; ANALOGOUS TECHNIQUES USING WAVES OTHER THAN OPTICAL WAVES; ELECTROGRAPHY; HOLOGRAPHY
- G03B—APPARATUS OR ARRANGEMENTS FOR TAKING PHOTOGRAPHS OR FOR PROJECTING OR VIEWING THEM; APPARATUS OR ARRANGEMENTS EMPLOYING ANALOGOUS TECHNIQUES USING WAVES OTHER THAN OPTICAL WAVES; ACCESSORIES THEREFOR
- G03B17/00—Details of cameras or camera bodies; Accessories therefor
- G03B17/56—Accessories
- G03B17/561—Support related camera accessories
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
- B64U2101/30—UAVs specially adapted for particular uses or applications for imaging, photography or videography
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Accessories Of Cameras (AREA)
Abstract
The invention provides an unmanned aerial vehicle. The unmanned aerial vehicle comprises a vehicle body, a first vehicle arm, a second vehicle arm, a camera base and a camera; the first vehicle arm is connected with the vehicle body through a first sliding ring; the second vehicle arm is connected with the first vehicle arm through a second sliding ring, the camera base is connected with the second vehicle arm through a third sliding ring, and the camera is arranged on the camera base. According to the technical scheme, the problem that in the prior art, when the unmanned aerial vehicle takes pictures or photographs, the camera mechanism of the unmanned aerial vehicle cannot take pictures or photograph in an all-around mode is effectively solved.
Description
Technical field
The present invention relates to the technical field of unmanned plane, in particular to a kind of unmanned plane.
Background technology
Unmanned plane (UAV) Technology of low altitude remote sensing is one of outer hot research problem of Now Domestic, is making up satellite remote sensing Jing
While often acquisition less than image shortcoming because of cloud cover, solve conventional satellite remote sensing revisiting period it is long, it is emergent not in time
The problems such as, it is significant to China's economic construction, national defense construction and social development, meteorology, agriculture are widely used at present
The fields such as industry, resource, environment, mapping, electric inspection process, relief assistance, news report.
Two axle heads only have pitch axis and roll axle, so Airborne Camera can only carry out level and lateral rotation, camera is clapped
When taking the photograph object and needing reverse, then plane nose needs u-turn, the risk of air crash to improve.And three axle heads are the bases in two axle heads
One is increased on plinth can be with the axis of orientation of 360 ° of horizontal rotations.When camera shooting object needs reverse, then aircraft is not needed to adjust
Head, it is only necessary to which axis of orientation horizontally rotates 180 °, greatly reduces due to air crash risk caused by aircraft u-turn.But due to
The data wire quantity of high-definition digital image transmitting is more, it is impossible to from three axle head slip rings inside cabling so that high definition figure is transmitted through three
Axle head becomes a bottleneck of unmanned plane sector application.
The content of the invention
Present invention is primarily targeted at provide a kind of unmanned plane, solving unmanned plane of the prior art taking pictures or
During shooting, the problem that the camera mechanism of unmanned plane omnibearing can not take pictures or image.
To achieve these goals, the invention provides a kind of unmanned plane, including：Fuselage main body；First horn, the first machine
Arm is connected with fuselage main body by the first slip ring；Second horn, the second horn is connected with the first horn by the second slip ring；Phase
Support, camera holder is connected with the second horn by the 3rd slip ring；Camera, camera is arranged on camera holder.
Further, the first slip ring includes the first rotor and the first stator, and the first rotor is connected with the first horn, first
Stator is connected with fuselage main body；Second slip ring includes the second rotor and the second stator, and the second rotor is connected with the second horn,
Second stator is connected with the first horn；3rd slip ring includes third trochanter and the 3rd stator, and third trochanter is connected with camera holder
Connect, the 3rd stator is connected with the second horn.
Further, the surface of the first rotor, the second rotor and third trochanter is respectively provided with wire coil spaced apart from each other, respectively
Wire coil one circuit of correspondence, the tinsel for being internally provided with elasticity of the first stator, the second stator and the 3rd stator, each gold
Category silk is accordingly arranged with each wire coil.
Further, the first rotor and the first stator are fixed together using screw, and the second rotor and the second stator are adopted
Screw is fixed together, and third trochanter and the 3rd stator are fixed together using screw.
Further, unmanned plane also includes：First drive division, the first drive division drives the first horn to turn around the first rotor
It is dynamic；Second drive division, the second drive division drives the second horn to rotate around the second rotor；3rd drive division, the 3rd drive division drives
Camera holder is rotated around third trochanter.
