CN208297905U - Camera structure, holder and unmanned plane - Google Patents
Camera structure, holder and unmanned plane Download PDFInfo
- Publication number
- CN208297905U CN208297905U CN201820850414.7U CN201820850414U CN208297905U CN 208297905 U CN208297905 U CN 208297905U CN 201820850414 U CN201820850414 U CN 201820850414U CN 208297905 U CN208297905 U CN 208297905U
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- Prior art keywords
- circuit board
- inertia measurement
- back side
- camera structure
- camera
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- 238000005259 measurement Methods 0.000 claims abstract description 94
- 238000003384 imaging method Methods 0.000 claims description 13
- 230000005611 electricity Effects 0.000 claims description 6
- 238000009434 installation Methods 0.000 abstract description 6
- 238000010586 diagram Methods 0.000 description 10
- 238000000034 method Methods 0.000 description 10
- 230000006870 function Effects 0.000 description 9
- 239000000463 material Substances 0.000 description 6
- 238000003860 storage Methods 0.000 description 6
- 230000003287 optical effect Effects 0.000 description 5
- 230000008901 benefit Effects 0.000 description 2
- 230000000295 complement effect Effects 0.000 description 2
- 238000013016 damping Methods 0.000 description 2
- 238000009413 insulation Methods 0.000 description 2
- 229910044991 metal oxide Inorganic materials 0.000 description 2
- 150000004706 metal oxides Chemical class 0.000 description 2
- 230000008569 process Effects 0.000 description 2
- 230000035939 shock Effects 0.000 description 2
- 230000000007 visual effect Effects 0.000 description 2
- 230000001154 acute effect Effects 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 239000004020 conductor Substances 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000000835 fiber Substances 0.000 description 1
- 239000004519 grease Substances 0.000 description 1
- 238000011900 installation process Methods 0.000 description 1
- 230000003993 interaction Effects 0.000 description 1
- 230000014759 maintenance of location Effects 0.000 description 1
- 239000011159 matrix material Substances 0.000 description 1
- 210000003733 optic disk Anatomy 0.000 description 1
- 239000011120 plywood Substances 0.000 description 1
- 230000001902 propagating effect Effects 0.000 description 1
- 238000004080 punching Methods 0.000 description 1
- 208000009146 rhinoscleroma Diseases 0.000 description 1
- 238000009738 saturating Methods 0.000 description 1
- 239000004065 semiconductor Substances 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U20/00—Constructional aspects of UAVs
- B64U20/80—Arrangement of on-board electronics, e.g. avionics systems or wiring
- B64U20/87—Mounting of imaging devices, e.g. mounting of gimbals
-
- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04N—PICTORIAL COMMUNICATION, e.g. TELEVISION
- H04N23/00—Cameras or camera modules comprising electronic image sensors; Control thereof
- H04N23/50—Constructional details
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C1/00—Measuring angles
-
- 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
- G03B17/02—Bodies
-
- 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
-
- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04N—PICTORIAL COMMUNICATION, e.g. TELEVISION
- H04N23/00—Cameras or camera modules comprising electronic image sensors; Control thereof
- H04N23/50—Constructional details
- H04N23/54—Mounting of pick-up tubes, electronic image sensors, deviation or focusing coils
-
- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04N—PICTORIAL COMMUNICATION, e.g. TELEVISION
- H04N23/00—Cameras or camera modules comprising electronic image sensors; Control thereof
- H04N23/57—Mechanical or electrical details of cameras or camera modules specially adapted for being embedded in other devices
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
- B64U10/13—Flying platforms
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Remote Sensing (AREA)
- Signal Processing (AREA)
- Multimedia (AREA)
- Radar, Positioning & Navigation (AREA)
- Microelectronics & Electronic Packaging (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Studio Devices (AREA)
- Camera Bodies And Camera Details Or Accessories (AREA)
- Gyroscopes (AREA)
Abstract
The utility model discloses a kind of camera structure, holder and unmanned planes.Camera structure is formed with the connected back side and side.Camera structure includes sensor circuit board, inertia measurement circuit board and Inertial Measurement Unit.The attitude data on inertia measurement circuit board and for obtaining camera is arranged in Inertial Measurement Unit.One is set to side in sensor circuit board and inertia measurement circuit board, another is set to the back side.In the camera structure of the utility model embodiment, holder and unmanned plane, one in sensor circuit board and inertia measurement circuit board is set to side, another is set to the back side, and overall volume utilization rate is higher, dramatically saves installation space.
Description
Technical field
The utility model relates to shoot field, in particular to a kind of camera structure, holder and unmanned plane.
