CN207638745U - A kind of holder camera, cradle head device and unmanned vehicle - Google Patents
A kind of holder camera, cradle head device and unmanned vehicle Download PDFInfo
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- CN207638745U CN207638745U CN201721429153.3U CN201721429153U CN207638745U CN 207638745 U CN207638745 U CN 207638745U CN 201721429153 U CN201721429153 U CN 201721429153U CN 207638745 U CN207638745 U CN 207638745U
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- 238000003384 imaging method Methods 0.000 claims abstract description 5
- 238000001931 thermography Methods 0.000 claims description 12
- 230000005611 electricity Effects 0.000 claims description 3
- 239000000463 material Substances 0.000 abstract description 6
- 238000000034 method Methods 0.000 abstract description 2
- 238000010586 diagram Methods 0.000 description 12
- 238000009434 installation Methods 0.000 description 7
- 238000005516 engineering process Methods 0.000 description 4
- 230000005540 biological transmission Effects 0.000 description 2
- BSYNRYMUTXBXSQ-UHFFFAOYSA-N Aspirin Chemical compound CC(=O)OC1=CC=CC=C1C(O)=O BSYNRYMUTXBXSQ-UHFFFAOYSA-N 0.000 description 1
- 230000000712 assembly Effects 0.000 description 1
- 238000000429 assembly Methods 0.000 description 1
- 230000007717 exclusion Effects 0.000 description 1
- 230000004927 fusion Effects 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
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Classifications
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- 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
- H04N23/55—Optical parts specially adapted for electronic image sensors; Mounting thereof
-
- 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
- H04N23/51—Housings
-
- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04N—PICTORIAL COMMUNICATION, e.g. TELEVISION
- H04N7/00—Television systems
- H04N7/18—Closed-circuit television [CCTV] systems, i.e. systems in which the video signal is not broadcast
-
- 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)
- Multimedia (AREA)
- Signal Processing (AREA)
- Microelectronics & Electronic Packaging (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Aviation & Aerospace Engineering (AREA)
- Accessories Of Cameras (AREA)
- Studio Devices (AREA)
Abstract
The utility model embodiment belongs to holder camera technique field, is related to a kind of holder camera, is applied to unmanned vehicle, and the fuselage of the holder camera includes mounting surface and joint face, and holder connector is provided on the joint face, for being connect with holder；The holder camera includes the first image acquisition part and the second image acquisition part, described first image acquisition portion and the second image acquisition part are arranged on the mounting surface, the corresponding imaging sensor of fuselage interior that described first image acquisition portion and second image acquisition part are respectively cooperating with the holder camera completes Image Acquisition, to export two-way image.The holder camera that the utility model embodiment provides can carry out Image Acquisition under different scenes, greatly improve the application range of holder camera, while the picture material acquired is more abundant and comprehensive；In addition the utility model embodiment additionally provides the cradle head device and unmanned vehicle using the holder camera.
Description
Technical field
The utility model embodiment belongs to holder camera technique field more particularly to a kind of holder camera and uses the cloud
The cradle head device and unmanned vehicle of platform camera.
Background technology
Holder camera by holder be mounted on unmanned vehicle on, can be used for unmanned vehicle take photo by plane or special screne under
Target tracking and monitoring etc., holder camera, which is capable of providing, in unmanned vehicle flight course stablizes clearly picture；However
Existing holder camera has that application scenarios are single, the image type of acquisition is single, and the user demand that can meet has
Limit, poor universality.
Utility model content
In order to solve the problems, such as that application scenarios existing for existing holder camera are single, the image type of acquisition is single, this
Utility model embodiment provides a kind of novel holder camera, to improve the ability of the more scene applications of holder camera, to a greater extent
Ground meet user more scenes are applied and diversiform data acquire the needs of；In addition, the utility model embodiment also provides use
The cradle head device and unmanned vehicle of the holder camera.
On the one hand, the utility model embodiment provides a kind of holder camera, is applied to unmanned vehicle, the holder camera
Fuselage include mounting surface and joint face, holder connector is provided on the joint face, for being connect with holder；
The holder camera includes the first image acquisition part and the second image acquisition part, described first image acquisition portion and the
Two image acquisition parts are arranged on the mounting surface, and described first image acquisition portion and second image acquisition part are respectively cooperating with
The corresponding imaging sensor of fuselage interior of the holder camera completes Image Acquisition, to export two-way image.
There are two image acquisition parts for the holder camera setting that the utility model embodiment provides, the two image acquisition parts can
It can also be configured to share out the work and help one another to be configured to work independently, by assigning the different structure of the two image acquisition parts and work(
It can so that the holder camera can carry out Image Acquisition under different scenes, and greatly improve holder camera applies model
The picture material enclosed, while acquired is more abundant and comprehensive, can meet the needs of users to a greater extent.
On the other hand, the utility model embodiment also provides a kind of cradle head device, including holder and above-mentioned holder camera,
The holder includes the first armshaft, the second armshaft, tilting component and roll component；
Wherein, one end of first armshaft is connected by the roll component with second armshaft, second axis
One end of arm is connected to the holder connector of the holder camera by the tilting component；
The tilting component includes pitching motor, for driving the holder camera to rotate；The roll component includes cross
Motor is rolled, for driving second armshaft, the tilting component and the holder camera unitary rotation.
