WO2019061524A1 - 镜头座、使用该镜头座的摄像系统及摄像系统的安装方法 - Google Patents

镜头座、使用该镜头座的摄像系统及摄像系统的安装方法 Download PDF

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Publication number
WO2019061524A1
WO2019061524A1 PCT/CN2017/105094 CN2017105094W WO2019061524A1 WO 2019061524 A1 WO2019061524 A1 WO 2019061524A1 CN 2017105094 W CN2017105094 W CN 2017105094W WO 2019061524 A1 WO2019061524 A1 WO 2019061524A1
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WO
WIPO (PCT)
Prior art keywords
weight
lens
target
lens mount
loading structure
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PCT/CN2017/105094
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English (en)
French (fr)
Inventor
王平
王婷
黄永结
Original Assignee
深圳市大疆灵眸科技有限公司
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Filing date
Publication date
Application filed by 深圳市大疆灵眸科技有限公司 filed Critical 深圳市大疆灵眸科技有限公司
Priority to PCT/CN2017/105094 priority Critical patent/WO2019061524A1/zh
Priority to CN201780009150.0A priority patent/CN108702433A/zh
Publication of WO2019061524A1 publication Critical patent/WO2019061524A1/zh

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    • HELECTRICITY
    • H04ELECTRIC COMMUNICATION TECHNIQUE
    • H04NPICTORIAL COMMUNICATION, e.g. TELEVISION
    • H04N23/00Cameras or camera modules comprising electronic image sensors; Control thereof
    • H04N23/50Constructional details
    • H04N23/55Optical parts specially adapted for electronic image sensors; Mounting thereof
    • GPHYSICS
    • G03PHOTOGRAPHY; CINEMATOGRAPHY; ANALOGOUS TECHNIQUES USING WAVES OTHER THAN OPTICAL WAVES; ELECTROGRAPHY; HOLOGRAPHY
    • G03BAPPARATUS 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
    • G03B17/00Details of cameras or camera bodies; Accessories therefor
    • G03B17/02Bodies
    • G03B17/12Bodies with means for supporting objectives, supplementary lenses, filters, masks, or turrets
    • HELECTRICITY
    • H04ELECTRIC COMMUNICATION TECHNIQUE
    • H04NPICTORIAL COMMUNICATION, e.g. TELEVISION
    • H04N23/00Cameras or camera modules comprising electronic image sensors; Control thereof
    • H04N23/50Constructional details

Definitions

  • the present invention relates to the field of flight technology, and in particular, to a lens mount, an imaging system using the lens mount, and a mounting method of the camera system.
  • the camera system using the PTZ can shoot with the lens.
  • the existing pan/tilt may only correspond to a lens of one model.
  • it is often necessary to change the lens so that after the new lens is replaced in the camera system, the center of gravity of the entire pan/tilt may change due to the change in the weight of the lens, affecting the camera system. Imaging even life.
  • the present invention aims to at least solve one of the technical problems existing in the related art. To this end, the present invention needs to provide a lens mount, an image pickup system using the same, and a mounting method of the image pickup system.
  • a lens mount according to an embodiment of the present invention is used in a camera system including a plurality of lenses of different weights or models, the plurality of lenses including a target lens mounted on the lens mount, the lens mount including a body and a plurality of counterweights of different weights or models, the body being rotatable relative to the pan/tilt about a rotating shaft, the body comprising a lens loading structure on one side of the rotating shaft and a matching on the other side of the rotating shaft a reloading structure, the weight loading structure comprising a first connecting element, the plurality of weight back covers being respectively mateable with the weight loading structure, each of the weight back covers comprising a second connecting element a plurality of counterweight back covers including a target weight rear cover, the target weight rear cover being loadable to the weight loading structure by cooperation of the first connecting element and the second connecting element Up to adjust the equivalent center of gravity of the lens holder and the target lens.
  • the center of gravity of the lens holder and the target lens can be adjusted by using the cooperation of the target weight rear cover and the weight loading structure, so that the weight change caused by the replacement of the target lens does not cause the center of gravity of the entire pan/tilt to occur.
  • the change ensures the imaging and lifetime of the camera system after the replacement of the target lens.
  • the target weight back cover is assembled to the weight loading structure.
  • the center of gravity of the lens holder and the target lens can be adjusted by using the cooperation of the target weight back cover and the weight loading structure, so that the entire pan/tilt is not caused by the weight change caused by the replacement of the target lens.
  • the center of gravity changes, which in turn ensures the imaging and service life of the camera system after the target lens is replaced.
  • the camera system of the embodiment of the present invention includes a pan/tilt head, a lens mount according to any of the above embodiments, and a plurality of lenses of different weights or models, wherein the lens mount is disposed on the pan/tilt head through the rotating shaft,
  • the lenses include a target lens loaded on the lens loading structure.
  • the center of gravity of the lens holder and the target lens can be adjusted by using the cooperation of the target weight back cover and the weight loading structure, so that the center of gravity of the entire pan/tilt does not occur due to the weight change caused by the replacement of the target lens.
  • the change ensures the imaging and lifetime of the camera system after the replacement of the target lens.
  • FIG. 1 is a perspective view of a camera system according to an embodiment of the present invention.
  • FIG. 2 is a perspective view of a lens mount and a lens of an imaging system according to an embodiment of the present invention
  • FIG 3 is a schematic perspective view of a weight rear cover of a lens mount of an imaging system according to an embodiment of the present invention.
  • PTZ 20 first rotating shaft 201, second rotating shaft 202, third rotating shaft 203, frame 21, first connecting frame 211, second connecting frame 212, motor assembly 22, pitch axis motor 221, roll axis motor 222, translation A shaft motor 223, a lens 30, and a connection case 31.
  • first and second are used for descriptive purposes only and are not to be construed as indicating or implying a relative importance or implicitly indicating the number of technical features indicated.
  • features defining “first” or “second” may include one or more of the described features either explicitly or implicitly.
  • the meaning of "a plurality” is two or more unless specifically and specifically defined otherwise.
  • connection In the description of the present invention, it should be noted that the terms “installation”, “connected”, and “connected” are to be understood broadly, and may be fixed or detachable, for example, unless otherwise explicitly defined and defined. Connected, or connected in one piece. It can be a mechanical connection or an electrical connection. It can be directly connected or indirectly connected through an intermediate medium, which can be the internal communication of two elements or the interaction of two elements. For those skilled in the art, the specific meanings of the above terms in the present invention can be understood on a case-by-case basis.
  • the lens mount 10 of the embodiment of the present invention may be, but is not limited to, the camera system 100 used in the embodiment of the present invention.
  • the camera system 100 of embodiments of the present invention may be, but is not limited to, used in drones, such as for multi-wing unmanned aerial vehicles.
  • the embodiment of the present invention will be described by taking the lens mount 10 for the imaging system 100 as an example. In other embodiments, the drone may also be an unmanned vehicle or an unmanned boat.