Background technique
The camera of holder is other than needing sensor circuit board, it is also necessary to which the inertia for Inertial Measurement Unit to be arranged is surveyed
Measure circuit board, wherein Inertial Measurement Unit is used to obtain the attitude data of camera.However, sensor circuit board and inertia measurement
Circuit board is generally separately mounted on camera, and occupied space is big.
Utility model content
The utility model embodiment provides a kind of camera structure, holder and unmanned plane.
The camera structure of the utility model embodiment is formed with the connected back side and side, and the camera structure includes:
Sensor circuit board；
Inertia measurement circuit board；And
Inertial Measurement Unit, the Inertial Measurement Unit are arranged on the inertia measurement circuit board and for obtaining camera
Attitude data；
One is set to the side in the sensor circuit board and the inertia measurement circuit board, another is set to
The back side.
In some embodiments, the camera structure further include:
Imaging sensor, described image sensor are arranged on the sensor circuit board.
In some embodiments, the sensor circuit board and the inertia measurement circuit board by flexible circuit board and
The connection of camera internal element；Or
The sensor circuit board and the inertia measurement circuit board are connected with each other by flexible circuit board.
In some embodiments, the sensor circuit board, the inertia measurement circuit board and the flexible circuit board
The board structure of circuit being integrated.
In some embodiments, the flexible circuit board is located at the back side；Or
The flexible circuit board is located at the side；Or
The flexible circuit board is located at the back side and the side.
In some embodiments, the back side is the back side of camera lens, and the side is vertical with the back side.
In some embodiments, the inertia measurement circuit board includes mounting portion and extension, and the extension is one
It is connect on a direction with the mounting portion.
In some embodiments, the camera structure further includes damper element, when the inertia measurement circuit board is arranged
When the side, the damper element is between the extension and the side；When the inertia measurement circuit board is set
When being placed in the back side, the damper element is between the extension and the back side.
In some embodiments, when the inertia measurement circuit board is set to the side, the side is formed with
Groove corresponding with the extension；When the inertia measurement circuit board is set to the back side, the back side be formed with
The corresponding groove of the extension；
The damper element is filled in the groove.
The holder of the utility model embodiment includes:
Holder ontology；With
Camera structure described in any of the above-described embodiment, the camera structure are arranged on the holder ontology.
In some embodiments, the holder further includes electric tuned plate, and the sensor circuit board and/or the inertia are surveyed
Amount circuit board is connect with the electric tuned plate.
In some embodiments, unmanned plane characterized by comprising
Fuselage；With
Holder described in any of the above-described embodiment, the holder are arranged on the fuselage.
In the camera structure of the utility model embodiment, holder and unmanned plane, sensor circuit board and inertia measurement electricity
One in the plate of road is set to side, another is set to the back side, and overall volume utilization rate is higher, and it is empty to dramatically save installation
Between.
The additional aspect and advantage of the utility model embodiment will be set forth in part in the description, partially will be under
Become obvious in the description in face, or is recognized by the practice of the utility model.
Detailed description of the invention
The above-mentioned and/or additional aspect and advantage of the utility model can retouch embodiment from conjunction with following accompanying drawings
It will be apparent and be readily appreciated that in stating, in which:
Fig. 1 is the structural schematic diagram of the camera structure of the utility model certain embodiments；
Fig. 2 is the partial structure diagram of the camera structure of the utility model certain embodiments, wherein camera structure
Board structure of circuit is the first visual angle；
Fig. 3 is the partial structure diagram of the camera structure of the utility model certain embodiments, wherein camera structure
Board structure of circuit is the second visual angle；
Fig. 4 is the partial structure diagram of the camera structure of the utility model certain embodiments；
Fig. 5 is the structural schematic diagram of the camera structure of the utility model certain embodiments；
Fig. 6 is the partial structure diagram of the camera structure of the utility model certain embodiments；
Fig. 7 is the structural schematic diagram of the unmanned plane of the utility model certain embodiments；
Fig. 8 is the partial structure diagram of the unmanned plane of the utility model certain embodiments；
Fig. 9 is the partial structure diagram of the unmanned plane of the utility model certain embodiments；
Figure 10 is the partial structure diagram of the unmanned plane of the utility model certain embodiments；
Main element and symbol description:
Camera structure 10, camera lens 11, the back side 112, side 114, first side 1141, second side 1142, third side
1143, the 4th side 1144, groove 1145, incidence surface 116, sensor circuit board 12, imaging sensor 13, inertia measurement circuit
Plate 14, mounting portion 142, extension 144, first side 1441, second side 1442, third side 1443, four side 1444,
Notch 1445, Inertial Measurement Unit 15, screw 16, flexible circuit board 17, camera internal element 18, damper element 19, holder sheet
Body 30, electric tuned plate 50, holder 100, fuselage 200, core board 300, unmanned plane 1000.