On the other hand, the utility model embodiment also provides a kind of unmanned vehicle, including unmanned vehicle body and cloud
Table apparatus, the cradle head device include holder and above-mentioned holder camera, and the holder includes the first armshaft, the second armshaft, bows
Face upward component and roll component；
Wherein, one end of first armshaft is connected by the roll component with second armshaft, second axis
One end of arm is connected to the holder connector of the holder camera by the tilting component, and the other end of first armshaft is solid
It is scheduled on the unmanned vehicle body；
The tilting component includes pitching motor, for driving the holder camera to rotate；The roll component includes cross
Motor is rolled, for driving second armshaft, the tilting component and the holder camera unitary rotation.
The cradle head device and unmanned vehicle provided according to the utility model embodiment, on the one hand, its holder phase used
There are two image acquisition part, the two image acquisition parts, which can be configured to work independently, can also be configured to division of labor conjunction for machine setting
Make, by assigning the two image acquisition parts different structure and functions so that the holder camera can be in different scenes
Lower carry out Image Acquisition greatly improves application range, while the picture material acquired is more abundant and comprehensive, being capable of bigger journey
It is met the needs of users on degree, on the other hand, the holder used replaces connection using twin shaft arm with tilting component, roll component
Form, it is simple in structure, it can be achieved that multistage motion control, stability higher.
Description of the drawings
It, below will be to embodiment or the prior art in order to illustrate more clearly of the utility model or scheme in the prior art
Attached drawing needed in description makees a simple introduction, it should be apparent that, the accompanying drawings in the following description is the utility model
Some embodiments for those of ordinary skill in the art without creative efforts, can also basis
These attached drawings obtain other attached drawings.
Fig. 1 is the structural schematic diagram for the holder camera that the utility model embodiment provides；
Fig. 2 is the airframe structure schematic diagram for the holder camera that Fig. 1 is provided；
Fig. 3 is that the first image acquisition part that the utility model embodiment provides and the second image acquisition part are arranged in holder phase
Schematic diagram on the fuselage of machine；
Fig. 4 is the structural schematic diagram for the holder connector that the utility model embodiment provides；
Fig. 5 is the structural schematic diagram for the cradle head device that the utility model embodiment provides；
Fig. 6 is the structural schematic diagram for the holder that the utility model embodiment provides；
Fig. 7 is the structural schematic diagram for the unmanned vehicle that the utility model embodiment provides.
Reference sign：
10 fuselages
11 mounting surfaces
111 first mounting holes
112 storage card mounting grooves
12 joint faces
121 second mounting holes
122 data-interfaces
20 first image acquisition parts
30 second image acquisition parts
40 holder connectors
41 links
411 fixed parts
412 limiting sections
50 lens mounts
1 unmanned vehicle body
2 cradle head devices
100 holder cameras
200 holders
210 first armshafts
220 second armshafts
230 roll components
231 roll motors
240 tilting components
241 pitching motors
250 Yaw assemblies
Specific implementation mode
In order to make those skilled in the art more fully understand the utility model, below to the utility model embodiment
In technical solution be clearly and completely described.Unless otherwise defined, all of technologies and scientific terms used here by the article
It has the same meaning as commonly understood by one of ordinary skill in the art to which the utility model belongs.Saying in the utility model herein
Term used in bright book, which is only for the purpose of describing specific embodiments, to be not intended to limit the utility model.
Referenced herein " embodiment " is it is meant that a particular feature, structure, or characteristic described can wrap in conjunction with the embodiments
It is contained at least one embodiment of the utility model., which there is the phrase, in each position in the description to be each meant
Identical embodiment, nor the independent or alternative embodiment with other embodiments mutual exclusion.Those skilled in the art are explicit
Ground and implicitly understand, embodiment described herein can be combined with other embodiments.
Referring to Fig. 1, Fig. 1 is a kind of holder camera that the utility model embodiment provides, which can be applied to
Unmanned vehicle, the holder camera include that fuselage 10 and the first image acquisition part 20 being arranged on fuselage 10, the second image are adopted
Collection portion 30 and holder connector 40；Fig. 2 is further regarded to, the wherein fuselage 10 of holder camera includes mounting surface 11 and joint face
12, holder connector 40 is arranged on joint face 12, and holder camera is connected to holder by holder connector 40, and the first image
Acquisition portion 20 and the second image acquisition part 30 are arranged on mounting surface 11, the first image acquisition part 20 and the second image acquisition part 30
The 10 corresponding imaging sensor in inside of fuselage for being respectively cooperating with holder camera completes Image Acquisition, to export two-way image.
