CN206107592U - Cloud platform, imaging system and aircraft - Google Patents
Cloud platform, imaging system and aircraft Download PDFInfo
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- CN206107592U CN206107592U CN201621163553.XU CN201621163553U CN206107592U CN 206107592 U CN206107592 U CN 206107592U CN 201621163553 U CN201621163553 U CN 201621163553U CN 206107592 U CN206107592 U CN 206107592U
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- motor
- head
- rotating shaft
- cable tray
- support
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- 230000007246 mechanism Effects 0.000 claims abstract description 115
- 230000005540 biological transmission Effects 0.000 claims abstract description 47
- 238000004891 communication Methods 0.000 claims description 15
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical group O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 claims description 7
- 230000008054 signal transmission Effects 0.000 claims description 4
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims description 3
- 239000003973 paint Substances 0.000 claims description 2
- 230000001681 protective effect Effects 0.000 description 5
- 238000010586 diagram Methods 0.000 description 3
- 238000005259 measurement Methods 0.000 description 3
- 238000007789 sealing Methods 0.000 description 3
- 238000005183 dynamical system Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 230000005611 electricity Effects 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 239000000499 gel Substances 0.000 description 2
- 230000033001 locomotion Effects 0.000 description 2
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 description 1
- 239000002519 antifouling agent Substances 0.000 description 1
- 238000005452 bending Methods 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 230000001105 regulatory effect Effects 0.000 description 1
- 230000006641 stabilisation Effects 0.000 description 1
- 238000011105 stabilization Methods 0.000 description 1
- 230000003319 supportive effect Effects 0.000 description 1
- 238000004804 winding Methods 0.000 description 1
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- Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
Abstract
The utility model provides a cloud platform, imaging system and aircraft. This cloud platform includes: this cloud platform includes at least one pivot mechanism and circuit board, and this pivot mechanism includes the motor, and this motor includes rotor and stator, this rotor drives the load of this cloud platform and does exercises, this stator is hollow to what form that being used for in this motor pass the transmission line walks the line passageway, this circuit board is arranged in connecting the transmission line of this cloud platform. The utility model discloses the cloud platform can move under abominable operational environment.
Description
Technical field
The utility model embodiment is related to a kind of head, camera system and aircraft.
Background technology
Load can be carried on head, for the fixation of load, the attitude of random regulating load (for example, changes load
Highly, inclination angle and/or direction), or the attitude for being maintained at determination for load stabilization.For example, it is capture apparatus in load
When, it is mounted on head can realize stable, smooth and multi-angled shooting.
In many cases, it is desirable to which head operates in (for example, sleety weather) under severe working environment, therefore, how
It is a problem demanding prompt solution to provide a kind of head with safeguard function.
Utility model content
The utility model embodiment provides a kind of head, camera system and aircraft, can operate in severe work
Under environment.
On the one hand, there is provided a kind of head, a kind of head, it is characterised in that the head includes at least one rotating shaft mechanism
And wiring board, the rotating shaft mechanism includes motor, and the motor includes rotor and stator；The rotor drives the load of the head to be transported
It is dynamic；The stator for hollow, with formed in the motor for through the cable tray of transmission line；The wiring board is used to connect the cloud
Transmission line in platform.
On the other hand, there is provided a kind of camera system, the camera system includes head and capture apparatus, wherein, the head
Including at least one rotating shaft mechanism and wiring board, the rotating shaft mechanism includes motor, and the motor includes rotor and stator；The rotor banding
Move the load campaign of the head；The stator for hollow, with formed in the motor for through the cable tray of transmission line；
The wiring board is used to connect the transmission line in the head.
On the other hand, there is provided a kind of aircraft, including head, wherein, a kind of head, it is characterised in that the head bag
At least one rotating shaft mechanism and wiring board are included, the rotating shaft mechanism includes motor, the motor includes rotor and stator；The rotor drives
The load campaign of the head；The stator for hollow, with formed in the motor for through the cable tray of transmission line；Should
Wiring board is used to connect the transmission line in the head.
In the head of the utility model embodiment, the stator of the motor that rotating shaft mechanism includes is hollow, can form motor
Interior cable tray, so that transmission line can enter walking line in stator, and plays protective action to transmission line, makes head
Can be operated under severe working environment；And hollow by stator is set to cable tray, wiring is simple, Yi Jike
To avoid transmission line from reversing caused transmission thread breakage.