Specific embodiment
The embodiments of the present invention is described below in detail, the example of the embodiment is shown in the accompanying drawings, wherein
Same or similar label indicates same or similar element or element with the same or similar functions from beginning to end.Lead to below
It crosses the embodiment being described with reference to the drawings to be exemplary, is only used for explaining the embodiments of the present invention, and cannot understand
For the limitation to the embodiments of the present invention.
In the description of the embodiments of the present invention, it is to be understood that term " center ", " longitudinal direction ", " transverse direction ",
" length ", " width ", " thickness ", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom",
The orientation or positional relationship of the instructions such as "inner", "outside", " clockwise ", " counterclockwise " is that orientation based on the figure or position are closed
System is merely for convenience of description the embodiments of the present invention and simplifies description, rather than the device of indication or suggestion meaning
Or element must have a particular orientation, be constructed and operated in a specific orientation, therefore should not be understood as to the utility model
The limitation of embodiment.In addition, term " first ", " second " are used for description purposes only, it is not understood to indicate or imply phase
To importance or implicitly indicate the quantity of indicated technical characteristic.Define " first " as a result, the feature of " second " can be with
Explicitly or implicitly include one or more feature.It is " more in the description of the embodiments of the present invention
It is a " it is meant that two or more, unless otherwise specifically defined.
In the description of the embodiments of the present invention, it should be noted that unless otherwise clearly defined and limited,
Term " installation ", " connection ", " connection " shall be understood in a broad sense, for example, it may be being fixedly connected, may be a detachable connection,
Or it is integrally connected；It can be mechanical connection, be also possible to be electrically connected or can mutually communicate；It can be and be directly connected to, it can also
To be indirectly connected with by intermediary, the connection inside two elements or the interaction relationship of two elements can be.For
For those skilled in the art, it can understand above-mentioned term in the embodiments of the present invention as the case may be
Concrete meaning.
Following disclosure provides many different embodiments or example is used to realize the embodiments of the present invention
Different structure.In order to simplify the disclosure of the embodiments of the present invention, hereinafter to the component of specific examples and be arranged into
Row description.Certainly, they are merely examples, and purpose does not lie in limitation the utility model.In addition, the implementation of the utility model
Mode can in different examples repeat reference numerals and/or reference letter, this repetition be for purposes of simplicity and clarity,
The relationship between discussed various embodiments and/or setting itself is not indicated.In addition, the embodiments of the present invention mentions
The example of the various specific techniques and material that have supplied, but those of ordinary skill in the art may be aware that other techniques are answered
With and/or other materials use.
Referring to Fig. 1, the utility model embodiment provides a kind of camera structure 10.Camera structure 10 is formed with connected
The back side 112 and side 114.The back side 112 is the back side 112 of the camera lens 11 of camera structure 10.Camera lens 11 further includes incidence surface 116.
Ambient is incident from incidence surface 116 and passes through the lens group (not shown) of camera lens 11.Incidence surface 116 and the back side 112 are located at saturating
The opposite two sides of microscope group.
Incorporated by reference to Fig. 2 and Fig. 3, camera structure 10 includes sensor circuit board 12, imaging sensor 13, inertia measurement circuit
Plate 14 and Inertial Measurement Unit 15.
Imaging sensor 13 is arranged on sensor circuit board 12.Imaging sensor 13 can be complementary metal oxide half
Conductor (Complementary Metal-Oxide Semiconductor, CMOS) imaging sensor or charge coupled cell
(Charge Coupled Device, CCD) imaging sensor etc..Imaging sensor 13 and sensor circuit board 12 are electrically connected,
And for imaging after carrying out photoelectric conversion from the incident light of incidence surface 116 to obtain image data, this image data can lead to
It crosses sensor circuit board 12 and is transmitted to the external world.
Inertial Measurement Unit 15 is arranged on inertia measurement circuit board 14.Inertial Measurement Unit 15 may include gyroscope, add
At least one of speedometer, magnetometer and pressure sensor.Inertial Measurement Unit 15 is used to obtain the attitude data of camera, example
Such as Eulerian angles, quaternary number, matrix, shaft angle, and the attitude data that will acquire are exported by inertia measurement circuit board 14 to realize
Gesture stability.
One is set to side 114 in sensor circuit board 12 and inertia measurement circuit board 14, another is set to the back side
112.For example, sensor circuit board 12 is set to side 114, inertia measurement circuit board 14 is set to the back side 112；Or sensor
Circuit board 12 is set to the back side 112, and inertia measurement circuit board 14 is set to side 114 (as shown in Figure 1).Specifically, sensor
Circuit board 12 and inertia measurement circuit board 14 can respectively by screw 16 or other such as weld, be clamped, bond mode and be fixed on
The back side 112 or side 114.Compared to the back that sensor circuit board 12 and inertia measurement circuit board 14 are stacked in camera structure 10
Face 112 or sensor circuit board 12 and inertia measurement circuit board 14 are stacked in for the side 114 of camera structure 10, this
In the camera structure 10 of utility model embodiment, one in sensor circuit board 12 and inertia measurement circuit board 14 is set to
Side 114, another is set to the back side 112, it is blocked up not to will lead to camera main-body, and overall volume utilization rate is higher, greatly
Save installation space.