In the utility model embodiment, the first image acquisition part 20 and the second image acquisition part 30 are set to holder camera
Fuselage 10 same mounting surface 11 on, wherein the first image acquisition part 20 and the second image acquisition part 30 can be set up in parallel,
It can also separate and be independently arranged, than being that the first image acquisition part 20 and the second image acquisition part 30 are set up in parallel as shown in Figure 1
Situation on the same mounting surface 11 of the fuselage 10 of holder camera, in the particular embodiment, 20 He of the first image acquisition part
Second image acquisition part 30 can be laterally arranged in same mounting surface 11, can also be longitudinally disposed in same mounting surface 11,
Or it can also be angularly disposed in same mounting surface 11；Refering to Fig. 3, (a), (c), (e), (g) are the first Image Acquisition in Fig. 3
The situation that portion 20 and the second image acquisition part 30 are set up in parallel in same mounting surface 11, (b) in Fig. 3, (d), (f), (h) are the
One image acquisition part 20 and the second image acquisition part 30 separate independently arranged situation in same mounting surface 11, wherein (a) is
The schematic diagram that first image acquisition part 20 and the second image acquisition part 30 are laterally set up in parallel in same mounting surface 11 is (c)
The schematic diagram that first image acquisition part 20 and the second image acquisition part 30 are longitudinally set up in parallel in same mounting surface 11, (e) and
(g) it is the first image acquisition part 20 and the second image acquisition part 30 oblique schematic diagram being set up in parallel in same mounting surface 11,
And (b), to be that the first image acquisition part 20 and the second image acquisition part 30 are laterally separated in same mounting surface 11 independently arranged show
It is intended to, is (d) the first image acquisition part 20 and the second image acquisition part 30 is longitudinally spaced apart in same mounting surface 11 is independently arranged
Schematic diagram, (f) and (h) be the first image acquisition part 20 and the second image acquisition part 30 it is oblique separated in same mounting surface 11
Independently arranged schematic diagram.
In another embodiment of the utility model, the first image acquisition part 20 and the second image acquisition part 30 are set to holder
On the different mounting surface 11 of the fuselage 10 of camera, again referring to Fig.2, the fuselage 10 of holder camera includes two adjacent mounting surfaces
11, the first image acquisition part 20 and the second image acquisition part 30 can be respectively installed on the two adjacent mounting surfaces 11, when
So, in other embodiments, the fuselage 10 of holder camera may include two opposite mounting surfaces 11, the first image acquisition part 20
It can be respectively installed on two opposite mounting surfaces 11 with the second image acquisition part 30.
In the above-described embodiments, the first image acquisition part 20 and the second image acquisition part 30 can be dismantled independently；Another
In some embodiments, the first image acquisition part 20 and the second image acquisition part 30 may be integral structure, the first Image Acquisition
On the mounting surface 11 for the fuselage 10 that portion 20 and the second image acquisition part 30 are removable installed in holder camera as a whole.
In the utility model embodiment, the fuselage 10 of holder camera is provided with the first image acquisition part 20 and the second image
It is additionally provided with lens mount 50 on the mounting surface 11 in acquisition portion 30, in some embodiments, the first image acquisition part 20 and
Two image acquisition parts 30 correspond to independent lens mount 50 respectively, to meet the first image acquisition part 20 and the second Image Acquisition
The independent fixed demand in portion 30；In further embodiments, the setting of lens mount 50 there are two camera lens fixed part, (do not mark by figure
Know), which fixes the first image acquisition part 20 and the second image acquisition part 30 respectively.
Further, lens mount 50 further includes fixed bit (figure does not identify), by the fixed bit camera lens is fixed
Part 50 can be fixed on the mounting surface 11 of the fuselage 10 of holder camera, specifically, the fixed bit can be screw hole or buckle
Structure so that the mode of mode or buckle that lens mount 50 can be screwed is fixed on the fuselage 10 of holder camera
Mounting surface 11 on, correspondingly, be provided on the mounting surface 11 of the fuselage 10 of holder camera matched mounting hole or
Buckle structure is provided with the first of installation lens mount 50 on the mounting surface 11 of the fuselage 10 of holder camera as shown in Figure 2
The quantity of mounting hole 111, the first mounting hole 111 can freely be set as needed.
In the utility model embodiment, again referring to Fig.2, being additionally provided on the mounting surface 11 of the fuselage 10 of holder camera
Storage card mounting groove 112, the storage card mounting groove 112 can be arranged with the first image acquisition part 20, the second image acquisition part 30
On the same mounting surface 11, different installations can also be mounted on the first image acquisition part 20, the second image acquisition part 30
On face 11, deposited with shown in Fig. 2 than the mounting surface 11 where 20 and second image acquisition part of the first image acquisition part 30 as shown in Figure 1
Mounting surface 11 where card storage mounting groove 112 is adjacent.
In the utility model embodiment, the shape of the fuselage 10 of holder camera can be cube either cylinder or class ball
Body.
In the utility model embodiment, holder connector 40 and the fuselage 10 of holder camera are structure as a whole.
In other embodiments of the utility model, holder connector 40 is removably attached on joint face 12, such as
Shown in Fig. 4, holder connector 40 includes horseshoe-shaped link 41, and the fixed part 411 that is arranged on link 41 and
Limiting section 412, fixed part 411 are fixed for holder connector 40 in the installation of the joint face 12 of the fuselage 10 of holder camera, together
Sample, which can be screw hole or buckle structure so that mode that holder connector 40 can be screwed or
On the joint face 12 for the fuselage 10 that the mode of person's buckle is fixed on holder camera, correspondingly, the company of the fuselage 10 in holder camera
Matched mounting hole or buckle structure are provided in junction 12, as shown in Figure 2 in the connection of the fuselage 10 of holder camera
The second mounting hole 121 of installation holder connector 40 is provided on face 12, the quantity of the second mounting hole 121 can as needed freely
Setting；And connection of the limiting section 412 for holder and holder connector 40 limits, and is connect with to ensure holder with holder camera steady
It is qualitative.