Further, unmanned plane also includes：Controlling organization, controlling organization is arranged in the cabin of unmanned plane, controlling organization
It is connected with the first drive division, the second drive division and the 3rd drive division, to control the first drive division, the second drive division and the 3rd driving
Portion.
Further, unmanned plane also includes：Horizontal gyro, horizontal gyro is arranged in the cabin of unmanned plane, level
Gyroscope is connected with controlling organization, during so that unmanned plane being inclined, camera holding level is adjusted according to horizontal gyro.
Further, the first horn includes horizontal arm and vertical arm, and horizontal arm is connected with fuselage main body, so that horizontal arm
Rotate in horizontal plane inner circumferential.
Further, the second horn includes the first lever arm and the second lever arm, and the first lever arm is connected with vertical arm, so that the
One lever arm can be circumferentially rotated around vertical arm, and the second lever arm is vertical with the first lever arm to be connected, and the second lever arm is towards away from the side of vertical arm
To extension.
Further, camera holder includes the 3rd lever arm and the 4th lever arm, and the 3rd lever arm and the second lever arm are connected, so that the
Three lever arms can be circumferentially rotated around the second lever arm, and the 4th lever arm and the 3rd lever arm vertically connect, and the 4th lever arm faces away from the second bar
Arm extends.
Using technical scheme, unmanned plane adopts the technical scheme can be with when taking pictures or imaging
360 ° of rotation is realized in three directions, such unmanned plane is when taking pictures or imaging, it is possible to achieve three different directions
On 360 ° taking pictures or image.Technical scheme efficiently solve unmanned plane of the prior art taking pictures or
When person images, the problem that the camera mechanism of unmanned plane omnibearing can not take pictures or image.
Description of the drawings
The Figure of description for constituting the part of the application is used for providing a further understanding of the present invention, and the present invention's shows
Meaning property embodiment and its illustrated for explaining the present invention, does not constitute inappropriate limitation of the present invention.In the accompanying drawings：
Fig. 1 shows the structural representation of the camera frame of the embodiment of unmanned plane of the invention；And
Fig. 2 shows the structural representation of the first slip ring of the unmanned plane of Fig. 1.
Wherein, above-mentioned accompanying drawing includes the following drawings labelling：
10th, fuselage main body；20th, the first horn；21st, the first rotor；22nd, the first stator；30th, the second horn；40th, camera
Seat.
Specific embodiment
It should be noted that in the case where not conflicting, the feature in embodiment and embodiment in the application can phase
Mutually combination.Below with reference to the accompanying drawings and in conjunction with the embodiments describing the present invention in detail.
It is noted that described further below is all exemplary, it is intended to provide further instruction to the application.Unless another
Indicate, all technologies used herein and scientific terminology are with usual with the application person of an ordinary skill in the technical field
The identical meanings of understanding.
For the ease of description, space relative terms can be used here, such as " ... on ", " ... top ",
" in ... upper surface ", " above " etc., for describing such as a device or feature shown in the figure and other devices or spy
The spatial relation levied.It should be appreciated that space relative terms are intended to comprising the orientation except device described in figure
Outside different azimuth in use or operation.For example, if the device in accompanying drawing is squeezed, it is described as " in other devices
To be positioned as " under other devices or construction after the device of part or construction top " or " on other devices or construction "
Side " or " under other devices or construction ".Thus, exemplary term " ... top " can include " ... top " and
" in ... lower section " two kinds of orientation.The device can also other different modes positioning (being rotated by 90 ° or in other orientation), and
And respective explanations are made to the relative description in space used herein above.
Now, it is more fully described with reference to the accompanying drawings according to an illustrative embodiment of the invention.However, these are exemplary
Embodiment can be implemented by many different forms, and should not be construed to be limited solely to embodiment party set forth herein
Formula.It should be appreciated that thesing embodiments are provided so that disclosure of the invention is thoroughly and complete, and these are shown
The design of example property embodiment is fully conveyed to those of ordinary skill in the art, in the accompanying drawings, for the sake of clarity, expands layer
With the thickness in region, and make to be presented with like reference characters identical device, thus description of them will be omitted.
As shown in figure 1, the unmanned plane of the present embodiment includes：Fuselage main body 10, the first horn 20, the second horn 30, camera
Seat 40 and camera.First horn 20 is connected with fuselage main body 10 by the first slip ring.Second horn 30 passes through with the first horn 20
Second slip ring is connected.Camera holder 40 is connected with the second horn 30 by the 3rd slip ring.Camera is arranged on camera holder 40.