Description of the drawings
In order to be illustrated more clearly that the technical scheme of the utility model embodiment, embodiment or prior art will be retouched below
The accompanying drawing to be used needed for stating is briefly described, it should be apparent that, drawings in the following description are only the utility model
Some embodiments, for those of ordinary skill in the art, on the premise of not paying creative work, can be with basis
These accompanying drawings obtain other accompanying drawings.
Fig. 1 is schematically schemed according to the overall structure of the head of the utility model embodiment.
Fig. 2 is the schematic figure of the cabling mode of the head according to the utility model embodiment.
Fig. 3 is the schematic figure of cabling mode in part rotating shaft mechanism according to the head of the utility model embodiment.
Fig. 4 is the part isometric exploded view of the head according to the utility model embodiment.
Fig. 5 is the part isometric exploded view of the head according to the utility model embodiment.
Fig. 6 is the schematic figure of the labyrinth seal structure according to the utility model embodiment.
Fig. 7 is the schematic figure of the silica gel ring sealing structure according to the utility model embodiment.
Fig. 8 is the schematic figure of the silica gel ring sealing structure according to the utility model embodiment.
Fig. 9 is the schematic block diagram of the flight system according to the utility model embodiment.
Specific 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 a part of embodiment of the utility model, rather than the enforcement of whole
Example.Based on the embodiment in the utility model, those of ordinary skill in the art are obtained under the premise of creative work is not made
The every other embodiment for obtaining, belongs to the scope of the utility model protection.
It should be noted that when a component and another component " being fixedly connected " or " connection " in the utility model embodiment,
Or, when a component " is fixed on " another component, directly on another component, or can also there is group placed in the middle in it
Part.
Unless otherwise stated, the utility model embodiment is used all technologies and scientific terminology with it is of the present utility model
The implication that those skilled in the art are generally understood that is identical.It is concrete that term used in the utility model is intended merely to description
Embodiment purpose, it is not intended that limit scope of the present utility model.The term "and/or" that the utility model is used includes
The arbitrary and all of combination listd of one or more correlations.
The utility model embodiment provides a kind of head, and the head includes at least one rotating shaft mechanism, the rotating shaft mechanism
Including motor, the motor includes rotor and stator；The rotor drives the load campaign of the head.
Alternatively, the motor that rotating shaft mechanism includes can be brushless electric machine, it is also possible to brush motor.
Alternatively, the load can be capture apparatus, or other equipment, and the utility model embodiment is not limited
It is fixed.
Alternatively, rotating shaft mechanism includes at least one of the following：Pitch axis (pitch) mechanism, roll axle (roll) machine
Structure and yaw axis (yaw) mechanism.
Alternatively, the rotating shaft mechanism that the utility model embodiment is mentioned also includes the support being connected with the rotor, the rotor
By driving the holder pivots, the load campaign is driven.
Alternatively, the head includes multiple rotating shaft mechanisms, and multiple rotating shaft mechanisms are connected in series.Alternatively, multiple turning engines
It can be following connected mode that structure is connected in series：From the head by from the beginning of bearing, motor and the support of each rotating shaft mechanism connect
Connect, the motor connection of the support of a upper rotating shaft mechanism and next rotating shaft mechanism.
Alternatively, in the utility model embodiment, the rotor in rotating shaft mechanism is fixedly connected with support, can be indirect
It is fixedly connected.
Alternatively, in the utility model embodiment, the support of a upper rotating shaft mechanism is determined with next rotating shaft mechanism
It can be indirectly connected to that son is connected.
For example, as shown in figure 1, the head includes driftage axis mechanism 110, roll axis mechanism 120 and pitching axis mechanism 130.
Wherein, the driftage axis mechanism 110, roll axis mechanism 120 and pitching axis mechanism 130 are sequentially connected in series.
Wherein, axis mechanism 110 of going off course includes motor 112 and support 114；Roll axis mechanism 120 includes motor 122 and support
124；The pitching axis mechanism 130 includes motor 132.