Optionally, the joint face 12 of the fuselage 10 of holder camera includes opposite the first joint face and the second joint face,
Be both provided with holder connector 40 on first joint face and the second joint face, holder simultaneously with the first joint face and the second joint face
On holder connector 40 connect, it will be understood that the connection of same holder can be set on the first joint face and the second joint face
Part 40 can also be arranged the holder connector 40 of different structure, for example holder connector shown in Fig. 4 is arranged in the first joint face
40, and an axis hole is only set on the second joint face, such, not reinflated explanation herein.
In the utility model embodiment, again referring to Fig.2, being additionally provided on the joint face 12 of the fuselage 10 of holder camera
Data-interface 122, when holder camera is mounted on holder, corresponding on the holder interface of data-interface 122 connects, with to cloud
The image data of the unmanned vehicle transmission holder camera acquisition of platform connection.
In the above-described embodiments, the first image acquisition part 20 and the second image acquisition part 30 can be infrared thermal imaging camera lenses
With it is one or two kinds of in visible light lens, you can be the first image acquisition part 20 be infrared thermal imaging camera lens, the second figure
Picture acquisition portion 30 is visible light lens for visible light lens or the first image acquisition part 20 and the second image acquisition part 30,
Or first image acquisition part 20 and the second image acquisition part 30 be infrared thermal imaging camera lens；Wherein, the first image is adopted
Integrate portion 20 as infrared thermal imaging camera lens, the second image acquisition part 30 is the situation of visible light lens, using the nothing of the holder camera
People's aircraft can both take photo by plane in day flight, can also take photo by plane in night flying, meet more scene capture demands,
Different types of image can also be acquired simultaneously, meets the acquisition demand of variety of images；For 20 He of the first image acquisition part
Second image acquisition part 30 is the situation of visible light lens, under the good environment of light, can be carried out in different directions
Image Acquisition only can also enable one of them and carry out unidirectional Image Acquisition, and more scene captures and more can be achieved in this way
The demand of sample Image Acquisition；It is infrared thermal imaging camera lens for the first image acquisition part 20 and the second image acquisition part 30
Situation can carry out infrared image acquisition, can also only enable one of them in different directions under the poor environment of light
And unidirectional infrared image acquisition is carried out, equally realize the demand of more scene captures and variety of images acquisition；At other
In embodiment, can also the two-way image/video that the first image acquisition part 20 and the second image acquisition part 30 acquire be subjected to image and melted
It closes or carries out picture-in-picture to show, novel image is provided and shows content.
There are following advantages relative to existing holder camera for the holder camera that the utility model embodiment provides：
There are two image acquisition parts for the holder camera setting that the utility model embodiment provides, the two image acquisition parts can
It can also be configured to share out the work and help one another to be configured to work independently, by assigning the different structure of the two image acquisition parts and work(
It can so that the holder camera can carry out Image Acquisition under different scenes, and greatly improve holder camera applies model
The picture material enclosed, while acquired is more abundant and comprehensive, can meet the needs of users to a greater extent.
The utility model embodiment also provides a kind of cradle head device, and refering to Fig. 5 and Fig. 6, cradle head device includes holder camera
100 and holder 200, holder 200 includes the first armshaft 210, the second armshaft 220, roll component 230 and tilting component 240, and first
One end of armshaft 210 is connected by roll component 230 and the second armshaft 220, and one end of the second armshaft 220 passes through tilting component
240 are connected to the holder connector 40 of holder camera 100；
Tilting component 240 includes pitching motor 241, for driving holder camera 100 to rotate；Roll component 230 includes cross
Motor 231 is rolled, for driving the second armshaft 220,100 unitary rotation of tilting component 240 and holder camera.
Cradle head device further includes Yaw assembly 250, and the other end of the first armshaft 210 connects Yaw assembly 250, Yaw assembly
250 include yaw motor (figure does not identify), for driving the first armshaft 210, roll component 230, the second armshaft 220, pitching group
100 unitary rotation of part 240 and holder camera.
Wherein, holder camera 100 is the holder camera 100 described in above-described embodiment, again refering to fig. 1 to Fig. 4, holder phase
Machine 100 includes fuselage 10 and the first image acquisition part 20 being arranged on fuselage 10, the second image acquisition part 30 and company of holder 200
Fitting 40；Further, the fuselage 10 of holder camera 100 includes mounting surface 11 and joint face 12, the setting of 200 connector 40 of holder
On joint face 12, holder camera 100 is connected to holder 200 by 200 connector 40 of holder, and 20 He of the first image acquisition part
Second image acquisition part 30 is arranged on mounting surface 11, and the first image acquisition part 20 and the second image acquisition part 30 are respectively cooperating with cloud
The 10 corresponding imaging sensor in inside of fuselage of platform camera 100 completes Image Acquisition, to export two-way image.
