WO2022141537A1 - Photographing device, gimbal assembly, unmanned aerial vehicle and unmanned aerial vehicle kit - Google Patents

Photographing device, gimbal assembly, unmanned aerial vehicle and unmanned aerial vehicle kit Download PDF

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Publication number
WO2022141537A1
WO2022141537A1 PCT/CN2020/142437 CN2020142437W WO2022141537A1 WO 2022141537 A1 WO2022141537 A1 WO 2022141537A1 CN 2020142437 W CN2020142437 W CN 2020142437W WO 2022141537 A1 WO2022141537 A1 WO 2022141537A1
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WO
WIPO (PCT)
Prior art keywords
photographing device
lens module
assembly
unmanned aerial
optical
Prior art date
Application number
PCT/CN2020/142437
Other languages
French (fr)
Chinese (zh)
Inventor
王平
杨镇坡
尤玉剑
夏龙光
Original Assignee
深圳市大疆创新科技有限公司
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
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Publication date
Application filed by 深圳市大疆创新科技有限公司 filed Critical 深圳市大疆创新科技有限公司
Priority to PCT/CN2020/142437 priority Critical patent/WO2022141537A1/en
Publication of WO2022141537A1 publication Critical patent/WO2022141537A1/en

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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U20/00Constructional aspects of UAVs
    • B64U20/80Arrangement of on-board electronics, e.g. avionics systems or wiring
    • B64U20/87Mounting of imaging devices, e.g. mounting of gimbals
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D47/00Equipment not otherwise provided for
    • 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

Definitions

  • the present application relates to the technical field of photographing equipment, and in particular, to a photographing device, a gimbal assembly, an unmanned aerial vehicle and an unmanned aerial vehicle kit.
  • the present application provides a photographing device, a pan/tilt assembly, an unmanned aerial vehicle, and an unmanned aerial vehicle kit, aiming at making the photographing device applicable to a pan/tilt or unmanned aerial vehicle to meet the miniaturization design of the product.
  • an embodiment of the present application provides a photographing device, the photographing device is used to connect to a pan/tilt, the pan/tilt is mounted on an unmanned aerial vehicle, and the unmanned aerial vehicle controls the The orientation of the shooting device; the shooting device includes a first lens module, and the first lens module includes:
  • a lens assembly including a casing and an optical element for receiving light from a shooting scene, the optical element being arranged on the casing;
  • the imaging element is arranged on the side circumference of the casing; the optical path changing element can change the propagation direction of the light passing through the optical element, and make the light after changing the propagation direction to be received by the imaging element .
  • an embodiment of the present application provides a pan-tilt assembly, including:
  • the imaging device is mounted on the platform.
  • an unmanned aerial vehicle including:
  • pan/tilt assembly described in any one of the above is provided on the main body of the unmanned aerial vehicle.
  • an unmanned aerial vehicle kit including:
  • pan/tilt assembly described in any one of the above is used to be installed on the unmanned aerial vehicle.
  • the embodiments of the present application provide a photographing device, a pan/tilt assembly, an unmanned aerial vehicle, and an unmanned aerial vehicle kit.
  • the light reaches the imaging element through the optical element and the optical path changing element of the photographing device in sequence, so that the first size of the photographing device can be reduced.
  • the volume and weight of the connecting bracket of the gimbal can be reduced, so the volume and weight of the gimbal assembly can be reduced, and the power consumption of the motor of the gimbal can be reduced, so that the gimbal assembly can realize Miniaturization, Lightweight and Portability.
  • the weight and volume of the unmanned aerial vehicle equipped with the gimbal assembly can be reduced, the power consumption of the unmanned aerial vehicle can be reduced, the use time of the unmanned aerial vehicle can be prolonged, and it is easy to realize Miniaturization, Lightweight and Portability.
  • FIG. 1 is a schematic structural diagram of an unmanned aerial vehicle kit provided by an embodiment of the present application.
  • FIG. 2 is a schematic structural diagram of a pan-tilt assembly provided by an embodiment of the present application.