In some embodiments, side 114 is vertical with the back side 112.In this way, being set to the sensor circuit at the back side 112
Plate 12 (or the inertia measurement circuit board 14 for being set to the back side 112) (or is set with the inertia measurement circuit board 14 for being set to side 114
It is placed in the sensor circuit board 12 of side 114) it is vertical arrangement, further save installation space.Side 114 can be ring junction
The lens group of structure and surrounding lens 11, specifically can substantially cirque structure (as shown in Figure 1 and Figure 4, the top of cirque structure
Portion and bottom open up jagged) or square ring structure (as shown in Figure 5 and Figure 6, side 114 includes four and joins end to end at this time
Side).
Also referring to Fig. 1 and Fig. 4, in some embodiments, side 114 includes the first side being sequentially connected
1141, second side 1142, third side 1143 and the 4th side 1144.First side 1141 and third side 1143 are opposite,
Second side 1142 and the 4th side 1144 are opposite.First side 1141, second side 1142, third side 1143 and the 4th side
Face 1144 is vertical with the back side 112.When sensor circuit board 12 is set to side 114, sensor circuit board 12 be can be set
In first side 1141, second side 1142, third side 1143 or the 4th side 1144；When inertia measurement circuit board 14 is arranged
When side 114, inertia measurement circuit board 14 be can be set in first side 1141, second side 1142, third side 1143
Or the 4th side 1144.
Certainly, in other embodiments, side 114 and the back side 112 can also at an acute angle or obtuse angle, at this point, camera
Camera lens 11 is round table-like.For example, side 114 and the back side 112 are in 80 degree of angles, so that the area of the incidence surface 116 of camera lens 11
Less than the area at the back side 112 of camera lens 11；Or side 114 and the back side 112 are in 100 degree of angles, so that camera lens 11 enters light
The area in face 116 is greater than the area etc. at the back side 112 of camera lens 11.
Referring to Fig. 1, in some embodiments, sensor circuit board 12 and inertia measurement circuit board 14 can pass through flexibility
Circuit board 17 is connected with each other.The image data that imaging sensor 13 obtains can pass through sensor circuit board 12 and flexible circuit board 17
It is transferred to inertia measurement circuit board 14, then signal transmssion line (such as coaxial line) is passed through for image data by inertia measurement circuit board 14
And/or attitude data is transferred to other processing modules and is handled；Or the attitude data that Inertial Measurement Unit 15 obtains can lead to
It crosses inertia measuring circuit plate 14 and flexible circuit board 17 is transferred to sensor circuit board 12, then letter is passed through by sensor circuit board 12
Image data and/or attitude data are transferred to other processing modules and handled by number transmission line.In this way, sensor circuit board 12
Image data and attitude data are transmitted it is not necessary that signal transmssion line is respectively set with inertia measurement circuit board 14, is conducive to reduce phase
The volume of machine structure 10.It is of course also possible to be: the image data that imaging sensor 13 obtains can by sensor circuit board 12 and
Flexible circuit board 17 is transferred to inertia measurement circuit board 14, then passes through wireless transport module for image by inertia measurement circuit board 14
Data and/or attitude data are transferred to other processing modules and are handled；Or the attitude data that Inertial Measurement Unit 15 obtains
It can be transferred to sensor circuit board 12 by inertia measurement circuit board 14 and flexible circuit board 17, then be led to by sensor circuit board 12
It crosses wireless transport module image data and/or attitude data is transferred to other processing modules and handle.In this way, sensor is electric
Road plate 12 and inertia measurement circuit board 14 are without being respectively set wireless transport module to transmit image data and attitude data.Separately
Outside, be conducive to bendingly connect positioned at the sensor circuit board 12 at the back side 112 and positioned at side 114 using flexible circuit board 17
Inertia measurement circuit board 14；Or be conducive to bendingly connect positioned at the inertia measurement circuit board 14 at the back side 112 and positioned at side
114 sensor circuit board 12.
Further, incorporated by reference to Fig. 2 and Fig. 3, sensor circuit board 12, inertia measurement circuit board 14 and flexible circuit board 17
The board structure of circuit that can be integrated.The board structure of circuit can be Rigid Flex, sensor circuit board 12 and inertia measurement electricity
Road plate 14 is the printed wiring board (Printed Circuit Board, PCB) in Rigid Flex, and flexible circuit board 17 is soft
Flexible circuit board (Flexible Printed Circuit, FPC) in scleroma plywood.Flexible circuit board 17 can be located at the back side
112 or flexible circuit board 17 be located at side 114；Or flexible circuit board 17 is across the back side 112 and side 114.