  • the camera system 100 includes a lens mount 10, a pan/tilt head 20, and a plurality of lenses.
  • the weights or models of the plurality of lenses are different, and the plurality of lenses include the target lens 30 mounted on the lens mount 10.
  • the lens mount 10 is disposed on the pan/tilt head 20 via the first rotating shaft 201 so as to be rotatable relative to the pan/tilt head 20.
  • the lens mount 10 includes a body 11 and a plurality of counterweights of different weights or models.
  • the shape of the body 11 can be set according to specific conditions. In the embodiment of the present invention, the body 11 has a polyhedral column shape.
  • the body 11 is rotatable relative to the platform 20 about the first axis of rotation 201.
  • the body 11 includes a lens loading structure 111 on one side of the first rotating shaft 201 and a weight loading structure 112 on the other side of the first rotating shaft 201.
  • the target lens 30 is loaded on the lens loading structure 111.
  • the weight loading structure 112 includes a first connecting element 113.
  • a plurality of counterweight back covers can be mated with the weight loading structure 112, respectively.
  • Each counterweight back cover includes a second connecting element.
  • a plurality of counterweight back covers include a target weight rear cover 12. In the example shown in Figure 2, after the target weight The cover 12 includes a second connecting element 121.
  • the target weight rear cover 12 can be loaded onto the weight loading structure 112 by the cooperation of the first connecting member 113 and the second connecting member 121 to adjust the equivalent center of gravity of the lens mount 10 and the target lens 30.
  • the center of gravity of the lens holder 10 and the target lens 30 can be adjusted by the cooperation of the target weight rear cover 12 and the weight loading structure 112, so that the entire cloud is not caused by the weight change caused by the replacement of the target lens 30.
  • the center of gravity of the stage 20 changes, which in turn ensures the imaging and service life of the camera system 100 after the replacement of the target lens 30.
  • first connecting member 113 and the second connecting member 121 to load the counterweight rear cover 12 to the weight loading structure 112 is simple and easy to implement.
  • a plurality of lenses can be respectively mounted on the lens loading structure 111.
  • the target lens 30 refers to any one of a plurality of lenses mounted on the lens loading structure 111.
  • a plurality of counterweight back covers can be mated with the weight loading structure 112, respectively.
  • the target weight rear cover 12 refers to one of a plurality of counterweight back covers that are loaded on the weight loading structure 112 and that can cooperate with the weight loading structure 112 to adjust the equivalent center of gravity of the lens mount 10 and the target lens 30. cover.
  • the embodiment of the present invention will be described with the cooperation of the target weight rear cover 12 and the weight loading structure 112 and the cooperation of the target lens 30 and the lens loading structure 111.
  • the purpose of matching the lenses of different weights or models can be achieved by changing the weight or model of the back cover.
  • the models of the plurality of counterweight back covers may have different shapes of the plurality of counterweight back covers, and may also have different sizes of the plurality of counterweight back covers.
  • the weights of the plurality of counterweight back covers are different, and the weight of the target weight back cover 12 matches the weight or shape of the target lens 30.
  • the purpose of adjusting the equivalent center of gravity of the lens holder 10 and the lens 30 can be achieved by matching the weight of the target weight rear cover 12 with the weight or shape of the target lens 30, and making the target lens 30 not due to its own The quality is too large or the size is too long and tilting, which in turn makes the center of gravity of the entire camera system 100 stable.
  • the weight of the target weight rear cover 12 matches the weight of the target lens 30. It can be understood that when the weight of the target lens 30 is large, the weight of the target weight rear cover 12 matched thereto is also large. Thereby, the object of enabling the target lens 30 to be smoothly photographed is achieved.
  • the weight of the target weight rear cover 12 matches the shape of the target lens 30. It can be understood that the target weight 30 has a larger volume or size when the target lens 30 is larger or longer. In order to achieve the purpose of enabling the target lens 30 to smoothly shoot.
  • the models of the plurality of counterweight back covers are different, and the model of the target weight rear cover 12 matches the model of the target lens 30.
  • the model of the target weight rear cover 12 can be matched with the model of the target lens 30 to achieve the purpose of adjusting the equivalent center of gravity of the lens holder 10 and the target lens 30, and the target lens 30 is not excessively large due to its own quality. Or the size is too long and the tilt occurs, which in turn makes the center of gravity of the entire camera system 100 tend to stable.
  • the model of the target weight rear cover 12 matches the model of the target lens 30, and the shape of the target weight rear cover 12 matches the shape of the target lens 30, and may also be the target weight rear cover 12.
  • the size matches the size of the target lens 30. For example, when the size of the target lens 30 is long or large, the size or volume of the target weight rear cover 12 corresponding thereto is also large, so that the target lens 30 can be smoothly photographed.
  • the purpose of making the weights or models of the plurality of weight back covers different by making the materials of each of the two weight back covers different can also be achieved by making the shape of each of the two weight back covers different.
  • the weight of the back cover is different for the purpose of the weight or model.
  • the purpose of changing the weight or model of the weight back cover can be achieved by changing the material or shape of the weight back cover.
  • each counterweight back cover is substantially the same, and different weights of the weight back cover are obtained by using different materials.
  • the above materials may be one or more of different molecular weight plastic materials, copper materials, aluminum materials or zinc materials. It should be noted that the material used for the back cover and the preparation method of the weight back cover are not specifically limited.
  • the number of counterweight back covers can be the same as the number of lenses, and multiple weight back covers can be respectively The shots correspond to each other. That is to say, each lens has a target weight back cover that matches it.
  • the target weight can be adjusted when the rear weight 12 is engaged with the weight loading structure 112 by the target weight to adjust the equivalent center of gravity of the lens holder 10 and the target lens 30.
  • the rear cover 12 is configured to enable the equivalent center of gravity of the lens mount 10 and the target lens 30 to approach or substantially fall first when loaded onto the weight loading structure 112 by the cooperation of the first connecting element 113 and the second connecting element 121 On the shaft 201. Thereby, the target lens 30 and the lens mount 10 can be smoothly rotated with respect to the first rotating shaft 201.
  • the equivalent center of gravity of the lens holder 10 and the target lens 30 can fall within the On a rotating shaft 201, and the gravity line of action of the equivalent center of gravity of the lens holder 10 and the target lens 30 is coplanar with the center line of the first rotating shaft 201, that is, the equivalent center of gravity of the lens holder 10 and the target lens 30 substantially falls on the first rotating shaft.
  • the centerline of 201 thus, the lens mount 10 and the target lens 30 are more smoothly distributed with respect to the entire first shaft 201.
  • the weight of the target weight rear cover 12 is matched with the weight of the target lens 30, and the cover 12 is loaded to the weight by the cooperation of the first connecting member 113 and the second connecting member 121 at the target weight.