  • FIG. 3 is an exploded schematic diagram of a pan/tilt assembly provided by an embodiment of the present application.
  • FIG. 4 is a schematic structural diagram of a photographing device provided by an embodiment of the present application.
  • FIG. 5 is an exploded schematic diagram of a photographing device provided by an embodiment of the present application.
  • FIG. 6 is a cross-sectional view of a photographing device provided by an embodiment of the present application.
  • FIG. 7 is an exploded schematic diagram of a photographing device provided by an embodiment of the present application.
  • FIG. 8 is an exploded schematic diagram of a photographing device provided by an embodiment of the present application.
  • FIG. 9 is a schematic structural diagram of a photographing device provided by an embodiment of the present application.
  • FIG. 10 is a schematic structural diagram of a photographing device provided by an embodiment of the present application.
  • FIG. 11 is a partial structural schematic diagram of a photographing apparatus provided by an embodiment of the present application.
  • the first lens module
  • Imaging element
  • the second lens module 201, the first accommodating slot; 202, the second accommodating slot; 203, the third accommodating slot; 204, the fourth accommodating slot;
  • 301 housing; 302, circuit board; 3021, first electrical connection part; 3022, second electrical connection part; 3023, third electrical connection part; 3024, fourth electrical connection part;
  • Unmanned aerial vehicle 1002. Unmanned aerial vehicle.
  • first and second are only used for descriptive purposes, and should not be construed as indicating or implying relative importance or implying the number of indicated technical features. Thus, features defined as “first”, “second” may expressly or implicitly include one or more of said features. In the description of the present application, “plurality” means two or more, unless otherwise expressly and specifically defined.
  • the traditional UAV shooting equipment does not have a reflector, and the light reaches the imaging sensor along the optical axis direction through the lens group, which will lead to a larger thickness and size of the shooting equipment.
  • the bracket of the gimbal also needs to be larger, so that the overall size and weight of the photographing device combined with the gimbal are relatively large.
  • the size and weight of the unmanned aerial vehicle equipped with the photographing device and the gimbal will also increase accordingly. Therefore, it is difficult for traditional photographing equipment to meet the requirements of miniaturization, portability and light weight of gimbals and unmanned aerial vehicles.
  • embodiments of the present application provide a photographing device, a pan-tilt assembly, an unmanned aerial vehicle, and an unmanned aerial vehicle kit, so that when the photographing device is applied to a pan-tilt or unmanned aerial vehicle, the miniaturized design of the product can be satisfied.
  • an unmanned aerial vehicle kit 1000 provided by an embodiment of the present application includes a gimbal assembly 1001 and an unmanned aerial vehicle 1002 .
  • the unmanned aerial vehicle 1002 may be a rotary-wing unmanned aerial vehicle, a fixed-wing unmanned aerial vehicle, an unmanned helicopter, or a hybrid fixed-wing-rotor-wing unmanned aerial vehicle, or the like.
  • the rotor unmanned aerial vehicle may be a single-rotor unmanned aerial vehicle or a multi-rotor unmanned aerial vehicle.
  • Multi-rotor UAVs include dual-rotor aircraft, tri-rotor aircraft, quad-rotor aircraft, hexa-rotor aircraft, octa-rotor aircraft, ten-rotor aircraft, twelve-rotor aircraft, etc.
  • unmanned aerial vehicle 1002 may include a fuselage, a powertrain.
  • the fuselage may include a center frame and one or more arms connected to the center frame, the one or more arms extending radially from the center frame.
  • the gimbal 102 of the gimbal assembly 1001 is fixedly or detachably connected to the body.
  • the power system includes a propeller and a motor, and the motor is used to drive the propeller to rotate, thereby providing flight power for the UAV 1002 .
  • the power motor and propeller are arranged on the arm.
  • the pan/tilt assembly 1001 includes a pan/tilt 102 and a camera 101 .
  • the gimbal 102 is mounted on the unmanned aerial vehicle 1002 .