Certainly, in other embodiments, sensor circuit board 12 and inertia measurement circuit board 14 can also pass through flexible electrical
Road plate 17 and the connection (as shown in Figure 1) of camera internal element 18.Camera internal element 18 for example can be camera internal circuit, electricity
Machine etc..Specifically, sensor circuit board 12 is connected to first camera internal element, and Inertial Measurement Unit 15 is connected to second camera
Internal element, first camera internal element pass through flexible circuit board 17 with second camera internal element again and connect.
The utility model embodiment passes through flexible circuit board 17 with sensor circuit board 12 and inertia measurement circuit board 14
It is connected with each other, and sensor circuit board 12 is set to the back side 112, inertia measurement circuit board 14 carries out for being set to side 114
Explanation.
Also referring to Fig. 1 and Fig. 2, inertia measurement circuit board 14 includes mounting portion 142 and extension 144.Mounting portion 142
It is connect with flexible circuit board 17 and side 114 is fixed on by screw 16,144 self installation portion 142 of extension extends, extension
144 connect with mounting portion 142 in one direction, other three directions are free end, form peninsular structure.Inertia measurement list
Member 15 is located at extension 144.In this way, the peninsular structure, is conducive to reduce each circuit board and (such as plays screw 16 during the installation process
When) deformation occurs to stress influence caused by the Inertial Measurement Unit 15 on extension 144, to avoid Inertial Measurement Unit 15
The attitude data of acquisition has large error.Referring to Fig. 2, the extending direction of mounting portion 142 includes being distributed in the counterclockwise direction
First direction 1., second direction 2., third direction 3., fourth direction 4., the 5th direction 5., the 6th direction 6., the 7th direction
7. 8. with eighth direction.Wherein, first direction is 1. 5. parallel with the optical axis direction of lens group with the 5th direction, third direction 3. and
7th direction is 7. vertical with the optical axis direction of lens group.Extension 144 can in a first direction 1., second direction 2., third direction
3., fourth direction 4., the 5th direction 5., the 6th direction 6., the 7th direction 7. with eighth direction 8. in any one direction on
It is connect with mounting portion 142.Preferably, extension 144 second direction 2. or eighth direction is 8. upper connect with mounting portion 142.Position
In on extension 144 Inertial Measurement Unit 15 and sensor circuit board 12 and flexible circuit board 17 apart from farther out, be conducive into
One step reduces circuit board when deformation occurs to stress influence caused by Inertial Measurement Unit 15.
Referring to Fig. 1, in some embodiments, camera structure 10 further includes damper element 19.Damper element 19 it is big
It is small to cooperate with extension 144.When inertia measurement circuit board 14 is set to side 114, damper element 19 be located at extension 144 with
Between side 114；When inertia measurement circuit board 14 is set to the back side 112, damper element 19 is located at extension 144 and the back side
Between 112.The material of damper element 19 is damping grease in the utility model embodiment, and damper element 19 is slow for playing shock insulation
The effect of punching, to stress influence caused by Inertial Measurement Unit 15 when deformation occurs to reduce circuit board.Certainly, in other implementations
In mode, the material of damper element 19 is also possible to other shock insulation padded coamings, here with no restriction.
In some embodiments, when inertia measurement circuit board 14 is set to side 114, side 114 is formed with and prolongs
The corresponding groove 1145 (as shown in Figure 4) of extending portion 144；When inertia measurement circuit board 14 is set to the back side 112,112 shape of the back side
The corresponding groove 1145 of Cheng Youyu extension 144.Damper element 19 is filled in groove 1145.Extension 144 passes through damping member
19 partial receipt of part is in groove 1145.
Specifically, groove 1145 can be recessed to be formed to the direction of the optical axis close to camera structure 10 for side 114；Or
Groove 1145 is to surround from side 114 to the structure of the direction protrusion of the optical axis far from camera structure 10；Or groove 1145 is
The back side 112 is recessed to be formed to the direction close to incidence surface 116；Or groove 1145 is from the back side 112 to far from incidence surface 116
The structure of direction protrusion surrounds.
Incorporated by reference to Fig. 2, in some embodiments, extension 144 includes the first side 1441 being sequentially connected, second side
Side 1442, third side 1443 and four side 1444, first side 1441 and third side 1443 are opposite, second side 1442
Opposite with four side 1444, second side 1442 and third side 1443 are located in groove 1145, first side 1441 and the
Four side 1444 and the connection of mounting portion 142 simultaneously form notch 1445, notch 1445 and groove 1145 between mounting portion 142 respectively
Cooperation.