  • the equivalent center of gravity of the lens mount 10 and the target lens 30 can fall on the first rotating shaft 201, so that the target lens 30 and the lens mount 10 can be smoothly rotated with respect to the first rotating shaft 201.
  • the target lens 30 And the lens mount 10 is less prone to sway, thereby ensuring the quality of the target lens 30.
  • the first rotating shaft 201 is represented by a broken line in the embodiment of the present invention.
  • the second rotating shaft 202 and the third rotating shaft 203 in the following are also indicated by broken lines.
  • the manner in which the target lens 30 is loaded by the lens loading structure 111 can be set according to specific conditions.
  • the target lens 30 may be mounted to the lens loading structure 111 by a detachable connection (for example, a screw connection or a snap connection), or may be attached to the lens loading structure 111 by a fixed connection.
  • the lens loading structure 111 is formed with a first cylindrical receiving groove (not shown).
  • the first receiving groove is formed with an internal thread (not shown).
  • the target lens 30 includes a substantially cylindrical connecting case 31 formed with an external thread (not shown) that can be engaged with the internal thread of the first receiving groove.
  • the target lens 30 is at least partially screwed into the first receiving groove through the connecting case 31 to be loaded on the lens loading structure 111.
  • the manner in which the lens loading structure 111 and the weight loading structure 112 are formed may be set according to specific conditions.
  • one end of the body 11 is formed with a lens loading structure 111
  • the other end of the body 11 is formed with a weight loading structure 112.
  • the target lens 30 is located at one end of the body 11 and away from the weight loading structure 112, so that the lens holder 10 and the target lens 30 can be integrated by the cooperation of the smaller mass weight loading structure 112 and the weight rear cover 12.
  • the redistribution of the center of gravity reduces the quality of the entire camera system 100 and facilitates miniaturization of the camera system 100.
  • the body 11 includes a side surface 110, and the opposite ends of the side surface 110 are respectively formed with a rotating shaft hole 1101.
  • the shaft hole 1101 substantially overlaps the first shaft 201.
  • the shaft hole 1101 is for engaging with the first rotating shaft 201. As such, the body 11 can be rotated more stably about the first rotating shaft 201 relative to the platform 20 .
  • the weight loading structure 112 is formed with a second receiving groove 114 that cooperates with the target weight rear cover 12.
  • the target weight rear cover 12 includes a connection surface 122 that is coupled to the bottom surface 1141 of the second receiving groove 114.
  • the first connecting element 113 is disposed on the bottom surface 1141 of the second receiving groove 114.
  • the second connecting element 121 is disposed on the connecting surface 122 corresponding to the first connecting element 113. As such, the target counterweight back cover 12 is more closely mated with the weight loading structure 112.
  • the manner of setting the first connecting element 113 may be set according to a specific situation, and the setting manner of the second connecting element 121 may be set according to a specific situation.
  • the stability of the cooperation of the target weight rear cover 12 with the weight loading structure 112 can be improved by providing a plurality of first connecting elements 113 and a plurality of second connecting elements 121 corresponding to the number of first connecting elements 113.
  • the bottom surface 1141 of the second receiving groove 114 has a rectangular shape
  • the first connecting member 113 includes four corners respectively disposed at the bottom surface 1141 of the second receiving groove 114. drop.
  • the second connecting element 121 comprises four and corresponds to the position of the four first connecting elements 113, respectively.
  • the weight loading structure 112 may include the first positioning structure 115 formed on the bottom surface 1141 of the second receiving groove 114, and may
  • the target weight rear cover 12 includes a second positioning structure (not shown) formed on the connecting surface 122.
  • the target weight rear cover 12 is coupled to the weight loading structure 112 by the first positioning structure 115 and the second positioning structure. That is, when the target weight rear cover 12 needs to be loaded on the weight loading structure 112, the second positioning structure may be first aligned with the first positioning structure 115, and then the second positioning structure and the first positioning structure 115 are made. The mating is positioned such that the target weight rear cover 12 is loaded onto the weight loading structure 112.
  • the manner of cooperation of the first connecting element 113 and the second connecting element 121 can be set according to specific conditions.
  • the first connecting element 113 and the second connecting element 121 can be connected by means of a snap-fit connection, or can be realized by a bonding connection by an adhesive.
  • the first connecting element 113 may be, but not limited to, a magnetic element
  • the second connecting element 121 may be, but not limited to, a magnetic element such as a magnet.
  • the first connecting element 113 and the second connecting element 121 are both magnetic elements, and the target weight rear cover 12 is loaded to the weight loading structure by the magnetic cooperation of the first connecting element 113 and the second connecting element 121.
  • 112 is used to adjust the center of gravity of the lens 30. In this way, the stability of the first connecting element 113 and the second connecting element 121 after mating with each other is better, and the quick disassembly and assembly of the target weight rear cover 12 can be realized, which is convenient and quick.
  • the bottom of the weight loading structure 112 is made of a magnetic material
  • the bottom of the target weight rear cover 12 is magnetically permeable.
  • the bottom of the target weight rear cover 12 can be matched with the bottom of the weight loading structure 112 to achieve the weight of the balance lens 30. Good results.
  • the weight loading structure 112 is formed with a first closure 116 surrounding the first connecting element 113.
  • the target weight rear cover 12 is formed with a second closing portion 123 that surrounds the second connecting member 121 and corresponds to the first closing portion 116.
  • the first closing portion 116 is in contact with the second closing portion 123 to close the magnetic forces of the first connecting member 113 and the second connecting member 121. In this way, the first connecting element 113 and the second connecting element 121 can be combined to form a magnetically closed environment for the mating target weight rear cover 12 and the weight loading structure 112, thereby avoiding affecting the normal use of the compass.
  • the magnetic force of the second connecting member 121 can be made by making the first closing portion 116 be made of a magnetic material, and by making the second closing portion 123 made of a magnetic material, so that the target weight rear cover 12 is matched with The closed effect of the magnetically enclosed environment formed by the reloading structure 112 is better.
  • the above-mentioned magnetic material may be an iron material or a boron material.
  • first connecting member 113 may be set according to a specific situation
  • shape of the second connecting member 121 may be set according to a specific situation.
  • first connecting element 113 is substantially cylindrical
  • second connecting element 121 is substantially cylindrical.
  • a method of mounting an imaging system according to an embodiment of the present invention is applied to the above-described imaging system 100.
  • the installation method of the camera system includes the following steps:
  • the plurality of lenses including a target lens 30;
  • the above-described target weight rear cover 12 is assembled to the weight loading structure 112.
  • the center of gravity of the lens mount 10 and the target lens 30 can be adjusted by the cooperation of the target weight rear cover 12 and the weight loading structure 112, so that the weight change caused by the replacement of the target lens 30 does not cause the entire pan/tilt head 20
  • the center of gravity changes which in turn ensures the imaging and service life of the camera system 100 after the replacement of the target lens 30.