  • the photographing device 101 is used for photographing pictures and/or videos.
  • the unmanned aerial vehicle 1002 controls the orientation of the photographing device 101 via the gimbal 102 .
  • the gimbal 102 can adjust the posture of the photographing device 101 and stabilize the photographing device 101 .
  • the photographing device 101 may be detachably or non-detachably connected to the pan/tilt head 102 .
  • the pan/tilt head 102 includes at least one of a pitch axis component 1021 , a roll axis component 1022 and a pan axis component 1023 for driving the camera 101 to move.
  • the photographing device 101 is connected to the gimbal 102 , the photographing device 101 is connected to any one of the pitch axis assembly 1021 , the roll axis assembly 1022 , and the pan axis assembly 1023 .
  • the gimbal 102 may include only one of the pitch axis assembly 1021 , the roll axis assembly 1022 and the pan axis assembly 1023 .
  • the gimbal 102 may also include any two of the pitch axis assembly 1021 , the roll axis assembly 1022 and the pan axis assembly 1023 .
  • the gimbal 102 may further include a pitch axis assembly 1021 , a roll axis assembly 1022 and a pan axis assembly 1023 .
  • the pan/tilt head 102 includes a pitch axis assembly 1021 , a roll axis assembly 1022 and a pan axis assembly 1023 .
  • the pan axis assembly 1023 includes a pan axis motor 10231 and a first connecting bracket 10232 .
  • the roll axis assembly 1022 includes a roll axis motor 10221 and a second connection bracket 10222 .
  • the pitch axis assembly 1021 includes a pitch axis motor 10211.
  • the rotating part of the pan axis motor 10231 is connected with the fixed part of the roll axis motor 10221 through the first connecting bracket 10232 for driving the camera 101 to rotate around the pan axis.
  • the rotating part of the roll axis motor 10221 is connected with the fixed part of the tilt axis motor 10211 through the second connecting bracket 10222, and is used to drive the photographing device 101 to rotate around the roll axis.
  • the photographing device 101 is mounted on the rotating part of the tilt axis motor 10211, and the tilt axis motor 10211 is used to drive the photographing device 101 to rotate around the tilt axis.
  • the photographing device 101 may be directly mounted or indirectly mounted on the rotating part of the pitch axis motor 10211 through the mounting portion.
  • the photographing device 101 may also be connected to the roll axis assembly 1022 or the pan axis assembly 1023, which is not limited herein.
  • a storage space 1024 is formed on the gimbal 102 for storing the photographing device 101 .
  • connection bracket including the first connection bracket 10232 and/or the second connection bracket 10222
  • motor including at least one of the pitch axis motor 10211 , the roll axis motor 10221 and the pan axis motor 10231
  • the storage space 1024 is formed in cooperation.
  • the imaging device 101 is at least partially accommodated in the accommodation space 1024 .
  • the size of the storage space 1024 is determined according to the size of the imaging device 101 .
  • the photographing device 101 includes a first lens module 100 .
  • the first lens module 100 includes a lens assembly 10 , an optical path changing element 20 and an imaging element 30 .
  • the lens assembly 10 includes a housing 11 and an optical element 12 for receiving light from a photographed scene.
  • the optical element 12 is provided on the casing 11 .
  • the optical path changing element 20 is provided on the casing 11 .
  • the imaging element 30 is provided on the housing 11 .
  • the imaging element 30 is provided on the side circumference of the casing 11 .
  • the optical path changing element 20 can change the propagation direction of the light passing through the optical element 12 , and make the light after changing the propagation direction to be received by the imaging element 30 .
  • the light reaches the imaging element 30 through the optical element 12 and the optical path changing element 20 in sequence, so that the thickness of the first lens module 100 can be reduced, thereby reducing the thickness of the first lens module 100 .
  • the small thickness of the photographing device 101 is beneficial to realize the miniaturization of the photographing device 101 .