Wherein, axis mechanism 110 of going off course can be connected with aircraft, and the motor 112 of axis mechanism 110 of going off course can be with yaw axis
The support 114 of mechanism 110 connects, and the support 114 of axis mechanism 110 of going off course can be connected with the motor 122 of roll axis mechanism 120,
The motor 122 of roll axis mechanism 120 can be connected with the support 124 of roll axis mechanism 120, the support 124 of roll axis mechanism 120
Can be connected with the motor 132 of pitching axis mechanism 130, the motor 132 of pitching axis mechanism 130 can be connected with load, roll axle
One end of the support 124 of mechanism 120 can be provided with limit shaft 126, and limit shaft 126 can together be rotated with load.
In the utility model embodiment, sometimes for the convenience of description, the motor of driftage axis mechanism can be referred to as inclined
Boat spindle motor, the support referred to as driftage bracing strut of axis mechanism of going off course, miscellaneous part or rotating shaft mechanism are similar to, and repeat no more.
It should be understood that in the utility model embodiment, not all of rotating shaft mechanism has support, for example, such as Fig. 1 institutes
Show, the pitching axis mechanism 130 includes motor 132 and do not include support, and the motor 132 of the pitch axis 130 can be directly connected to
Load, without by support.
It should also be understood that the rotating shaft mechanism shown in Fig. 1 is only schematically to scheme, in order to illustrate the overall structure of head, should
The concrete structure of the head of the utility model embodiment is caused to limit.For example, not shown driftage axis mechanism 110 and aircraft
Attachment structure, and not shown pitching axis mechanism 130 and the attachment structure for loading.
It will also be understood that, although Fig. 1 show driftage axis mechanism 110, roll axis mechanism 120 and pitching axis mechanism 130 successively
It is connected in series, but the utility model embodiment is not limited to this kind of connected mode, for example, it may be roll axis mechanism, pitching
Axis mechanism and driftage axis mechanism are sequentially connected in series, or, can be pitching axis mechanism, roll axis mechanism and pitching axis mechanism according to
It is secondary to be connected in series, can also be that other are connected in series mode certainly, it is numerous to list herein.
Alternatively, the concrete structure of the support of the utility model embodiment can be designed according to different demands.For example, exist
In embodiment shown in Fig. 1, roll bracing strut 124 includes two bending walls, and wherein they can be joined directly together, or by other
Part is connected, U-shaped to scrabble up.
Alternatively, in the utility model embodiment, the stator that motor includes can be hollow, for being formed in the motor
Cable tray.
Alternatively, in the utility model embodiment, cable tray can also be provided with the support that rotating shaft mechanism includes,
Cable tray in the support can extend along the bearing of trend of the support, and the cable tray in the support can not leak outside
Or it is fully closed.
Alternatively, the cable tray in support can run through whole support, it is also possible in being provided only on a part for support.
For example, the cable tray of roll bracing strut 124 can be provided only on the electricity of roll spindle motor 122 and pitching axis mechanism
In support between machine 132.
Alternatively, in the utility model embodiment, the side of support has trough, it is possible to by bracket cover and support
It is detachably connected, to seal trough, so as to form cable tray.
Alternatively, in the utility model embodiment, it is also possible to directly enter eleven punch 11 to support, to form cable tray.
Alternatively, in the utility model embodiment, the cable tray and the rotating shaft mechanism in the support of rotating shaft mechanism
Cable tray in stator is connected.
Alternatively, in the utility model embodiment, the cable tray in multiple rotating shaft mechanisms is connected.
Specifically, the cabling in the motor of the cable tray in the support of a upper rotating shaft mechanism and next rotating shaft mechanism
Passage is connected.
For example, in the utility model embodiment, the head includes first rotating shaft mechanism, the second rotating shaft mechanism and the 3rd turn
Axis mechanism, the first rotating shaft mechanism includes the first motor and first support, and second rotating shaft mechanism includes the second motor and second
Support, the 3rd rotating shaft mechanism includes the 3rd motor；Wherein, the stator of first motor is fixedly connected with aircraft, and this first
The rotor of motor is fixedly connected with the first support；The first support is fixedly connected with the stator of second motor, and this is second electric
The rotor of machine is fixedly connected with the second support；The second support is fixedly connected with the stator of the 3rd motor；3rd motor
Rotor be fixedly connected with the load.Wherein, the cable tray in the stator of first motor and the cabling in the first support
Passage is connected；Cable tray in the first support is connected with the cable tray in the stator of second motor；This second
Cable tray in the stator of motor is connected with the cable tray in the second support；Cable tray in the second support with
Cable tray in the stator of the 3rd motor is connected.