  • a plurality of lenses can be respectively mounted on the lens loading structure 111.
  • the target lens 30 refers to any one of a plurality of lenses mounted on the lens loading structure 111.
  • the target weight rear cover 12 corresponds to the weight or model of the target lens 30
  • the equivalent center of gravity of the lens mount 10 and the target lens 30 can be close to or substantially fall on the first rotating shaft 201, so that the center of gravity of the camera system 100 tends to balance.
  • the equivalent center of gravity of the lens mount 10 and the target lens 30 can fall on the first rotating shaft 201 and the lens mount 10 and the target lens 30
  • the gravitational action line of the equivalent center of gravity can be coplanar with the center line of the first rotating shaft 201, that is, the equivalent center of gravity of the lens mount 10 and the target lens 30 can substantially fall on the center line of the first rotating shaft 201.
  • each of the two weight rear covers 12 may be different for each of the two weight rear covers 12, or may be different for each of the two weight rear covers 12.
  • the corresponding target weight rear cover 12 can be selected in the following manner, and the weighted lens 30 can be compared with the weight of the plurality of weight rear cover 12
  • the large counterweight cover 12 or the larger weight rear cover 12 is matched, and the longer-sized lens 30 can also be combined with the weighted rear cover 12 of the plurality of counterweights 12 to have a larger size.
  • Counterweight back cover 12 to match.
  • the platform 20 includes a frame 21 and a motor assembly 22 fixed to the frame 21 and capable of driving the frame 21 to rotate.
  • the lens mount 10 can be disposed within the frame 21 through the first rotating shaft 201. That is, the lens mount 10 is rotatable relative to the frame 21, and the frame 21 can support and protect the lens mount 10.
  • the platform 20 can be, but is not limited to, a three-axis pan/tilt.
  • the pan/tilt head 20 is a three-axis pan/tilt head, that is, includes a first rotating shaft 201 (pitch axis, that is, a Pitch axis), a second rotating shaft 202 (rolling axis, that is, a Roll axis), and a third rotating shaft. 203 (translation axis, ie YAW axis).
  • the frame 21 includes a first connecting frame 211 and a second connecting frame 212.
  • the lens mount 10 is rotatably disposed in the first connecting frame 211 through the first rotating shaft 201.
  • the first connecting frame 211 is rotatably connected to the second connecting frame 212 through the second rotating shaft 202.
  • the motor assembly 22 includes three motors, respectively, a pitch axis (Pitch axis) motor 221 that controls the lens holder 10 and the lens 30 to pitch about the first rotating shaft 201, and controls the lens holder 10 and the lens 30 to roll around the second rotating shaft 202.
  • the first feature "on” or “under” the second feature may include direct contact of the first and second features, and may also include first and second features, unless otherwise specifically defined and defined. It is not in direct contact but through additional features between them.
  • the first feature "above”, “above” and “above” the second feature includes the first feature directly above and above the second feature, or merely indicating that the first feature level is higher than the second feature.