Using the technical scheme of the present embodiment, unmanned plane, can using technical scheme when taking pictures or imaging
To realize 360 ° of rotation in three directions, such unmanned plane is when taking pictures or imaging, it is possible to achieve three different sides
Upwards 360 ° being taken pictures or imaging.The technical scheme of the present embodiment efficiently solves unmanned plane of the prior art and is clapping
According to or during shooting, the problem that the camera mechanism of unmanned plane omnibearing can not take pictures or image.
As depicted in figs. 1 and 2, in the technical scheme of the present embodiment, the first slip ring is fixed including the first rotor 21 and first
Son 22, the first rotor 21 is connected with the first horn 20, and the first stator is connected with fuselage main body 10.Second slip ring includes second
Rotor and the second stator, the second rotor is connected with the second horn 30, and the second stator is connected with the first horn 20.3rd slip ring
Including third trochanter and the 3rd stator, third trochanter is connected with camera holder 40, and the 3rd stator is connected with the second horn 30.On
Structure is stated so that 360 ° of rotation can be realized between the first horn 20 and fuselage main body 10, the second horn 30 and the first horn 20
Between can realize 360 ° of rotation, 360 ° of rotation can be realized between the horn 30 of camera holder 40 and second.Thus realize
The rotation of the various dimensions of camera holder, specifically realizes the rotation of the various dimensions of camera.So so that camera is when taking pictures
Taking pictures for various dimensions can be carried out by camera frame, without unmanned plane the action such as turn is carried out again.
As shown in figure 1, in the technical scheme of the present embodiment, the surface of the first rotor 21, the second rotor and third trochanter
Wire coil spaced apart from each other is respectively provided with, each wire coil corresponds to a circuit, the first stator, the second stator and the 3rd stator
The tinsel of elasticity is internally provided with, each tinsel is accordingly arranged with each wire coil.So unmanned plane is to camera holder 40
Multiple circuits can be set, and then be more convenient for the control to camera.
As depicted in figs. 1 and 2, in the technical scheme of the present embodiment, the stator 22 of the first rotor 21 and first adopts screw
It is fixed together, the second rotor and the second stator are fixed together using screw, third trochanter and the 3rd stator are solid using screw
It is scheduled on together.Above-mentioned fixed form, arranges simple, and cost of manufacture is relatively low.As shown in Fig. 2 screw is three, so on the one hand
Screw is saved, furthermore such that simple structure.
As shown in figure 1, in the technical scheme of the present embodiment, unmanned plane also includes：First drive division, the first drive division drives
Dynamic first horn 20 is rotated around the first rotor.Second drive division, the second drive division drives the second horn 30 to rotate around the second rotor.
3rd drive division, the 3rd drive division drives camera holder 40 to rotate around third trochanter.The setting of the first drive division causes the first horn
20 rotation is more convenient, and the setting of the second drive division causes the rotation of the second horn more convenient, the setting of the 3rd drive division
So that the rotation of camera holder is more convenient.Said structure enables the first horn 20, the second horn 30 and camera holder to control respectively
System, is so conducive to the various dimensions of camera, the shooting of multi-angle.
As shown in figure 1, in the technical scheme of the present embodiment, unmanned plane also includes：Controlling organization, controlling organization is arranged on
In the cabin of unmanned plane, controlling organization is connected with the first drive division, the second drive division and the 3rd drive division, to control the first driving
Portion, the second drive division and the 3rd drive division.Said structure enables the first drive division, the second drive division and the 3rd drive division real
Existing intelligentized control method, the setting of controlling organization reduces artificial operation.
As shown in figure 1, in the technical scheme of the present embodiment, unmanned plane also includes：Horizontal gyro, horizontal gyro sets
Put in the cabin of unmanned plane, horizontal gyro is connected with controlling organization, during so that unmanned plane being inclined, according to horizontal gyro
To adjust camera holding level.Horizontal gyro is connected with controlling organization, can be with so when unmanned machine vibration or when inclining
Camera is adjusted by the control of horizontal gyro, makes camera keep original state.The setting of horizontal gyro is significantly
Save the labor intensity for manually adjusting.
As shown in figure 1, in the technical scheme of the present embodiment, the first horn 20 includes horizontal arm and vertical arm, horizontal arm
It is connected with fuselage main body 10, so that horizontal arm is rotated in horizontal plane inner circumferential.Said structure is easily worked, cost of manufacture compared with
It is low.Horizontal arm realizes 360 ° of rotation in horizontal plane, realizes rotation of the camera in the first dimension.