Referring to Fig. 7, the utility model embodiment also provides a kind of holder 100.Holder 100 includes 30 He of holder ontology
The camera structure 10 of any of the above-described embodiment.Camera structure 10 is arranged on holder ontology 30.
Specifically, holder 100 can be uniaxial holder, two axle The Cloud Terraces or three axis holders etc..Holder 100 can be hand
It holds holder or is mounted in the carrying holder used on unmanned plane 1000.When 10 carry of camera structure is when on holder ontology 30,
Holder ontology 30 stabilized camera structure 10 and can change the direction of camera structure 10, angle etc., keep camera structure 10 real
Existing steady shot and the function of adjusting shooting angle.
Fig. 8 to Figure 10 is please referred to, in some embodiments, holder 100 further includes electric tuned plate 50.Sensor circuit board 12
And/or inertia measurement circuit board 14 is connect with electric tuned plate 50.Electric tuned plate 50 also passes through the core of flexible circuit board and unmanned plane 1000
Core 300 connects.
Referring to Fig. 8, when sensor circuit board 12 is connect with electric tuned plate 50, the posture number of the acquisition of Inertial Measurement Unit 15
According to inertia measurement circuit board 14 can be passed through and flexible circuit board 17 is transferred to sensor circuit board 12, then by sensor circuit board 12
Attitude data and/or image data are transferred to electric tuned plate 50 by signal transmssion line or wireless transport module, electric tuned plate 50 is used
In processing attitude data and will be at the core board 300 that image data is transferred to unmanned plane 1000 by flexible circuit board
Reason.
Referring to Fig. 9, when inertia measurement circuit board 14 is connect with electric tuned plate 50, the picture number of the acquisition of imaging sensor 13
According to sensor circuit board 12 can be passed through and flexible circuit board 17 is transferred to inertia measurement circuit board 14, then by inertia measurement circuit board
Attitude data and/or image data are transferred to electric tuned plate 50, electric tuned plate 50 by signal transmssion line or wireless transport module by 14
For handling attitude data and image data being transferred at the core board 300 of unmanned plane 1000 by flexible circuit board
Reason.
Referring to Fig. 10, when sensor circuit board 12 and inertia measurement circuit board 14 are connect with electric tuned plate 50, image
The image data that sensor 13 obtains can be transferred to electric tuned plate 50, inertia measurement list by signal transmssion line or wireless transport module
The attitude data that member 15 obtains can be transferred to electric tuned plate 50 by signal transmssion line or wireless transport module, and electric tuned plate 50 is for locating
Reason attitude data will simultaneously be handled the core board 300 that image data is transferred to unmanned plane 1000 by flexible circuit board.
Referring to Fig. 7, the utility model embodiment also provides a kind of unmanned plane 1000.Unmanned plane 1000 includes fuselage
200 and any of the above-described embodiment holder 100.Holder 100 is arranged on fuselage 200.
In the description of this specification, reference term " embodiment ", " some embodiments ", " schematically implementation
The description of mode ", " example ", specific examples or " some examples " etc. means the tool described in conjunction with the embodiment or example
Body characteristics, structure, material or feature are contained at least one embodiment or example of the utility model.In this specification
In, schematic expression of the above terms are not necessarily referring to identical embodiment or example.Moreover, the specific spy of description
Sign, structure, material or feature can be combined in any suitable manner in any one or more embodiments or example.
Any process described otherwise above or method description are construed as in flow chart or herein, and expression includes
It is one or more for realizing specific logical function or process the step of executable instruction code module, segment or portion
Point, and the range of preferred embodiments of the present invention includes other realization, wherein can not be by shown or discussion
Sequence, including according to related function by it is basic simultaneously in the way of or in the opposite order, to execute function, this should be by this
The embodiment person of ordinary skill in the field of utility model is understood.
Expression or logic and/or step described otherwise above herein in flow charts, for example, being considered use
In the order list for the executable instruction for realizing logic function, may be embodied in any computer-readable medium, for
Instruction execution system, device or equipment (such as computer based system, including the system of processing module or other can be from instruction
Execute system, device or equipment instruction fetch and the system that executes instruction) use, or combine these instruction execution systems, device or
Equipment and use.For the purpose of this specification, " computer-readable medium " can be it is any may include, store, communicating, propagating or
Transfer program uses for instruction execution system, device or equipment or in conjunction with these instruction execution systems, device or equipment
Device.The more specific example (non-exhaustive list) of computer-readable medium include the following: there are one or more wirings
Electrical connection section (IPM current foldback circuit), portable computer diskette box (magnetic device), random access memory (RAM) are read-only to deposit
Reservoir (ROM), erasable edit read-only storage (EPROM or flash memory), fiber device and portable optic disk are only
It reads memory (CDROM).In addition, computer-readable medium can even is that the paper that can print described program on it or other conjunctions
Suitable medium, because can then be edited for example by carrying out optical scanner to paper or other media, be interpreted or when necessary
It is handled with other suitable methods electronically to obtain described program, is then stored in computer storage.