  • the first feature “below”, “below” and “below” the second feature includes the first feature directly below and below the second feature, or merely the first feature level being less than the second feature.

Abstract

一种镜头座(10)、使用镜头座(10)的摄像系统(100)及摄像系统(100)的安装方法。摄像系统(100)包括多个不同重量或型号的镜头,多个镜头包括装载于镜头座(10)上的目标镜头(30),镜头座(10)包括本体(11)和多个不同重量或型号的配重后盖,本体(11)能够绕转轴(201)相对于云台(20)转动,本体(11)包括位于转轴(201)一侧的镜头装载结构(111)和位于转轴(201)另一侧的配重装载结构(112),配重装载结构(112)包括第一连接元件(113),多个配重后盖能够分别与配重装载结构(112)配合,每个配重后盖均包括一个第二连接元件(121),多个配重后盖中包括一个目标配重后盖(12),目标配重后盖(12)能够通过第一连接元件(113)和第二连接元件(121)的配合装载到配重装载结构(112)上以调整镜头座(10)和目标镜头(30)的等效重心。

Description

镜头座、使用该镜头座的摄像系统及摄像系统的安装方法 技术领域
本发明涉及飞行技术领域,尤其涉及一种镜头座、使用该镜头座的摄像系统以及摄像系统的安装方法。
背景技术
使用云台的摄像系统可通过镜头进行拍摄。然而,现有的云台可能只对应适应一款型号的镜头。然而在需要通过摄像系统进行不同的拍摄要求时,常常需要更换镜头,这样在摄像系统中更换新的镜头后,可能会由于镜头的重量变化而导致整个云台的重心发生变化,影响摄像系统的成像甚至使用寿命。
发明内容
本发明旨在至少解决相关技术中存在的技术问题之一。为此,本发明需要提供一种镜头座、使用该镜头座的摄像系统及摄像系统的安装方法。
本发明实施方式的镜头座用于摄像系统,所述摄像系统包括不同重量或型号的多个镜头,所述多个镜头包括装载于所述镜头座上的目标镜头,所述镜头座包括本体和多个不同重量或型号的配重后盖,所述本体能够绕转轴相对于所述云台转动,所述本体包括位于所述转轴一侧的镜头装载结构和位于所述转轴另一侧的配重装载结构,所述配重装载结构包括第一连接元件,所述多个配重后盖能够分别与所述配重装载结构配合,每个所述配重后盖均包括一个第二连接元件,所述多个配重后盖中包括一个目标配重后盖,所述目标配重后盖能够通过所述第一连接元件和所述第二连接元件的配合装载到所述配重装载结构上以调整所述镜头座和所述目标镜头的等效重心。
上述镜头座中,可利用目标配重后盖和配重装载结构的配合来调整镜头座和目标镜头整体的重心,这样不会由于目标镜头的更换而产生的重量变化导致整个云台的重心发生变化,继而能够保证更换目标镜头后的摄像系统的成像及使用寿命。
本发明实施方式的摄像系统的安装方法,包括以下步骤:
提供上述任一实施方式所述的镜头座和多个不同重量或型号的镜头,多个所述镜头中包括一个所述目标镜头;
将所述目标镜头安装到所述镜头装载结构上;
根据所述目标镜头的重量或型号选择对应的所述目标配重后盖;
将所述目标配重后盖装配到所述配重装载结构上。
上述摄像系统的安装方法中,可利用目标配重后盖和配重装载结构的配合来调整镜头座和目标镜头整体的重心,这样不会由于目标镜头的更换而产生的重量变化导致整个云台的重心发生变化,继而能够保证更换目标镜头后的摄像系统的成像及使用寿命。
本发明实施方式的摄像系统包括云台、上述任一实施方式所述的镜头座和多个不同重量或型号的镜头,所述镜头座通过所述转轴设置在所述云台上,所述多个镜头包括装载在所述镜头装载结构上的目标镜头。
上述摄像系统中,可利用目标配重后盖和配重装载结构的配合来调整镜头座和目标镜头整体的重心,这样不会由于目标镜头的更换而产生的重量变化导致整个云台的重心发生变化,继而能够保证更换目标镜头后的摄像系统的成像及使用寿命。。
本发明实施方式的附加方面和优点将在下面的描述中部分给出,部分将从下面的描述中变得明显,或通过本发明的实践了解到。
附图说明
本发明的上述和/或附加的方面和优点从结合下面附图对实施方式的描述中将变得明显和容易理解,其中:
图1是本发明实施方式的摄像系统的立体示意图;
图2是本发明实施方式的摄像系统的镜头座和镜头的立体示意图;
图3是本发明实施方式的摄像系统的镜头座的配重后盖的立体示意图。
主要元件符号说明:
摄像系统100;
镜头座10、本体11、侧表面110、转轴孔1101、镜头装载结构111、配重装载结构112、第一连接元件113、第二收容槽114、底面1141、第一定位结构115、第一封闭部116、配重后盖12、第二连接元件121、连接面122、第二封闭部123;
云台20、第一转轴201、第二转轴202、第三转轴203、框架21、第一连接架211、第二连接架212、电机组件22、俯仰轴电机221、横滚轴电机222、平移轴电机223、镜头30、连接壳31。
具体实施方式
下面详细描述本发明的实施方式,所述实施方式的示例在附图中示出,其中自始至终相同或类似的标号表示相同或类似的元件或具有相同或类似功能的元件。下面通过参考附图描述的实施方式是示例性的,仅用于解释本发明,而不能理解为对本发明的限制。
在本发明的描述中,需要理解的是,术语“中心”、“纵向”、“横向”、“长度”、“宽度”、“厚度”、“上”、“下”、“前”、“后”、“左”、“右”、“竖直”、“水平”、“顶”、“底”、“内”、“外”、“顺时针”、“逆时针”等指示的方位或位置关系为基于附图所示的方位或位置关系,仅是为了便于描述本发明和简化描述,而不是指示或暗示所指的装置或元件必须具有特定的方位、以特定的方位构造和操作,因此不能理解为对本发明的限制。此外,术语“第一”、“第二”仅用于描述目的,而不能理解为指示或暗示相对重要性或者隐含指明所指示的技术特征的数量。由此,限定有“第一”、“第二”的特征可以明示或者隐含地包括一个或者更多个所述特征。在本发明的描述中,“多个”的含义是两个或两个以上,除非另有明确具体的限定。
在本发明的描述中,需要说明的是,除非另有明确的规定和限定,术语“安装”、“相连”、“连接”应做广义理解,例如,可以是固定连接,也可以是可拆卸连接,或一体地连接。可以是机械连接,也可以是电连接。可以是直接相连,也可以通过中间媒介间接相连,可以是两个元件内部的连通或两个元件的相互作用关系。对于本领域的普通技术人员而言,可以根据具体情况理解上述术语在本发明中的具体含义。
请一并参阅图1至图3,本发明实施方式的镜头座10可以但不限于用于本发明实施方式的摄像系统100。本发明实施方式的摄像系统100可以但不限于用于无人机,例如用于多翼无人飞行器。本发明实施方式以镜头座10用于摄像系统100为例进行说明。在其他实施例中,所述无人机也可以是无人车或无人船。
在本发明实施方式中,摄像系统100包括镜头座10、云台20和多个镜头。其中,多个镜头的重量或型号不同,多个镜头中包括装载于镜头座10上的目标镜头30。镜头座10可通过第一转轴201设置在云台20上,从而可相对于云台20转动。
请结合图2,镜头座10包括本体11和多个不同重量或型号的配重后盖。其中,本体11的形状可根据具体情况进行设置。在本发明实施方式中,本体11呈多面体柱状。本体11能够绕第一转轴201相对于云台20转动。本体11包括位于第一转轴201一侧的镜头装载结构111和位于第一转轴201另一侧的配重装载结构112。目标镜头30装载于镜头装载结构111上。配重装载结构112包括第一连接元件113。