As shown in figure 1, in the technical scheme of the present embodiment, the second horn 30 includes the first lever arm and the second lever arm, the
One lever arm is connected with vertical arm, so that the first lever arm can be circumferentially rotated around vertical arm, the second lever arm is vertical with the first lever arm to be connected
Connect, the second lever arm is towards the direction extension away from vertical arm.Said structure causes camera to realize the rotation in the second dimension.
As shown in figure 1, in the technical scheme of the present embodiment, camera holder 40 includes the 3rd lever arm and the 4th lever arm, the 3rd
Lever arm and the second lever arm are connected, so that the 3rd lever arm can be circumferentially rotated around the second lever arm, the 4th lever arm and the 3rd lever arm are vertical
Connection, the 4th lever arm faces away from the extension of the second lever arm.Said structure causes camera to realize the rotation in third dimension.
In this application, three axle heads (camera frame) are made up of camera holder, the first horn and the second horn；The work of camera holder
With being fixed camera, the annexation between the first horn, the second horn and camera holder enables camera to realize three dimensions
The shooting of degree.
The operation principle of three axle heads：1. when unmanned plane run-off the straight or rotation, the horizontal gyro of three axle heads
Inclination angle just can be immediately calculated with 3-axis acceleration sensor, then signal is fed back to the control circuit of horizontal stage electric machine,
So that motor occurs corresponding rotation, the original state of camera is kept.2. when hang, want to allow camera lens to change
During shooting direction, can be rotated with controlled motor, make camera lens turn to target location.Three axle heads both can make shooting picture more
Plus delicate and smooth, reduce float, the safety of unmanned plane can be kept in the case where highly difficult shooting demand is completed again.
The slip ring of the application be responsible for for rotary body connection, conveying signal electric component, also can be popular be referred to as " rotation
Turn connection " or " rotation is logical ".Slip ring is typically mounted on the center of rotation of equipment, is mainly made up of with static two large divisions rotation.Rotation
The rotational structure of transfer part point connection equipment simultaneously rotates with motion, and referred to as " rotor ", stationary part connects the fixed structure of equipment
The energy, referred to as " stator ".Slip ring is integrally by elastic force overlap joint principle, rolling overlap joint principle or sealing principle, and moves knot
Structure makes cooperation, rational selection etc. with design of Sealing Structure, accurate part, constitutes reliable and stable rotational communication system.
Briefly, rotor surface has many wire coils spaced apart from each other, each coil one circuit of correspondence, and the inside of stator
The filament of many elasticity is arranged, each filament is pressed in a wire coil surface, thus can be in rotor
Can realize that signal transmission can reach the risk that wiring is attractive in appearance, avoid line winding again while rotation.
The application also solves the problem of wiring while high-definition digital image transmitting is realized, improves unmanned plane and flies
Capable safety and operability.Meanwhile, patrolled and examined in operation using unmanned plane, can reach patrol and examine immediately first, send out immediately
Existing defect, makes an inspection tour to rejected region lean, so as to solve the timeliness sex chromosome mosaicism that unmanned plane is patrolled and examined, greatly improves work effect
Rate and job security.Meanwhile, the project passes unmanned plane figure to possess the function of instant high definition long range propagation, can be the
Unmanned plane is patrolled and examined handling situations and is projected on command centre's sheet thousands of miles away by way of figure is passed with the first visual angle by one time
Portion's giant-screen, makes command centre's very first time intuitively understand line condition with the first visual angle, judges so as to make correct commander.
This possesses the meaning do not replaced in the patrolling and examining of unmanned plane.
It should be noted that term used herein above is merely to describe specific embodiment, and be not intended to restricted root
According to the illustrative embodiments of the application.As used herein, unless the context clearly indicates otherwise, otherwise singulative
It is also intended to include plural form, additionally, it should be understood that, when in this manual using term "comprising" and/or " bag
Include " when, it indicates existing characteristics, step, operation, device, component and/or combinations thereof.
It should be noted that description and claims of this specification and the term " first " in above-mentioned accompanying drawing, "
Two " it is etc. the object for distinguishing similar, without for describing specific order or precedence.It should be appreciated that so using
Data can exchange in the appropriate case, so that embodiments of the present invention described herein for example can be with except here
Order beyond those of diagram or description is implemented.Additionally, term " comprising " and " having " and their any deformation, it is intended that
Be cover it is non-exclusive include, for example, contain process, method, system, product or the equipment of series of steps or unit not
Be necessarily limited to those steps or the unit clearly listed, but may include clearly not list or for these processes, side
Other intrinsic steps of method, product or equipment or unit.
The preferred embodiments of the present invention are the foregoing is only, the present invention is not limited to, for the skill of this area
For art personnel, the present invention can have various modifications and variations.It is all within the spirit and principles in the present invention, made any repair
Change, equivalent, improvement etc., should be included within the scope of the present invention.