  • the thickness of the storage space 1024 of the gimbal 102 along the photographing device 101 can be reduced, thereby reducing the volume and weight of the connecting bracket of the gimbal 102, thereby reducing the assembly of the gimbal
  • the volume and weight of 1001 reduce the power consumption of the motor of the pan/tilt 102, so that the pan/tilt assembly 1001 can achieve miniaturization, light weight and portability.
  • the weight and volume of the unmanned aerial vehicle 1002 equipped with the gimbal assembly 1001 can be reduced, the power consumption of the unmanned aerial vehicle 1002 can be reduced, and the life of the unmanned aerial vehicle 1002 can be prolonged. It can be used for a long time, and it is easy to achieve miniaturization, light weight and portability.
  • the photographing device 101 of the embodiment of the present application compared with the photographing device in which the light reaches the imaging sensor (corresponding to the imaging element 30 ) through the reflector (corresponding to the optical path changing element 20 ) and the lens group (corresponding to the optical element 12 ) in sequence, the photographing device 101 of the embodiment of the present application, the light passing through The optical elements 12 converge to reach the optical path changing element 20 , which can reduce the size and weight of the optical path changing element 20 , thereby reducing the width and thickness of the photographing device 101 , which is conducive to realizing the miniaturization of the photographing device 101 .
  • the size of the storage space 1024 of the pan-tilt 102 can be reduced, thereby reducing the volume and weight of the connecting bracket of the pan-tilt 102, thereby reducing the volume and weight of the pan-tilt assembly 1001.
  • the weight reduces the power consumption of the motor of the pan/tilt 102, so that the pan/tilt assembly 1001 can achieve miniaturization, light weight and portability.
  • the weight and volume of the unmanned aerial vehicle 1002 equipped with the gimbal assembly 1001 can be reduced, the power consumption of the unmanned aerial vehicle 1002 can be reduced, and the life of the unmanned aerial vehicle 1002 can be prolonged. It can be used for a long time, and it is easy to achieve miniaturization, light weight and portability.
  • the thickness extending direction of the photographing device 101 is substantially perpendicular to the width extending direction of the photographing device 101 .
  • the thickness extension direction of the photographing device 101 is shown in the Y direction in FIG. 3 and FIG. 4 .
  • the extending direction of the thickness of the photographing device 101 is parallel to the light incident to the first lens module 100 .
  • the thickness extension direction of the photographing device 101 is parallel to the optical axis incident to the optical element 12 .
  • the thickness extension direction of the photographing device 101 is parallel to or coincident with the roll axis of the roll axis motor 10221 .
  • the number of pitch axis motors 10211 is two, and the two pitch axis motors 10211 are arranged at intervals.
  • the photographing device 101 is sandwiched between two pitch axis motors 10211 .
  • the width extension direction of the photographing device 101 is parallel to the arrangement direction of the two pitch axis motors 10211 .
  • the width extension direction of the photographing device 101 is parallel to the pitch axis of the pitch axis motor 10211 .
  • the width extension direction of the photographing device 101 is shown in the X direction in FIGS. 3 and 4 .
  • the light incident to the optical element 12 is parallel to the roll axis of the roll axis motor 10221 .
  • the optical axis of the optical element 12 is parallel to or coincident with the roll axis of the roll axis motor 10221 .
  • the photographing device 101 further includes a housing 301 .
  • the first lens module 100 is disposed in the casing 301 .
  • the housing 301 is connected to any one of the pitch axis assembly 1021 , the roll axis assembly 1022 , and the pan axis assembly 1023 .
  • the size and weight of the housing 301 can also be correspondingly reduced.
  • the optical axis of the optical element 12 is parallel to the imaging element 30 .
  • the thickness of the first lens module 100 can be reduced, thereby reducing the thickness and weight of the housing 301 , and thus the thickness of the photographing device 101 can be reduced, which is beneficial to realize the miniaturization, light weight and portability of the photographing device 101 .
  • the photographing device 101 of this embodiment can further reduce the volume and weight of the connecting bracket of the gimbal 102 and reduce the power consumption of the motor of the gimbal 102 .