多个配重后盖能够分别与配重装载结构112配合。每个配重后盖均包括一个第二连接元件。多个配重后盖中包括一个目标配重后盖12。在图2所示的例子中,目标配重后 盖12包括第二连接元件121。目标配重后盖12能够通过第一连接元件113和第二连接元件121的配合装载到配重装载结构112上以调整镜头座10和目标镜头30的等效重心。
也就是说,可利用目标配重后盖12和配重装载结构112的配合来调整镜头座10和目标镜头30整体的重心,这样不会由于目标镜头30的更换而产生的重量变化导致整个云台20的重心发生变化,继而能够保证更换目标镜头30后的摄像系统100的成像及使用寿命。
另外,通过第一连接元件113和第二连接元件121的配合以使得配重后盖12装载到配重装载结构112的设置方式操作简单,易于实现。
需要说明的是,多个镜头能够分别装载于镜头装载结构111上。目标镜头30指代装载于镜头装载结构111上的多个镜头中的任意一个镜头。多个配重后盖能够分别与配重装载结构112配合。目标配重后盖12指代装载于配重装载结构112并能够与配重装载结构112配合以调整镜头座10和目标镜头30的等效重心的多个配重后盖中的一个配重后盖。本发明实施方式以目标配重后盖12与配重装载结构112的配合以及目标镜头30与镜头装载结构111的配合进行说明。
再有,由于多个配重后盖的重量或型号不同,这样可通过变更配重后盖的重量或型号而达到匹配不同重量或型号的镜头的目的。其中,多个配重后盖的型号不同可以为多个配重后盖的形状不同,也可以为多个配重后盖的尺寸不同。
例如,在一些实施例中,多个配重后盖的重量不同,目标配重后盖12的重量与目标镜头30的重量或形状相匹配。如此,可通过使得目标配重后盖12的重量与目标镜头30的重量或形状相匹配以达到调整镜头座10和镜头30的等效重心的目的,并使得使目标镜头30不会由于自身的质量过大或尺寸过长而发生倾斜,继而使整个摄像系统100的重心能够趋于稳定。
需要说明的是,目标配重后盖12的重量与目标镜头30的重量相匹配可以理解为在目标镜头30的重量较大时,与之匹配的目标配重后盖12的重量也较大,从而达到能够使得目标镜头30平稳进行拍摄的目的。目标配重后盖12的重量与目标镜头30的形状相匹配可以理解为在目标镜头30的体积较大或尺寸较长时,与之匹配的目标配重后盖12的体积或尺寸也较大,从而达到能够使得目标镜头30平稳进行拍摄的目的。
又如,其他实施例中,多个配重后盖的型号不同,目标配重后盖12的型号与目标镜头30的型号相匹配。如此,可通过目标配重后盖12的型号与目标镜头30的型号相匹配以达到调整镜头座10和目标镜头30的等效重心的目的,并使得目标镜头30不会由于自身的质量过大或尺寸过长而发生倾斜,继而使整个摄像系统100的重心能够趋于 稳定。
需要说明的是,目标配重后盖12的型号与目标镜头30的型号相匹配可以为目标配重后盖12的形状与目标镜头30的形状相匹配,也可以为目标配重后盖12的尺寸与目标镜头30的尺寸相匹配。例如,当目标镜头30的尺寸较长或体积较大时,与其对应匹配的目标配重后盖12的尺寸或体积也较大,从而达到能够使得目标镜头30平稳进行拍摄的目的。
另外,可通过使得每两个配重后盖的材料不同而达到使得多个配重后盖的重量或型号不同的目的,也可通过使得每两个配重后盖的形状不同而达到使得多个配重后盖的重量或型号不同的目的。如此,可通过改变配重后盖的材料或形状以达到改变配重后盖的重量或型号的目的。
例如,在一些例子中,每个配重后盖的形状基本相同,通过采用不同材料得到不同重量的配重后盖。上述材料可以为不同分子量的塑料材料、铜材料、铝材料或锌材料中的一种或多种。需要说明的是,配重后盖所采用的材料及配重后盖的制备方式没有具体限制。
可以理解,为了能够更好的匹配多个镜头,以满足用户使用不同镜头进行拍摄的需求,可使得配重后盖的数目与镜头的数目相同,并且使得多个配重后盖能够分别与多个镜头对应匹配。也就是说,每个镜头均具有与之对应匹配的目标配重后盖。
可以理解,为了使得目标镜头30能够更平稳地进行拍摄,在通过目标配重后盖12与配重装载结构112配合以调整镜头座10和目标镜头30的等效重心时,可将目标配重后盖12配置成在通过第一连接元件113和第二连接元件121的配合装载到配重装载结构112上时能够使得镜头座10及目标镜头30的等效重心能够靠近或基本落在第一转轴201上。从而使得目标镜头30及镜头座10能够相对于第一转轴201平稳地转动。较佳地,在目标配重后盖12通过第一连接元件113和第二连接元件121的配合装载到配重装载结构112上时,镜头座10及目标镜头30的等效重心能够落在第一转轴201上,并且镜头座10和目标镜头30的等效重心的重力作用线与第一转轴201的中心线共面,即镜头座10和目标镜头30的等效重心基本落在第一转轴201的中心线上。这样镜头座10和目标镜头30相对于第一转轴201整体分布更加平稳。在本发明实施方式中,目标配重后盖12的重量与目标镜头30的重量相匹配,并且在目标配重后盖12通过第一连接元件113和第二连接元件121的配合装载到配重装载结构112上时,镜头座10及目标镜头30的等效重心能够落在第一转轴201上,从而使得目标镜头30及镜头座10能够相对于第一转轴201平稳地转动。这样在使用摄像系统100进行拍摄时,目标镜头30 及镜头座10不容易产生晃动,从而可保证目标镜头30拍摄质量。
还有,为了从整体上体现镜头座10的安装位置,本发明实施方式中以虚线代表第一转轴201。在下述中的第二转轴202及第三转轴203也均以虚线表示。
进一步地,通过镜头装载结构111装载目标镜头30的方式可根据具体情况进行设置。目标镜头30可以通过可拆卸的连接方式(例如螺纹连接或卡合连接)安装于镜头装载结构111,也可以通过固定的连接方式安装于镜头装载结构111。在本发明实施方式中,镜头装载结构111形成有基本呈圆柱体状的第一收容槽(图未示出)。第一收容槽形成有内螺纹(图未示出)。目标镜头30包括基本呈圆柱体状的连接壳31,连接壳31形成有能够与第一收容槽的内螺纹配合的外螺纹(图未示出)。目标镜头30通过连接壳31至少部分地旋入第一收容槽内以装载于镜头装载结构111上。
进一步地,镜头装载结构111与配重装载结构112的形成方式可根据具体情况进行设置。在本发明实施方式中,本体11的一端形成有镜头装载结构111,本体11的另一端形成有配重装载结构112。如此,目标镜头30为位于本体11的一端并远离配重装载结构112,这样可通过较小质量的配重装载结构112与配重后盖12的配合而实现镜头座10和目标镜头30整体的重心的重新分布,从而降低了整个摄像系统100的质量,便于摄像系统100的小型化。
进一步地,本体11通过第一转轴201设置于云台20的方式可根据具体情况进行设置。在本发明实施方式中,本体11包括有侧表面110,侧表面110相背两端分别形成有转轴孔1101。转轴孔1101与第一转轴201基本重叠。转轴孔1101用于与第一转轴201配合。如此,本体11能够更稳定地绕第一转轴201相对于云台20转动。
进一步地,目标配重后盖12与配重装载结构112的配合方式可根据具体情况进行设置。在本发明实施方式中,配重装载结构112形成有与目标配重后盖12配合的第二收容槽114。目标配重后盖12包括与第二收容槽114的底面1141连接的连接面122。第一连接元件113设置在第二收容槽114的底面1141上。第二连接元件121对应第一连接元件113设置在连接面122上。如此,目标配重后盖12与配重装载结构112的配合更加紧密。