It should be appreciated that each section of the embodiments of the present invention can use hardware, software, firmware or their combination
To realize.In the above-described embodiment, multiple steps or method can be with storages in memory and by suitable instruction execution
The software or firmware that system executes are realized.For example, in another embodiment, can be used if realized with hardware
Any one of following technology well known in the art or their combination are realized: being had for realizing logic function to data-signal
The discrete logic of the logic gates of energy, the specific integrated circuit with suitable combinational logic gate circuit, programmable gate
Array (PGA), field programmable gate array (FPGA) etc..
Those skilled in the art are understood that realize all or part of step that above-described embodiment method carries
It suddenly is that relevant hardware can be instructed to complete by program, the program can store in a kind of computer-readable storage medium
In matter, which when being executed, includes the steps that one or a combination set of embodiment of the method.
In addition, can integrate in a processing module in each functional unit in each embodiment of the utility model,
It is also possible to each unit to physically exist alone, can also be integrated in two or more units in a module.Above-mentioned collection
At module both can take the form of hardware realization, can also be realized in the form of software function module.It is described integrated
If module is realized and when sold or used as an independent product in the form of software function module, also can store at one
In computer-readable storage medium.
Storage medium mentioned above can be read-only memory, disk or CD etc..
Although the embodiments of the present invention has been shown and described above, it is to be understood that above-mentioned embodiment party
Formula is exemplary, and should not be understood as limiting the present invention, and those skilled in the art are in the utility model
Above embodiment can be changed, be modified in range, replacement and variant.
Claims (12)
1. a kind of camera structure, which is characterized in that the camera structure is formed with the connected back side and side, the camera structure
Include:
Sensor circuit board；
Inertia measurement circuit board；And
The appearance on the inertia measurement circuit board and for obtaining camera is arranged in Inertial Measurement Unit, the Inertial Measurement Unit
State data；
One is set to the side in the sensor circuit board and the inertia measurement circuit board, another is set to described
The back side.
2. camera structure according to claim 1, which is characterized in that the camera structure further include:
Imaging sensor, described image sensor are arranged on the sensor circuit board.
3. camera structure according to claim 1, which is characterized in that the sensor circuit board and inertia measurement electricity
Road plate is connected by flexible circuit board with camera internal element；Or
The sensor circuit board and the inertia measurement circuit board are connected with each other by flexible circuit board.
4. camera structure according to claim 3, which is characterized in that the sensor circuit board, inertia measurement electricity
The board structure of circuit that road plate and the flexible circuit board are integrated.
5. camera structure according to claim 3, which is characterized in that
The flexible circuit board is located at the back side；Or
The flexible circuit board is located at the side；Or
The flexible circuit board is located at the back side and the side.
6. camera structure according to claim 1, which is characterized in that the back side be camera lens the back side, the side with
The back side is vertical.
7. camera structure according to claim 1, which is characterized in that the inertia measurement circuit board includes mounting portion and prolongs
Extending portion, the extension are connect with the mounting portion in one direction.
8. camera structure according to claim 7, which is characterized in that the camera structure further includes damper element, works as institute
When stating inertia measurement circuit board and being set to the side, the damper element is between the extension and the side；When
When the inertia measurement circuit board is set to the back side, the damper element is between the extension and the back side.
9. camera structure according to claim 8, which is characterized in that when the inertia measurement circuit board is set to the side
When face, the side is formed with groove corresponding with the extension；When the inertia measurement circuit board is set to the back side
When, the back side is formed with groove corresponding with the extension；
The damper element is filled in the groove.
10. a kind of holder characterized by comprising
Holder ontology；With
Camera structure described in any one of claim 1-9, the camera structure are arranged on the holder ontology.
11. holder according to claim 10, which is characterized in that the holder further includes electric tuned plate, the sensor electricity
Road plate and/or the inertia measurement circuit board are connect with the electric tuned plate.
12. a kind of unmanned plane characterized by comprising
Fuselage；With
Holder described in claim 10 or 11, the holder are arranged on the fuselage.