In order to make it easy to understand, describing the concrete structure of the head according to the utility model embodiment below with reference to Fig. 2-5
And cabling mode.
Wherein, Fig. 2 is the overall trace-diagram of head, and Fig. 3 is roll axle and the trace-diagram at pitch axis.Fig. 3 is the A- of Fig. 2
The section in A directions.Thicker dotted line 170 in Fig. 2 and Fig. 3 is transmission line, and dotted line expression implication is used for the purpose of and perimeter line
Bar makes a distinction, and the utility model embodiment should not be constituted and be limited.Fig. 4 and Fig. 5 are the part isometric exploded views of head.
For example, as shown in Figure 2-5, the rotor 112a gone off course in the motor 112 of axis mechanism is set in stator 112b, stator
112b is hollow, and stator 112b can be fixedly connected with attachment means 113, and attachment means 113 can arrange wiring board and turn
Jointing holes, the wiring board is used to connect transmission line, and the transfer jack can be used for being connected with aircraft, and the attachment means 113 can
To be fixed on aircraft.The rotor 112a of motor 112 can be connected to housing 115, and drive the rotation of housing 115, housing
115 can be connected with driftage bracing strut 114, it is possible to drive the rotation of the support.The support 114 can with roll axis mechanism at
Housing 121 connect, the stator 122b in roll spindle motor can be connected with the housing 121, the rotor 122a of roll spindle motor
Can be set on stator 122b, and be placed in housing 121, bonnet 123 can be covered with housing 121.Roll spindle motor 122
In rotor 122a be connected with roll bracing strut 124, rotor 122a can drive the motion of roll bracing strut 124.Roll axle
Frame 124 is connected with the housing 131 in pitching spindle motor 132, and housing 131 can be connected with the stator 132b in pitching spindle motor,
Rotor 132a in pitching spindle motor 132 is set on stator 132b, and rotor 132a is connected with load 150.
Wherein, stator 112b, the stator 122b of the motor of roll axis mechanism and the pitching gone off course in the motor of axis mechanism
The stator 132b of the motor of axis mechanism be it is hollow, so as to form cable tray.
The rack body of the support yaw axis of each rotating shaft mechanism can offer groove, and bracket cover can be covered in rack body
On, so that forming cable tray in the support.
For example, the rack body 114a of yaw axis can offer groove, and bracket cover 114b can be covered in rack body 114a
On, so that forming cable tray in the support.
Again for example, the rack body 124a of yaw axis can offer groove, and bracket cover 124b can be covered in rack body
On 124a, so that forming cable tray in the support.
Wherein, when shell is connected with stator, there can be gap so that the cable tray of stator can be walked with support
Line passage is connected.
Wherein, go off course axis mechanism 110 in motor 112 stator 112b in cable tray can with yaw axis 110 in
Cable tray in support 114 is connected, and the cable tray gone off course in bracing strut 114 can be with motor in roll axis mechanism 120
The cable tray in stator 122b in 122 is connected, the cable tray in stator 122b can with roll axis mechanism 120 in
Cable tray in support 124 is connected, the cable tray in support 124 in roll axis mechanism 120 and pitching axis mechanism 130
In the cable tray of stator 132b of motor be connected.
Then correspondingly, the cable tray in the stator 112b that transmission line can be from motor 112 is through walking in support 114
Line passage, and the cable tray of stator 122b in motor 122 is further passed through, the cable tray in support 124 is then passed through,
And further pass through the cable tray of stator 132b in motor 132.
Alternatively, the cable tray is used to accommodate power transmission line and/or signal transmssion line；Wherein, the power transmission line
For powering for the motor, and/or for the load supplying of the head；The signal transmssion line is used to transmit the communication letter of the motor
Number, and/or the signal of communication for transmitting the load.
Alternatively, the cable tray is used for through coaxial line, can be the winding displacement of coaxial line composition specifically.Certainly, should
Cable tray can pass through other kinds of transmission line, the utility model here to be not specifically limited.