In the utility model embodiment, the first image acquisition part 20 and the second image acquisition part 30 are set to holder camera
On the same mounting surface 11 of 100 fuselage 10, wherein the first image acquisition part 20 and the second image acquisition part 30 can be set side by side
It sets, can also separate and be independently arranged, than being that the first image acquisition part 20 and the second image acquisition part 30 are set side by side as shown in Figure 1
The situation being placed on the same mounting surface 11 of the fuselage 10 of holder camera 100, in the particular embodiment, the first image acquisition part
20 and second image acquisition part 30 can laterally be arranged in same mounting surface 11, can also longitudinally be set in same mounting surface 11
It sets, or can also be angularly disposed in same mounting surface 11；
In another embodiment of the utility model, the first image acquisition part 20 and the second image acquisition part 30 are set to holder
On the different mounting surface 11 of the fuselage 10 of camera 100, again referring to Fig.2, the fuselage 10 of holder camera 100 includes two adjacent
Mounting surface 11, the first image acquisition part 20 and the second image acquisition part 30 can be respectively installed in the two adjacent mounting surfaces 11
On, certainly, in other embodiments, the fuselage 10 of holder camera 100 may include two opposite mounting surfaces 11, the first image
Acquisition portion 20 and the second image acquisition part 30 can be respectively installed on two opposite mounting surfaces 11, in this case, cloud
Table apparatus drives holder camera 100 to rotate, it can be achieved that the first image acquisition part 20 and the second Image Acquisition by tilting component 240
Position switching of the portion 30 on unmanned vehicle course.
In the above-described embodiments, the first image acquisition part 20 and the second image acquisition part 30 can be dismantled independently；Another
In some embodiments, the first image acquisition part 20 and the second image acquisition part 30 may be integral structure, the first Image Acquisition
Portion 20 and the second image acquisition part 30 are removable installed in the mounting surface 11 of the fuselage 10 of holder camera 100 as a whole
On.
In the utility model embodiment, the fuselage 10 of holder camera 100 is provided with the first image acquisition part 20 and second
It is additionally provided with lens mount 50 on the mounting surface 11 of image acquisition part 30, in some embodiments, the first image acquisition part 20
Independent lens mount 50 is corresponded to respectively with the second image acquisition part 30, to meet the first image acquisition part 20 and the second image
The independent fixed demand in acquisition portion 30；In further embodiments, (figure is not there are two camera lens fixed part for the setting of lens mount 50
Mark), which fixes the first image acquisition part 20 and the second image acquisition part 30 respectively.
Further, lens mount 50 further includes fixed bit, by the fixed bit lens mount 50 is consolidated
It is scheduled on the mounting surface 11 of the fuselage 10 of holder camera 100, specifically, the fixed bit can be screw hole or buckle structure, makes
The mode of mode or buckle that can be screwed of lens mount 50 be fixed on holder camera 100 fuselage 10 peace
On dress face 11, correspondingly, being provided with matched mounting hole or card on the mounting surface 11 of the fuselage 10 of holder camera 100
Buckle structure is provided with the first of installation lens mount 50 on the mounting surface 11 of the fuselage 10 of holder camera 100 as shown in Figure 2
The quantity of mounting hole 111, the first mounting hole 111 can freely be set as needed.
In the utility model embodiment, again referring to Fig.2, also being set on the mounting surface 11 of the fuselage 10 of holder camera 100
It is equipped with storage card mounting groove 112, which can be with the first image acquisition part 20, the second image acquisition part 30
It is arranged on the same mounting surface 11, can also be mounted on the first image acquisition part 20, the second image acquisition part 30 different
On mounting surface 11, the mounting surface 11 than 20 and second image acquisition part of the first image acquisition part, 30 place as shown in Figure 1 and Fig. 2 institutes
Mounting surface 11 where showing storage card mounting groove 112 is adjacent.
In the utility model embodiment, the shape of the fuselage 10 of holder camera 100 can be cube either cylinder or
Globoid.
In the utility model embodiment, 200 connector 40 of holder and the fuselage 10 of holder camera 100 are structure as a whole.
In some embodiments of the utility model, 200 connector 40 of holder is removably attached on joint face 12, as shown in figure 4,
200 connector 40 of holder includes horseshoe-shaped link 41, and the fixed part 411 and limiting section being arranged on link 41
412, fixed part 411 is fixed for 200 connector 40 of holder in the installation of the joint face 12 of the fuselage 10 of holder camera 100, together
Sample, which can be screw hole or buckle structure so that the side that 200 connector 40 of holder can be screwed
Formula or the mode of buckle are fixed on the joint face 12 of the fuselage 10 of holder camera 100, correspondingly, in holder camera 100
Matched mounting hole or buckle structure are provided on the joint face 12 of fuselage 10, as shown in Figure 2 in holder camera 100
The second mounting hole 121 of installation 200 connector 40 of holder, the number of the second mounting hole 121 are provided on the joint face 12 of fuselage 10
Amount can freely be set as needed；And limiting section 412 is limited for holder 200 and the connection of 200 connector 40 of holder, to ensure
The stability that holder 200 is connect with holder camera 100, the wherein connecting component of the rotation axis connection of the pitching motor of holder 200
The intermediate region of embedded link, limiting section 412 thereon are supported to limiting section 412.
Optionally, the joint face 12 of the fuselage 10 of holder camera 100 includes opposite the first joint face and the second joint face,
Be both provided with 200 connector 40 of holder on the first joint face and the second joint face, holder 200 simultaneously with the first joint face and the
200 connector 40 of holder connection on two joint faces, can so improve the stability that holder 200 is connect with holder camera 100,
It is appreciated that 200 connector 40 of same holder can be arranged on the first joint face and the second joint face, difference can also be set
200 connector 40 of holder of structure, for example 200 connector 40 of holder shown in Fig. 4 is set in the first joint face, and connect second
One axis hole is only set in junction, and one end of the second armshaft 220 of holder 200 is connected to cloud shown in Fig. 4 by tilting component 240
200 connector 40 of platform, and the other end is inserted directly into the axis hole by the rotary shaft of end set, completes connection, it is such,
This not reinflated explanation.