Priority Applications (4)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820850414.7U CN208297905U (en) | 2018-05-31 | 2018-05-31 | Camera structure, holder and unmanned plane |
| PCT/CN2018/105269 WO2019227768A1 (en) | 2018-05-31 | 2018-09-12 | Camera structure, pan-tilt and unmanned aerial vehicle |
| CN201880014280.8A CN110896684B (en) | 2018-05-31 | 2018-09-12 | Camera structure, cloud platform and unmanned aerial vehicle |
| CN202110783959.7A CN113507551A (en) | 2018-05-31 | 2018-09-12 | Camera structure, cloud platform and unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820850414.7U CN208297905U (en) | 2018-05-31 | 2018-05-31 | Camera structure, holder and unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208297905U true CN208297905U (en) | 2018-12-28 |
Family
ID=64723517
Family Applications (3)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820850414.7U Expired - Fee Related CN208297905U (en) | 2018-05-31 | 2018-05-31 | Camera structure, holder and unmanned plane |
| CN201880014280.8A Expired - Fee Related CN110896684B (en) | 2018-05-31 | 2018-09-12 | Camera structure, cloud platform and unmanned aerial vehicle |
| CN202110783959.7A Withdrawn CN113507551A (en) | 2018-05-31 | 2018-09-12 | Camera structure, cloud platform and unmanned aerial vehicle |
Family Applications After (2)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201880014280.8A Expired - Fee Related CN110896684B (en) | 2018-05-31 | 2018-09-12 | Camera structure, cloud platform and unmanned aerial vehicle |
| CN202110783959.7A Withdrawn CN113507551A (en) | 2018-05-31 | 2018-09-12 | Camera structure, cloud platform and unmanned aerial vehicle |
Country Status (2)
| Country | Link |
|---|---|
| CN (3) | CN208297905U (en) |
| WO (1) | WO2019227768A1 (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2022077365A1 (en) * | 2020-10-15 | 2022-04-21 | 深圳市大疆创新科技有限公司 | Stability-augmenting gimbal and movable platform |
Family Cites Families (15)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7710459B2 (en) * | 2004-07-21 | 2010-05-04 | Hewlett-Packard Development Company, L.P. | Ferrofluid suspension for image stabilization |
| US7893958B1 (en) * | 2006-04-03 | 2011-02-22 | D Agostino Daniel M | Vehicle video recorder |
| CN201812346U (en) * | 2010-09-30 | 2011-04-27 | 马克·伊恩·提本汉姆 | Monitoring equipment of security system |
| CN202617248U (en) * | 2012-06-04 | 2012-12-19 | 美细耐斯(上海)电子有限公司 | Camera module |
| KR102282458B1 (en) * | 2015-03-23 | 2021-07-27 | 한화테크윈 주식회사 | Method and Device for dewobbling scene |
| CN104902159A (en) * | 2015-06-30 | 2015-09-09 | 桂林飞宇电子科技有限公司 | Motion camera with lens stabilizing function |
| WO2017020245A1 (en) * | 2015-08-04 | 2017-02-09 | 桂林飞宇电子科技有限公司 | Sports camera having lens stabilization function |
| CN105744162A (en) * | 2016-02-23 | 2016-07-06 | 桂林飞宇电子科技有限公司 | Photographing system with stability enhancement function |
| CN205545612U (en) * | 2016-05-05 | 2016-08-31 | 零度智控（北京）智能科技有限公司 | Camera module and camera device |
| CN206181178U (en) * | 2016-08-31 | 2017-05-17 | 深圳零度智能飞行器有限公司 | Camera of taking photo by plane |
| CN207106921U (en) * | 2017-06-27 | 2018-03-16 | 深圳市大疆创新科技有限公司 | Unmanned plane |
| CN207292469U (en) * | 2017-08-31 | 2018-05-01 | 深圳曼塔智能科技有限公司 | Multi-pose sensor cradle head device, camera and unmanned plane during flying device |
| CN207191468U (en) * | 2017-09-11 | 2018-04-06 | 深圳市大疆创新科技有限公司 | Head camera and the unmanned plane with the head camera |
| CN207399403U (en) * | 2017-10-30 | 2018-05-22 | 南京开天眼无人机科技有限公司 | A kind of unmanned plane monitoring platform |
| CN208750323U (en) * | 2018-09-03 | 2019-04-16 | 江西希德防务系统技术有限公司 | A kind of unmanned plane electric platform mechanism |
-
2018
- 2018-05-31 CN CN201820850414.7U patent/CN208297905U/en not_active Expired - Fee Related
- 2018-09-12 CN CN201880014280.8A patent/CN110896684B/en not_active Expired - Fee Related
- 2018-09-12 WO PCT/CN2018/105269 patent/WO2019227768A1/en active Application Filing
- 2018-09-12 CN CN202110783959.7A patent/CN113507551A/en not_active Withdrawn
Also Published As
| Publication number | Publication date |
|---|---|
| CN110896684A (en) | 2020-03-20 |
| CN110896684B (en) | 2021-07-30 |
| CN113507551A (en) | 2021-10-15 |
| WO2019227768A1 (en) | 2019-12-05 |
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| GR01 | Patent grant | ||
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