Alternatively, in the utility model embodiment, transmission line can be contained in cable tray and be attached to cabling and lead to
On the wall in road, for example, can be attached on the inwall of stator, and be attached in the inwall of support.Certainly, transmission line can also
It is not attached on inwall, only in receiving and cable tray.
Alternatively, in the utility model embodiment, in order to avoid the caused transmission in rotation process of rotating shaft mechanism
The fracture of line, the transmission line in cable tray can be in cable tray into curly.Wherein, the length of curling can according to turn
Amplitude and radius setting that axle is rotated.
Alternatively, the head also includes wiring board, and the wiring board is used to connect the transmission line in head.
Alternatively, the head is additionally provided with first line plate, the first line plate be used for connection the first power transmission line and/
Or first signal transmssion line；Wherein, first power transmission line is used to be that first motor and second motor are powered；This first
Signal transmssion line is used to transmit first motor and the signal of communication of second motor.
Alternatively, the first line plate is arranged at the side away from the load of second motor.Alternatively, the First Line
Road plate is removably mounted on the side away from the load of second motor.The first line plate is optionally pcb board.
For example, there is wiring board 140 between the stator 122b and rotor 122a, with bonnet 123 of roll spindle motor.Its
In, the wiring board 140 may be used for driftage spindle motor and power, and/or the signal of communication of transmission pitching spindle motor, and/or be
Roll spindle motor is powered, and/or the signal of communication of transmission roll spindle motor.
Alternatively, the head is additionally provided with the second wiring board, second wiring board be used for connection the second power transmission line and/
Or secondary signal transmission line；Wherein, second power transmission line is used for as the 3rd motor and the load supplying；The secondary signal
Transmission line is used to transmit the signal of communication of the 3rd motor and the signal of communication of the load.
Alternatively, second wiring board is arranged at the side relative with the 3rd motor of the load.
For example, the side relative with the pitching spindle motor of load 150 is provided with wiring board 160, wherein, the wiring board
160 can power for pitch axis motor, and/or the signal of communication of transmission pitching spindle motor, and/or power for pitching spindle motor,
And/or the signal of communication of transmission pitching spindle motor.Wherein, when stator 132b of the transmission line from pitching spindle motor is passed through, can be with
From load 150 side around opposite side, to be connected to wiring board 160.
Being described above can arrange cable tray in the inside of head, such that it is able to rise to the transmission line in head
To protective action, and head is set to be operated under severe working environment.
However, the utility model embodiment is not limited to this, the utility model embodiment can also have other means to play
Protective action to head, these means can be used in combination with the means being illustrated above, or be used alone.
Alternatively, in the utility model embodiment, sealed by way of labyrinth seal at the rotation of head.
The enlarged drawing at the 6a at pitching axis mechanism shown in Fig. 3 can be as shown in Figure 6.From fig. 6 it can be seen that rotation
Place can adopt labyrinth seal structure, wherein, the width in the gap 180 in the labyrinth seal structure shown in Fig. 6 is 0.5mm,
But the utility model embodiment is not limited to this, for example, the width in the gap in labyrinth seal structure can be 0.2-0.7mm.
Alternatively, in the utility model embodiment, can with by the way of silica gel ring to it is non-rotating contact seal.
For example, as shown in Figure 7 and Figure 8, groove 153 can be opened up on the upper lid 152 of capture apparatus, and in the groove
Filling gel in 153, and cover in the main body of capture apparatus, it is of course also possible to groove is offered in capture apparatus main body, and
Filling gel, and cover upper in the main body of the capture apparatus.Wherein, Fig. 7 is the top view that silica gel ring is installed, and Fig. 8 is
The profile of silica gel ring.
Alternatively, in order to realize better seal effect, rotation water proof ring can be increased at the rotation of head, to realize
Sealing, wherein, the resistance of increase can be overcome by necessary electromotor torsion.
Alternatively, at least one wiring board for arranging in the head is coated with underwater paint, such that it is able to further increase
Waterproof.
Therefore, in the head of the utility model embodiment, the stator of the motor that rotating shaft mechanism includes is hollow, can be formed
Cable tray in motor, so that transmission line can enter walking line in stator, and plays protective action to transmission line, makes
Head can be operated under severe working environment；And hollow by stator is set to cable tray, wiring is simple, with
And transmission line can be avoided to reverse caused transmission thread breakage.