In the utility model embodiment, again referring to Fig.2, also being set on the joint face 12 of the fuselage 10 of holder camera 100
It is equipped with data-interface 122, when holder camera 100 is mounted on holder 200, the interface corresponding on holder 200 of data-interface 122
Connection, with the image data acquired to the unmanned vehicle transmission holder camera 100 being connect with holder 200.
In the above-described embodiments, the first image acquisition part 20 and the second image acquisition part 30 can be infrared thermal imaging camera lenses
With it is one or two kinds of in visible light lens, you can be the first image acquisition part 20 be infrared thermal imaging camera lens, the second figure
Picture acquisition portion 30 is visible light lens for visible light lens or the first image acquisition part 20 and the second image acquisition part 30,
Or first image acquisition part 20 and the second image acquisition part 30 be infrared thermal imaging camera lens；Wherein, the first image is adopted
Integrate portion 20 as infrared thermal imaging camera lens, the second image acquisition part 30 is the situation of visible light lens, using the holder camera 100
Unmanned vehicle can both take photo by plane in day flight, can also take photo by plane in night flying, meet more scene capture need
It asks, while different types of image can also be acquired, meet the acquisition demand of variety of images；For the first image acquisition part 20
Be the situation of visible light lens with the second image acquisition part 30, under the good environment of light, can in different directions into
Row Image Acquisition only can also enable one of them and carry out unidirectional Image Acquisition, in this way can be achieved more scene captures and
The demand of variety of images acquisition；It is infrared thermal imaging camera lens for the first image acquisition part 20 and the second image acquisition part 30
Situation can carry out infrared image acquisition in different directions under the poor environment of light, can also only enable wherein one
It is a and carry out unidirectional infrared image acquisition, equally realize the demand of more scene captures and variety of images acquisition；At it
In his embodiment, can also the two-way image/video that the first image acquisition part 20 and the second image acquisition part 30 acquire be subjected to image
Fusion or progress picture-in-picture are shown, are provided novel image and are shown content.
The correlation for the holder camera of holder camera 100 described in the present embodiment also seen described in previous embodiment
Technology contents.
The cradle head device provided according to the utility model embodiment, on the one hand, its holder camera 100 used is provided with two
A image acquisition part, the two image acquisition parts can be configured to work independently and can also be configured to share out the work and help one another, and pass through imparting
The different structure and function of the two image acquisition parts so that the holder camera 100 can carry out figure under different scenes
As acquisition, application range is greatly improved, while the picture material acquired is more abundant with comprehensively, can meet to a greater extent
The demand of user, on the other hand, the holder 200 used is using twin shaft arm and tilting component 240, roll component 230, yaw group
Part 250 replaces type of attachment and forms the steady holder 200 of increasing of two axis or three axis, it can be achieved that the steady function of the increasing of holder camera 100, expands
Exhibition shooting spatial dimension, holder 200 provided by the utility model is simple in structure, it can be achieved that multistage motion control, stability is more
It is high.
The utility model embodiment also provides a kind of unmanned vehicle, as shown in fig. 7, unmanned vehicle includes unmanned flight
Device body 1 and cradle head device 2, wherein cradle head device 2 include holder camera 100 and holder 200, and holder 200 includes the first armshaft
210, one end of the second armshaft 220, tilting component 240 and roll component 230, the first armshaft 210 passes through roll component 230 and
Two armshafts 220 connect, and one end of the second armshaft 220 is connected to the holder connector of holder camera 100 by tilting component 240
40, the other end of the first armshaft 210 is fixed on unmanned vehicle body 1；
Tilting component 240 includes pitching motor, for driving holder camera 100 to rotate；Roll component 230 includes roll electricity
Machine, for driving the second armshaft 220,100 unitary rotation of tilting component 240 and holder camera.
Further, cradle head device 2 further includes Yaw assembly 250, and the other end of the first armshaft 210 connects Yaw assembly
250, Yaw assembly 250 is fixed on unmanned vehicle body 1；Yaw assembly 250 includes yaw motor, for driving first axle
Arm 210, roll component 230,100 unitary rotation of the second armshaft 220, tilting component 240 and holder camera.In some embodiments
In, Yaw assembly 250 and the junction of unmanned vehicle body 1 are optionally also set in the Quick Release interface using Quick Release interface
It is equipped with sealing element, improves the water resistance of cradle head device 2 so that cradle head device 2 can be used in the rain or in wet environment.
In the present embodiment, the relevant technologies content of the holder camera 100 and the cradle head device 2 sees aforementioned reality
The holder camera and cradle head device of example offer are applied, details are not described herein.
The unmanned vehicle provided according to the utility model embodiment, on the one hand, its holder camera 100 used is provided with
Two image acquisition parts, the two image acquisition parts can be configured to work independently and can also be configured to share out the work and help one another, and pass through tax
Give the different structure and function of the two image acquisition parts so that the holder camera 100 can carry out under different scenes
Image Acquisition greatly improves application range, while the picture material acquired is more abundant and comprehensive, can expire to a greater extent
The demand of sufficient user, on the other hand, the holder 200 used is using twin shaft arm and tilting component 240, roll component 230, yaw
Component 250 replaces type of attachment and forms the steady holders 200 of increasing of two axis or three axis, it can be achieved that the steady function of the increasing of holder camera 100,
Extension shooting spatial dimension, holder 200 provided by the utility model are simple in structure, it can be achieved that multistage motion control, stability
Higher.