进一步地,第一连接元件113的设置方式可根据具体情况进行设置,第二连接元件121的设置方式可根据具体情况进行设置。例如,可通过设置多个第一连接元件113及与第一连接元件113数目对应的多个第二连接元件121来提高目标配重后盖12与配重装载结构112的配合的稳定性。在本发明实施方式中,第二收容槽114的底面1141呈矩形,第一连接元件113包括四个并分别设置在第二收容槽114的底面1141的四个角 落。第二连接元件121包括四个并分别与四个第一连接元件113的位置对应。
进一步地,为了提高目标配重后盖12与配重装载结构112配合装载精确度,可使得配重装载结构112包括形成于第二收容槽114的底面1141的第一定位结构115,并可使得目标配重后盖12包括形成于连接面122上的第二定位结构(图未示出)。目标配重后盖12通过第一定位结构115和第二定位结构配合定位到配重装载结构112上。也就是说,在需要将目标配重后盖12装载于配重装载结构112上时,可先使得第二定位结构对准第一定位结构115,然后使得第二定位结构与第一定位结构115配合定位以使得目标配重后盖12装载于配重装载结构112上。
其次,第一连接元件113与第二连接元件121的配合方式可根据具体情况进行设置。第一连接元件113与第二连接元件121可以通过卡合的连接方式实现配合连接,也可以通过粘结剂以粘结的连接方式实现配合连接。另外,第一连接元件113可以但不限于为磁性元件,第二连接元件121可以但不限于为磁性元件,磁性元件例如为磁铁。在本发明实施方式中,第一连接元件113和第二连接元件121均为磁性元件,目标配重后盖12通过第一连接元件113和第二连接元件121的磁力配合装载到配重装载结构112上以调整镜头30的重心。如此,第一连接元件113和第二连接元件121相互配合后的稳定性较佳,并且能够实现目标配重后盖12的快速拆装,方便快捷。
更进一步地,在第一连接元件113和第二连接元件121均采用磁性元件时,若使配重装载结构112的底部采用通磁材料构成,并使目标配重后盖12的底部采用通磁材料构成,则在将第一连接元件113和第二连接元件121对应配合时,目标配重后盖12的底部与配重装载结构112的底部对应配合后能够在平衡镜头30的重量方面达到较佳的效果。
更进一步地,当摄像系统100包括有用于辨识方向的指南针(图未示出),尤其是在指南针安装于云台20上时,若第一连接元件113和第二连接元件121均采用磁性元件,则需要避免第一连接元件113和第二连接元件121形成的磁场影响指南针的正常使用。在本发明实施方式中,配重装载结构112形成有围绕第一连接元件113的第一封闭部116。目标配重后盖12形成有围绕第二连接元件121并与第一封闭部116对应的第二封闭部123。第一封闭部116与第二封闭部123贴合以封闭第一连接元件113和第二连接元件121的磁力。如此,第一连接元件113和第二连接元件121配合吸合后能够使得配合的目标配重后盖12与配重装载结构112形成磁封闭环境,从而可避免影响指南针的正常使用。
更进一步地,若设计第一封闭部116与第二封闭部123贴合以封闭第一连接元件113 和第二连接元件121的磁力,则可通过使得第一封闭部116采用通磁材料制成,并通过使得第二封闭部123采用通磁材料制成,从而使目标配重后盖12与配重装载结构112配合形成的磁封闭环境的封闭效果更佳。需要说明的是,上述通磁材料可为铁材料或硼材料等。
另外,第一连接元件113的形状可根据具体情况进行设置,第二连接元件121的形状可根据具体情况进行设置。在本发明实施方式中,第一连接元件113基本呈圆柱体状,第二连接元件121基本呈圆柱体状。
请结合图2和图3,本发明实施方式的摄像系统的安装方法,用于上述的摄像系统100。具体地,摄像系统的安装方法包括以下步骤:
提供上述的镜头座10和多个不同重量或型号的镜头,多个镜头包括一个目标镜头30;
将目标镜头30安装到镜头装载结构111上;
根据目标镜头30的重量或型号选择对应的目标配重后盖12;
将上述目标配重后盖12装配到配重装载结构112上。
如此,可利用目标配重后盖12和配重装载结构112的配合来调整镜头座10和目标镜头30整体的重心,这样不会由于目标镜头30的更换而产生的重量变化导致整个云台20的重心发生变化,继而能够保证更换目标镜头30后的摄像系统100的成像及使用寿命。
需要说明的是,多个镜头能够分别装载于镜头装载结构111上。目标镜头30指代装载于镜头装载结构111上的多个镜头中的任意一个镜头。在目标配重后盖12与目标镜头30的重量或型号对应时,镜头座10和目标镜头30的等效重心能够靠近或基本落在第一转轴201上,从而使得摄像系统100的重心趋于平衡。较佳地,在目标配重后盖12与目标镜头30的重量或型号对应时,镜头座10和目标镜头30的等效重心能够落在第一转轴201上并且镜头座10和目标镜头30的等效重心的重力作用线能够与第一转轴201的中心线共面,即镜头座10和目标镜头30的等效重心能够基本落在第一转轴201的中心线上。
另外,每两个的配重后盖12的型号不同可以为每两个的配重后盖12的形状不同,也可以为每两个的配重后盖12的尺寸不同。在根据镜头30的重量或型号选择目标配重后盖12之时,可按照以下方式选择对应的目标配重后盖12,重量较大的镜头30可与多个配重后盖12中重量较大的配重后盖12或尺寸较大的配重后盖12进行匹配,尺寸较长的镜头30也可与多个配重后盖12中重量较大的配重后盖12或尺寸较大的配重后盖 12进行匹配。
进一步地,在本发明实施方式的摄像系统100中,云台20包括框架21和固定于框架21上并能够驱动框架21转动的电机组件22。并且,镜头座10可通过第一转轴201设置在框架21内。也就是说,镜头座10可相对于框架21转动,而框架21能够对镜头座10起到支撑及保护的作用。
可以理解,云台20可以但不限于是三轴云台。在图1所示的例子中,云台20为三轴云台,即包括第一转轴201(俯仰轴,即Pitch轴)、第二转轴202(横滚轴,即Roll轴)及第三转轴203(平移轴,即YAW轴)。框架21包括第一连接架211和第二连接架212。镜头座10为通过第一转轴201可转动地设置在第一连接架211内。第一连接架211通过第二转轴202可转动连接第二连接架212。电机组件22包括三个电机,分别为控制镜头座10及镜头30绕第一转轴201俯仰运动的俯仰轴(Pitch轴)电机221、控制镜头座10及镜头30绕第二转轴202横滚运动的横滚轴(Roll轴)电机222以及控制镜头座10及镜头30绕第三转轴203平移运动的平移轴(YAW轴)电机223。
在本发明中,除非另有明确的规定和限定,第一特征在第二特征之“上”或之“下”可以包括第一和第二特征直接接触,也可以包括第一和第二特征不是直接接触而是通过它们之间的另外的特征接触。而且,第一特征在第二特征“之上”、“上方”和“上面”包括第一特征在第二特征正上方和斜上方,或仅仅表示第一特征水平高度高于第二特征。第一特征在第二特征“之下”、“下方”和“下面”包括第一特征在第二特征正下方和斜下方,或仅仅表示第一特征水平高度小于第二特征。
下文的公开提供了许多不同的实施方式或例子用来实现本发明的不同结构。为了简化本发明的公开,下文中对特定例子的部件和设置进行描述。当然,它们仅仅为示例,并且目的不在于限制本发明。此外,本发明可以在不同例子中重复参考数字和/或参考字母,这种重复是为了简化和清楚的目的,其本身不指示所讨论各种实施方式和/或设置之间的关系。此外,本发明提供了的各种特定的工艺和材料的例子,但是本领域普通技术人员可以意识到其他工艺的应用和/或其他材料的使用。
在本说明书的描述中,参考术语“一个实施方式”、“一些实施方式”、“示意性实施方式”、“示例”、“具体示例”、或“一些示例”等的描述意指结合实施方式或示例描述的具体特征、结构、材料或者特点包含于本发明的至少一个实施方式或示例中。在本说明书中,对上述术语的示意性表述不一定指的是相同的实施方式或示例。而且,描述的具体特征、结构、材料或者特点可以在任何的一个或多个实施方式或示例中以合适的方式结合。