And further, cable tray is provided with rotating shaft mechanism support, further protection can be played to transmission line and be made
With.Also, the cable tray in support is connected with the cable tray in stator, can further avoid due to rotating shaft mechanism
The brought transmission line of rotation is reversed, so as to avoid transmitting thread breakage.
And in the utility model embodiment, can be by carrying out labyrinth seal or rotation water proof ring at the rotation of head
Mode sealed, or non-rotating contact is sealed by the way of silica gel ring, or coat protective paint in the circuit board,
Can protective action be played to head, head is operated under severe working environment.
Alternatively, the head can carry capture apparatus, in the utility model embodiment, can be by with capture apparatus
Camera system is referred to as with the system of head.
Alternatively, the head is used to be connected to aircraft.The aircraft can be unmanned vehicle (Unmanned
Aerial Vehicle, UAV).
In order to clearly manage aircraft, describe aircraft below with reference to the flight system shown in Fig. 9 and flying
Effect played in journey, and the object for being interacted.The present embodiment is illustrated by taking rotor craft as an example.
Flight system can include UAV200, display device 300 and commanding apparatus 400.Wherein, UAV200 can include flying
Row control system 210, dynamical system 220, head 230, load 240 and frame 250.UAV 200 can with commanding apparatus 300 and
Display device 400 carries out radio communication.
Frame 250 can include fuselage and foot rest (also referred to as undercarriage).Fuselage can include centre frame and and center
One or more horns of frame connection, one or more horns radially extend from centre frame.Foot rest is connected with fuselage, uses
In playing a supportive role when UAV 200 lands.
Dynamical system 220 can include electron speed regulator (referred to as electricity adjust) 223, one or more screws 221 and
One or more motors 222 corresponding with one or more screws 221, wherein motor 222 is connected to electron speed regulator 223
Between screw 221, motor 222 and screw 221 are arranged on corresponding horn；Electron speed regulator 223 is used to receive winged
The drive signal that row control system 210 is produced, and according to drive signal driving current is provided to motor 222, with controlled motor 222
Rotating speed.Motor 222 is used to drive screw to rotate, and so as to provide power for the flight of UAV 200, the power causes UAV
200 motions that can realize one or more frees degree.It should be understood that motor 222 can be direct current generator, it is also possible to alternating current
Machine.In addition, motor 222 can be brushless electric machine, it is also possible to brush motor.
Flight control system 210 can include flight controller 211 and sensor-based system 212.Sensor-based system 212 is used to measure
The attitude information of UAV.Sensor-based system 212 for example can include gyroscope, electronic compass, IMU (Inertial Measurement Unit,
Inertial Measurement Unit), vision sensor, GPS (global positioning system, Global Positioning
System at least one) and in the sensor such as barometer.Flight controller 211 is used to control the flight of UAV 200, for example,
The flight of UAV 200 can be controlled according to the attitude information of the measurement of sensor-based system 212.
Head 230 can be used to carry load 240.Wherein, load 240 can be capture apparatus (for example, according to machine, shooting
Machine etc.).
Display device 300 is located at the ground surface end of flight system, can be communicated with UAV 200 wirelessly, and
And it is displayed for the attitude information of UAV 200.In addition, when it is capture apparatus to load 240, can be with display device
The image that capture apparatus shoot is shown on 300.It should be understood that display device 300 can be independent equipment, it is also possible to be arranged on behaviour
It is longitudinally set with standby 400.
Commanding apparatus 400 is located at the ground surface end of unmanned flight's system, can be communicated with UAV200 wirelessly,
For carrying out remote control to UAV 200.Commanding apparatus for example can be remote control or be provided with the APP (applications of control UAV
Program, Application) terminal device, for example, smart mobile phone, panel computer etc..In embodiment of the present utility model, lead to
Cross the input of commanding apparatus receive user, can refer to by remote control pull out the input units such as wheel, button, button, rocking bar or
User interface (UI) on person's terminal device is manipulated to UAV.