Obviously, embodiments described above is only the utility model a part of the embodiment, rather than whole implementation
, the preferred embodiment of the utility model is given in attached drawing, but be not intended to limit the scope of the claims of the utility model.This practicality is new
Type can realize in many different forms, make public affairs to the utility model on the contrary, purpose of providing these embodiments is
The understanding for opening content is more thorough and comprehensive.Although the utility model is described in detail with reference to the foregoing embodiments, for
For those skilled in the art comes, the technical solution recorded in aforementioned each specific implementation mode can still be repaiied
Change, or equivalence replacement is carried out to which part technical characteristic.It is every to be done using the utility model specification and accompanying drawing content
Equivalent structure, other related technical areas are directly or indirectly used in, similarly in the utility model patent protection domain
Within.
Claims (15)
1. a kind of holder camera, be applied to unmanned vehicle, which is characterized in that the fuselage of the holder camera include mounting surface and
Joint face is provided with holder connector on the joint face, for being connect with holder；
The holder camera includes the first image acquisition part and the second image acquisition part, described first image acquisition portion and the second figure
As acquisition portion is arranged on the mounting surface, described first image acquisition portion and second image acquisition part are respectively cooperating with described
The corresponding imaging sensor of fuselage interior of holder camera completes Image Acquisition, to export two-way image.
2. holder camera according to claim 1, which is characterized in that described first image acquisition portion and the second Image Acquisition
Portion is set on the same mounting surface of the fuselage of the holder camera.
3. holder camera according to claim 2, which is characterized in that described first image acquisition portion and the second Image Acquisition
Portion is laterally set up in parallel in the mounting surface；Or
Described first image acquisition portion and the second image acquisition part are longitudinally set up in parallel in the mounting surface；Or
Described first image acquisition portion and the second image acquisition part is oblique in the mounting surface is set up in parallel.
4. holder camera according to claim 2, which is characterized in that the fuselage of the holder camera is provided with described first
It is additionally provided with lens mount on the mounting surface of image acquisition part and the second image acquisition part.
5. holder camera according to claim 2, which is characterized in that described first image acquisition portion and the second Image Acquisition
Portion can independently dismantle.
6. holder camera according to claim 1, which is characterized in that described first image acquisition portion and the second Image Acquisition
Portion is set to mounting surface different on the fuselage of the holder camera.
7. holder camera according to claim 1, which is characterized in that described first image acquisition portion and the second Image Acquisition
Portion is structure as a whole, and is set to the holder camera to described first image acquisition portion and the second image acquisition part Whole-dismountable
Fuselage mounting surface on.
8. holder camera according to claim 1, which is characterized in that the joint face include opposite the first joint face and
Second joint face.
9. holder camera according to claim 1, which is characterized in that the machine of the holder connector and the holder camera
As integral structure；Or
The holder connector is removably attached on the joint face.
10. holder camera according to claim 1, which is characterized in that be additionally provided with data-interface, institute on the joint face
When stating holder camera on holder, data-interface interface connection corresponding on holder.
11. holder camera according to claim 1, which is characterized in that described first image acquisition portion is infrared thermal imaging
Camera lens, second image acquisition part are visible light lens；Or
Described first image acquisition portion and second image acquisition part are visible light lens；Or
Described first image acquisition portion and second image acquisition part are infrared thermal imaging camera lens.
12. a kind of cradle head device, which is characterized in that including holder and claim 1 to 11 any one of them holder camera, institute
It includes the first armshaft, the second armshaft, tilting component and roll component to state holder；
Wherein, one end of first armshaft is connected by the roll component with second armshaft, second armshaft
One end is connected to the holder connector of the holder camera by the tilting component；
The tilting component includes pitching motor, for driving the holder camera to rotate；The roll component includes roll electricity
Machine, for driving second armshaft, the tilting component and the holder camera unitary rotation.
13. cradle head device according to claim 12, the cradle head device further includes Yaw assembly, first armshaft
The other end connects the Yaw assembly.
14. a kind of unmanned vehicle, which is characterized in that the unmanned vehicle includes unmanned vehicle body and cradle head device,
The cradle head device includes holder and claim 1 to 11 any one of them holder camera, the holder include the first armshaft,
Second armshaft, tilting component and roll component；
Wherein, one end of first armshaft is connected by the roll component with second armshaft, second armshaft
One end is connected to the holder connector of the holder camera by the tilting component, and the other end of first armshaft is fixed on
On the unmanned vehicle body；
The tilting component includes pitching motor, for driving the holder camera to rotate；The roll component includes roll electricity
Machine, for driving second armshaft, the tilting component and the holder camera unitary rotation.
15. unmanned vehicle according to claim 14, which is characterized in that the cradle head device further includes Yaw assembly,
The other end of first armshaft connects the Yaw assembly, and the Yaw assembly is fixed on the unmanned vehicle body；
The Yaw assembly includes yaw motor, for drive first armshaft, the roll component, second armshaft,
The tilting component and the holder camera unitary rotation.