尽管已经示出和描述了本发明的实施方式,本领域的普通技术人员可以理解:在不 脱离本发明的原理和宗旨的情况下可以对这些实施方式进行多种变化、修改、替换和变型,本发明的范围由权利要求及其等同物限定。

Claims (17)

  1. 一种镜头座,用于摄像系统,所述摄像系统包括多个不同型号或重量的镜头,所述多个镜头包括装载于所述镜头座上的目标镜头,所述镜头座包括:
    能够绕转轴相对于所述云台转动的本体,所述本体包括位于所述转轴一侧的镜头装载结构和位于所述转轴另一侧的配重装载结构,所述配重装载结构包括第一连接元件;和
    能够分别与所述配重装载结构配合的多个不同重量或型号的配重后盖,每个所述配重后盖均包括一个第二连接元件,所述多个配重后盖中包括一个目标配重后盖,所述目标配重后盖能够通过所述第一连接元件和所述第二连接元件的配合装载到所述配重装载结构上以调整所述镜头座和所述目标镜头的等效重心。
  2. 如权利要求1所述的镜头座,其特征在于,所述镜头座和所述目标镜头的等效重心基本落在所述转轴上。
  3. 如权利要求1所述的镜头座,其特征在于,所述多个配重后盖的重量不同,所述目标配重后盖的重量与所述目标镜头的重量或形状相匹配。
  4. 如权利要求1所述的镜头座,其特征在于,所述多个配重后盖的型号不同,所述目标配重后盖的型号与所述目标镜头的型号相匹配。
  5. 如权利要求4所述的镜头座,其特征在于,所述目标配重后盖的形状与所述目标镜头的形状相匹配。
  6. 如权利要求1所述的镜头座,其特征在于,每两个所述配重后盖的材料不同,或者每两个所述配重后盖的形状不同。
  7. 如权利要求1所述的镜头座,其特征在于,所述本体呈多面体柱状,所述本体的一端形成有所述镜头装载结构,所述本体的另一端形成有所述配重装载结构。
  8. 如权利要求1所述的镜头座,其特征在于,所述本体呈多面体柱状并包括有侧表面,所述侧表面相背两端分别形成有转轴孔,所述转轴孔与所述转轴基本重叠,所述转 轴孔用于与所述云台的转轴配合。
  9. 如权利要求1所述的镜头座,其特征在于,所述第一连接元件为磁性元件,所述第二连接元件为磁性元件,所述目标配重后盖通过所述第一连接元件与所述第二连接元件的磁力配合装载到所述配重装载结构上。
  10. 如权利要求9所述的镜头座,其特征在于,所述配重装载结构形成有围绕所述第一连接元件的第一封闭部,所述目标配重后盖形成有围绕所述第二连接元件并与所述第一封闭部对应的第二封闭部,所述第一封闭部与所述第二封闭部贴合以封闭所述第一连接元件和所述第二连接元件的磁力。
  11. 如权利要求10所述的镜头座,其特征在于,所述第一封闭部采用通磁材料制成,所述第二封闭部采用通磁材料制成。
  12. 如权利要求1所述的镜头座,其特征在于,所述配重装载结构形成有与所述目标配重后盖配合的收容槽,所述目标配重后盖包括与所述收容槽的底面连接的连接面;
    所述第一连接元件设置在所述收容槽的底面上;
    所述第二连接元件对应所述第一连接元件设置在所述连接面上。
  13. 如权利要求12所述的镜头座,其特征在于,所述收容槽的底面呈矩形,所述第一连接元件包括四个并分别设置在所述收容槽的底面的四个角落。
  14. 如权利要求12所述的镜头座,其特征在于,所述配重装载结构包括形成于所述收容槽的底面的第一定位结构,所述目标配重后盖包括形成于所述连接面上的第二定位结构;
    所述目标配重后盖通过所述第一定位结构和所述第二定位结构配合定位到所述配重装载结构上。
  15. 一种摄像系统的安装方法,其特征在于包括以下步骤:
    提供如权利要求1-14任一项所述的镜头座和多个不同重量或型号的镜头,多个所述镜头中包括一个所述目标镜头;
    将所述目标镜头安装到所述镜头装载结构上;
    根据所述目标镜头的重量或型号选择对应的所述目标配重后盖;
    将所述目标配重后盖装配到所述配重装载结构上。
  16. 一种摄像系统,其特征在于包括:
    云台;
    如权利要求1-14任意一项所述的镜头座,所述镜头座通过所述转轴设置在所述云台上;和
    多个不同重量或型号的镜头,所述多个镜头包括装载在所述镜头装载结构上的目标镜头。
  17. 如权利要求16所述的摄像系统,其特征在于,所述云台包括框架和固定于所述框架上并能够驱动所述框架转动的电机组件,所述镜头座通过所述转轴设置在所述框架内。
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Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN203827428U (zh) * 2014-05-15 2014-09-10 王伟 监控摄像机
WO2017067005A1 (en) * 2015-10-23 2017-04-27 SZ DJI Technology Co., Ltd. Imaging system
US20170163896A1 (en) * 2015-12-03 2017-06-08 Samsung Electronics Co., Ltd. Camera gimbal
CN206446802U (zh) * 2017-01-19 2017-08-29 京杭遥感技术(杭州)有限公司 一种快速提升飞手技能的无人机
CN107097937A (zh) * 2017-03-18 2017-08-29 淄博萃智工业设计咨询有限公司 一种电力输配电网络鸟巢清除无人机系统使用方法
CN207015597U (zh) * 2017-06-23 2018-02-16 北京臻迪科技股份有限公司 一种云台系统
CN207304711U (zh) * 2017-09-30 2018-05-01 深圳市大疆灵眸科技有限公司 镜头座及使用该镜头座的摄像系统

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP4341267B2 (ja) * 2003-03-18 2009-10-07 カシオ計算機株式会社 携帯電子機器システム、携帯電子機器、携帯電子機器の制御方法及びプログラム
JP2010039350A (ja) * 2008-08-07 2010-02-18 Tamagawa Seiki Co Ltd 空間安定装置の重量バランス調整構造

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN203827428U (zh) * 2014-05-15 2014-09-10 王伟 监控摄像机
WO2017067005A1 (en) * 2015-10-23 2017-04-27 SZ DJI Technology Co., Ltd. Imaging system
US20170163896A1 (en) * 2015-12-03 2017-06-08 Samsung Electronics Co., Ltd. Camera gimbal
CN206446802U (zh) * 2017-01-19 2017-08-29 京杭遥感技术(杭州)有限公司 一种快速提升飞手技能的无人机
CN107097937A (zh) * 2017-03-18 2017-08-29 淄博萃智工业设计咨询有限公司 一种电力输配电网络鸟巢清除无人机系统使用方法
CN207015597U (zh) * 2017-06-23 2018-02-16 北京臻迪科技股份有限公司 一种云台系统
CN207304711U (zh) * 2017-09-30 2018-05-01 深圳市大疆灵眸科技有限公司 镜头座及使用该镜头座的摄像系统

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