The above, specific embodiment only of the present utility model, but protection domain of the present utility model do not limit to
In this, any those familiar with the art can readily occur in change in the technical scope that the utility model is disclosed
Or replace, all should cover within protection domain of the present utility model.Therefore, protection domain of the present utility model should be described with power
The protection domain that profit is required is defined.
Claims (21)
1. a kind of head, it is characterised in that the head includes at least one rotating shaft mechanism and wiring board, the rotating shaft mechanism bag
Motor is included, the motor includes rotor and stator；
The rotor drives the load campaign of the head；
The stator for hollow, with formed in the motor for through the cable tray of transmission line；
The wiring board is used to connect the transmission line in the head.
2. head according to claim 1, it is characterised in that the rotating shaft mechanism also include being connected with the rotor
Frame, the rotor drives the load to be moved by driving the holder pivots；
Wherein, cable tray is provided with the support, the cable tray in the support prolongs along the bearing of trend of the support
Stretch.
3. head according to claim 2, it is characterised in that walking in the cable tray in the support and the stator
Line passage is connected.
4. head according to any one of claim 1 to 3, it is characterised in that rotating shaft mechanism includes described at least one
At least one of the following：
Pitching axis mechanism, roll axis mechanism and driftage axis mechanism.
5. head according to any one of claim 1 to 3, it is characterised in that the cable tray is used for through coaxial
Line.
6. head according to any one of claim 1 to 3, it is characterised in that the cable tray is used to accommodate electric power
Transmission line and/or signal transmssion line；
Wherein, the power transmission line is used to be powered for the motor, and/or for the load supplying of the head；
The signal transmssion line is used to transmit the signal of communication of the motor, and/or the signal of communication for transmitting the load.
7. head according to any one of claim 1 to 3, it is characterised in that the head includes multiple rotating shafts
Mechanism, multiple rotating shaft mechanisms are connected in series；
Wherein, the cable tray in multiple rotating shaft mechanisms is connected.
8. head according to claim 7, it is characterised in that from the head by bearing from the beginning of, a upper turning engine
The motor connection of the support of structure and next rotating shaft mechanism；
Wherein, the cable tray phase in the cable tray in the support of a upper rotating shaft mechanism and the motor of next rotating shaft mechanism
Connection.
9. head according to claim 8, it is characterised in that the head includes first rotating shaft mechanism, the second turning engine
Structure and the 3rd rotating shaft mechanism, the first rotating shaft mechanism includes the first motor and first support, and second rotating shaft mechanism includes
Second motor and second support, the 3rd rotating shaft mechanism includes the 3rd motor；
Wherein, the stator of first motor is fixedly connected with aircraft, rotor and the first support of first motor
It is fixedly connected；The first support is fixedly connected with the stator of second motor, the rotor of second motor and described
Two supports are fixedly connected；The second support is fixedly connected with the stator of the 3rd motor；The rotor of the 3rd motor with
The load is fixedly connected；
Cable tray in the stator of first motor is connected with the cable tray in the first support；Described first
Cable tray in frame is connected with the cable tray in the stator of second motor；Walking in the stator of second motor
Line passage is connected with the cable tray in the second support；Cable tray in the second support and the 3rd motor
Stator in cable tray be connected.
10. head according to claim 9, it is characterised in that the head is additionally provided with first line plate, described first
Wiring board is used for the first power transmission line of connection and/or the first signal transmssion line；
Wherein, first power transmission line is used to be that first motor and second motor are powered；
First signal transmssion line is used to transmit the signal of communication of first motor and second motor.
11. heads according to the claim 10, it is characterised in that it is electric that the first line plate is arranged at described second
The side away from the load of machine.
12. heads according to claim 9, it is characterised in that the head is additionally provided with the second wiring board, described second
Wiring board is used for the second power transmission line of connection and/or secondary signal transmission line；Wherein,
Second power transmission line is used for as the 3rd motor and the load supplying；
The secondary signal transmission line is used to transmit the signal of communication of the 3rd motor and the signal of communication of the load.
13. heads according to claim 12, it is characterised in that second wiring board be arranged at the load with institute
State the relative side of the 3rd motor.
14. heads according to claim 9, it is characterised in that the first rotating shaft mechanism is driftage axis mechanism, described the
Two rotating shaft mechanisms are roll axis mechanism, and the 3rd rotating shaft mechanism is pitching axis mechanism.