Claims (10)
1. a kind of unmanned plane, it is characterised in that include：
Fuselage main body (10)；
First horn (20), first horn (20) is connected with the fuselage main body (10) by the first slip ring；
Second horn (30), second horn (30) is connected with first horn (20) by the second slip ring；
Camera holder (40), the camera holder (40) is connected with second horn (30) by the 3rd slip ring；
Camera, the camera is arranged on the camera holder (40).
2. unmanned plane according to claim 1, it is characterised in that
First slip ring includes the first rotor and the first stator, and the first rotor is connected with first horn (20),
First stator is connected with the fuselage main body (10)；
Second slip ring includes the second rotor and the second stator, and second rotor is connected with second horn (30),
Second stator is connected with first horn (20)；
3rd slip ring includes third trochanter and the 3rd stator, and the third trochanter is connected with the camera holder (40), institute
State the 3rd stator to be connected with second horn (30).
3. unmanned plane according to claim 2, it is characterised in that the first rotor, second rotor and described
The surface of triple-spool is respectively provided with wire coil spaced apart from each other, one circuit of each wire coil correspondence, first stator,
The tinsel for being internally provided with elasticity of second stator and the 3rd stator, each tinsel and each metal wire
Circle is accordingly arranged.
4. unmanned plane according to claim 2, it is characterised in that the first rotor and first stator adopt screw
It is fixed together, second rotor and second stator are fixed together using screw, the third trochanter and described
Three stators are fixed together using screw.
5. unmanned plane according to claim 2, it is characterised in that the unmanned plane also includes：
First drive division, first drive division drives first horn (20) to rotate around the first rotor；
Second drive division, second drive division drives second horn (30) to rotate around second rotor；
3rd drive division, the 3rd drive division drives the camera holder (40) to rotate around the third trochanter.
6. unmanned plane according to claim 5, it is characterised in that the unmanned plane also includes：
Controlling organization, the controlling organization is arranged in the cabin of the unmanned plane, and the controlling organization drives with described first
Portion, second drive division are connected with the 3rd drive division, to control first drive division, second drive division and institute
State the 3rd drive division.
7. unmanned plane according to claim 6, it is characterised in that the unmanned plane also includes：
Horizontal gyro, the horizontal gyro is arranged in the cabin of the unmanned plane, the horizontal gyro and the control
Mechanism processed is connected, so that the unmanned plane adjusts the camera holding level according to the horizontal gyro when inclining.
8. unmanned plane according to claim 1, it is characterised in that first horn (20) is including horizontal arm and vertically
Arm, the horizontal arm is connected with the fuselage main body (10), so that the horizontal arm is rotated in horizontal plane inner circumferential.
9. unmanned plane according to claim 8, it is characterised in that second horn (30) is including the first lever arm and second
Lever arm, first lever arm is connected with the vertical arm, so that first lever arm can be circumferentially rotated around the vertical arm, the
Two lever arms are vertical with first lever arm to be connected, and second lever arm is towards the direction extension away from the vertical arm.
10. unmanned plane according to claim 9, it is characterised in that the camera holder (40) is including the 3rd lever arm and the 4th
Lever arm, the 3rd lever arm is connected with second lever arm, so that the 3rd lever arm can circumferentially turn around second lever arm
Dynamic, the 4th lever arm is vertical with the 3rd lever arm to be connected, and the 4th lever arm faces away from second lever arm and extends.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611117061.1A CN106672252A (en) | 2016-12-07 | 2016-12-07 | Unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611117061.1A CN106672252A (en) | 2016-12-07 | 2016-12-07 | Unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106672252A true CN106672252A (en) | 2017-05-17 |
Family
ID=58868462
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201611117061.1A Pending CN106672252A (en) | 2016-12-07 | 2016-12-07 | Unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106672252A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109835495A (en) * | 2017-11-29 | 2019-06-04 | 云南电网有限责任公司玉溪供电局 | A kind of aircraft inclination flight Self-stabilization holder |
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| JP2006264567A (en) * | 2005-03-25 | 2006-10-05 | Yamaha Motor Co Ltd | Helicopter |
| CN101811578A (en) * | 2010-04-23 | 2010-08-25 | 福建省电力有限公司福州电业局 | Special photoelectric nacelle of power patrol unmanned helicopter |
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| CN109835495A (en) * | 2017-11-29 | 2019-06-04 | 云南电网有限责任公司玉溪供电局 | A kind of aircraft inclination flight Self-stabilization holder |
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