Priority Applications (4)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721429153.3U CN207638745U (en) | 2017-10-31 | 2017-10-31 | A kind of holder camera, cradle head device and unmanned vehicle |
| PCT/CN2017/115277 WO2019085154A1 (en) | 2017-10-31 | 2017-12-08 | Pan-tilt camera, pan-tilt device and unmanned aerial vehicle |
| CN201780003968.1A CN108401495B (en) | 2017-10-31 | 2017-12-08 | Cloud platform camera, cloud platform device and unmanned vehicles |
| CN202110179237.0A CN112804433A (en) | 2017-10-31 | 2017-12-08 | Cloud platform camera, cloud platform device and unmanned vehicles |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721429153.3U CN207638745U (en) | 2017-10-31 | 2017-10-31 | A kind of holder camera, cradle head device and unmanned vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207638745U true CN207638745U (en) | 2018-07-20 |
Family
ID=62859303
Family Applications (2)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721429153.3U Active CN207638745U (en) | 2017-10-31 | 2017-10-31 | A kind of holder camera, cradle head device and unmanned vehicle |
| CN202110179237.0A Pending CN112804433A (en) | 2017-10-31 | 2017-12-08 | Cloud platform camera, cloud platform device and unmanned vehicles |
Family Applications After (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202110179237.0A Pending CN112804433A (en) | 2017-10-31 | 2017-12-08 | Cloud platform camera, cloud platform device and unmanned vehicles |
Country Status (2)
| Country | Link |
|---|---|
| CN (2) | CN207638745U (en) |
| WO (1) | WO2019085154A1 (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
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| CN110603504A (en) * | 2018-07-26 | 2019-12-20 | 深圳市大疆创新科技有限公司 | Multi-cradle-head control method and device, unmanned aerial vehicle, medium and electronic equipment |
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| CN103024281A (en) * | 2013-01-11 | 2013-04-03 | 重庆大学 | Infrared and visible video integration system |
| CN103269413A (en) * | 2013-05-13 | 2013-08-28 | 重庆大学 | Multi-source video fusion system |
| CN203722695U (en) * | 2013-12-10 | 2014-07-16 | 广州供电局有限公司 | Double-vision holder camera |
| CN105447838A (en) * | 2014-08-27 | 2016-03-30 | 北京计算机技术及应用研究所 | Method and system for infrared and low-level-light/visible-light fusion imaging |
| CN204515542U (en) * | 2015-03-27 | 2015-07-29 | 深圳市科卫泰实业发展有限公司 | A kind of fast-spliced twin-lens diaxon is from steady cradle head device |
| CN204979266U (en) * | 2015-07-16 | 2016-01-20 | 零度智控（北京）智能科技有限公司 | Cloud platform structure and cloud platform camera device with protective housing |
| CN205071156U (en) * | 2015-07-28 | 2016-03-02 | 杭州海康威视数字技术股份有限公司 | Two spectrum cameras |
| CN205221128U (en) * | 2015-10-28 | 2016-05-11 | 厦门汉航精密科技有限公司 | Unmanned aerial vehicle's tripod head structure |
| CN205345353U (en) * | 2016-01-26 | 2016-06-29 | 上海伯镭智能科技有限公司 | Parallelly connected cloud platform that carries on miniature thermal infrared imager and moving camera |
| CN108698705B (en) * | 2016-01-26 | 2022-02-18 | 深圳市大疆创新科技有限公司 | Stability augmentation platform and camera |
| CN205418138U (en) * | 2016-03-18 | 2016-08-03 | 江苏数字鹰科技发展有限公司 | Triaxial optoelectronic pod |
| CN205726140U (en) * | 2016-04-22 | 2016-11-23 | 优利科技有限公司 | The Cloud Terrace, the aircraft containing it and clouds terrace system |
| CN105872336A (en) * | 2016-05-24 | 2016-08-17 | 北京小米移动软件有限公司 | Camera |
| CN205707410U (en) * | 2016-06-14 | 2016-11-23 | 深圳极天创新科技有限公司 | Multi-cam unmanned plane |
| CN205872506U (en) * | 2016-08-04 | 2017-01-11 | 广州习疆电子科技有限公司 | Unmanned aerial vehicle's nacelle |
| CN106412439B (en) * | 2016-10-27 | 2020-01-07 | 北京小米移动软件有限公司 | Image acquisition equipment, image acquisition method and controller |
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| CN206561953U (en) * | 2017-02-21 | 2017-10-17 | 武汉星巡智能科技有限公司 | Head and the unmanned vehicle with the head |
| CN107124534B (en) * | 2017-03-29 | 2020-11-27 | 歌尔股份有限公司 | Three-axis holder, shooting equipment, shooting system and unmanned shooting system |
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- 2017-10-31 CN CN201721429153.3U patent/CN207638745U/en active Active
- 2017-12-08 WO PCT/CN2017/115277 patent/WO2019085154A1/en active Application Filing
- 2017-12-08 CN CN202110179237.0A patent/CN112804433A/en active Pending
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110603504A (en) * | 2018-07-26 | 2019-12-20 | 深圳市大疆创新科技有限公司 | Multi-cradle-head control method and device, unmanned aerial vehicle, medium and electronic equipment |
Also Published As
| Publication number | Publication date |
|---|---|
| CN112804433A (en) | 2021-05-14 |
| WO2019085154A1 (en) | 2019-05-09 |
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