15. according to any one of claims 1 to 3 head, it is characterised in that it is anti-by labyrinth at the rotation of the head
The mode of water is sealed.
16. heads according to any one of claim 1 to 3, it is characterised in that be provided with the seam crossing of the head
Silica gel ring.
17. heads according to any one of claim 1 to 3, it is characterised in that be provided with the rotation of the head anti-
Hydrosphere.
18. heads according to any one of claim 1 to 3, it is characterised in that at least one arranged in the head
Wiring board is coated with underwater paint.
19. heads according to any one of claim 1 to 3, it is characterised in that the head is used to be connected to flight
Device.
20. a kind of camera systems, it is characterised in that include the head according to any one of claim 1 to 19, and clap
Take the photograph equipment.
21. a kind of aircraft, it is characterised in that include the head according to any one of claim 1 to 19.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621163553.XU CN206107592U (en) | 2016-10-24 | 2016-10-24 | Cloud platform, imaging system and aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621163553.XU CN206107592U (en) | 2016-10-24 | 2016-10-24 | Cloud platform, imaging system and aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206107592U true CN206107592U (en) | 2017-04-19 |
Family
ID=58528184
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621163553.XU Expired - Fee Related CN206107592U (en) | 2016-10-24 | 2016-10-24 | Cloud platform, imaging system and aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206107592U (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2018076136A1 (en) * | 2016-10-24 | 2018-05-03 | 深圳市大疆创新科技有限公司 | Cradle head, photographing system and aerial vehicle |
| WO2019205037A1 (en) * | 2018-04-25 | 2019-10-31 | 深圳市大疆创新科技有限公司 | Ball head, machine frame, and unmanned aerial vehicle |
| WO2019227779A1 (en) * | 2018-05-31 | 2019-12-05 | 深圳市大疆创新科技有限公司 | Holder |
| TWI709011B (en) * | 2018-11-16 | 2020-11-01 | 大陸商廣州昂寶電子有限公司 | Method for calculating and controlling UAV heading |
| CN117146141A (en) * | 2023-10-24 | 2023-12-01 | 杭州海康威视数字技术股份有限公司 | Tripod head camera |
-
2016
- 2016-10-24 CN CN201621163553.XU patent/CN206107592U/en not_active Expired - Fee Related
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2018076136A1 (en) * | 2016-10-24 | 2018-05-03 | 深圳市大疆创新科技有限公司 | Cradle head, photographing system and aerial vehicle |
| WO2019205037A1 (en) * | 2018-04-25 | 2019-10-31 | 深圳市大疆创新科技有限公司 | Ball head, machine frame, and unmanned aerial vehicle |
| CN110637184A (en) * | 2018-04-25 | 2019-12-31 | 深圳市大疆创新科技有限公司 | Cloud platform, frame and unmanned aerial vehicle |
| CN110637184B (en) * | 2018-04-25 | 2022-05-24 | 深圳市大疆创新科技有限公司 | Cloud platform, frame and unmanned aerial vehicle |
| US11338919B2 (en) | 2018-04-25 | 2022-05-24 | SZ DJI Technology Co., Ltd. | Gimbal, frame, and unmanned aerial vehicle |
| WO2019227779A1 (en) * | 2018-05-31 | 2019-12-05 | 深圳市大疆创新科技有限公司 | Holder |
| TWI709011B (en) * | 2018-11-16 | 2020-11-01 | 大陸商廣州昂寶電子有限公司 | Method for calculating and controlling UAV heading |
| CN117146141A (en) * | 2023-10-24 | 2023-12-01 | 杭州海康威视数字技术股份有限公司 | Tripod head camera |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20190715 Address after: 518005 Baiwang Creative Factory, 1051 Songbai Road, Xili Street, Nanshan District, Shenzhen City, Guangdong Province, 7 101, 102-1 and 201/9 buildings Patentee after: DJI BAIWANG TECHNOLOGY Co.,Ltd. Address before: 518057 Guangdong province Shenzhen city Nanshan District high tech Zone South Hing a No. 9 Hongkong, Shenzhen building 6 floor Patentee before: SZ DJI TECHNOLOGY Co.,Ltd. |
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| 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: 20170419 |