  • the weight and volume of the unmanned aerial vehicle 1002 equipped with the gimbal 102 can be further reduced, the power consumption of the unmanned aerial vehicle 1002 can be reduced, and the unmanned aerial vehicle 1002 can be extended.
  • the imaging element 30 is perpendicular to the optical element 12 .
  • the extending direction of the imaging element 30 in the first direction is perpendicular to the optical element 12 .
  • the thickness of the photographing device 101 can be reduced, and the thickness and weight of the casing 301 can be reduced, which is beneficial to realize the miniaturization, weight reduction and portability of the photographing device 101 .
  • the photographing device 101 of this embodiment can further reduce the volume and weight of the connecting bracket of the gimbal 102 and reduce the power consumption of the motor of the gimbal 102 .
  • the weight and volume of the unmanned aerial vehicle 1002 carrying the gimbal 102 can be further reduced, the power consumption of the unmanned aerial vehicle 1002 can be reduced, and the unmanned aerial vehicle 1002 can be extended.
  • the duration of use of the human aircraft 1002 is not limited.
  • the photographing device 101 when the photographing device 101 is connected to the gimbal 102 , the photographing device 101 is connected to any one of the pitch axis assembly 1021 , the roll axis assembly 1022 , and the pan axis assembly 1023 , and the imaging The element 30 is perpendicular to the pitch axis assembly 1021 , the roll axis assembly 1022 or the pan axis assembly 1023 connected to the camera 101 .
  • the photographing device 101 is connected to the pitch axis assembly 1021, and the imaging element 30 is perpendicular to the pitch axis of the pitch axis assembly 1021.
  • the photographing device 101 is connected to the roll axis assembly 1022 , and the imaging element 30 is perpendicular to the roll axis of the roll axis assembly 1022 .
  • the photographing device 101 is connected to the pan axis assembly 1023 , and the imaging element 30 is perpendicular to the pan axis of the pan axis assembly 1023 .
  • the photographing device 101 is fixedly connected to the pitch axis assembly 1021 , and the imaging element 30 is perpendicular to the pitch axis of the pitch axis motor 10211 of the pitch axis assembly 1021 .
  • the center of gravity of the photographing device 101 can be as close as possible to at least one of the pitch axis of the pitch axis assembly 1021 , the pitch axis of the roll axis assembly 1022 , and the pan axis of the pan axis assembly 1023 , saving the motor of the gimbal 102
  • the power consumption of the pan/tilt head 102 is increased, and the usage time of the motor of the gimbal 102 is prolonged.
  • the photographing device 101 may be fixedly connected to the rotating part of the pitch axis motor 10211 in a detachable connection manner or a non-detachable connection manner.
  • the pitch axis of the pitch axis motor 10211 may be a real axis or an imaginary axis, which is not limited here.
  • the extension direction of the pitch axis of the pitch axis motor 10211 is shown by the dotted line P in FIG. 3 .
  • the imaging element 30 is perpendicular to the dotted line P. As shown in FIG.
  • first part is perpendicular to the second part, including the case where the included angle between the first part and the second part is 80°, 85°, 90° and any other suitable angle between 80°-90° .
  • the third part is parallel to the fourth part, including the case where the included angle between the third part and the fourth part is 0°, 5°, 10° and any other suitable angle between 0°-10°.
  • the optical path changing element 20 may be fixedly connected to the lens assembly 10 through any suitable fixing structure, for example, the optical path changing element 20 is connected to the lens through at least one of an adhesive structure, a snap-fit structure, a quick-release structure, etc.
  • the assembly 10 is fixedly connected.
  • the imaging element 30 includes an imaging sensor, which utilizes the photoelectric conversion function of the photoelectric device to convert the optical signal received on the photosensitive surface thereof into an electrical signal corresponding to the optical signal.
  • the photographing device 101 further includes a second lens module 200 .
  • the first lens module 100 is connected to the second lens module 200 , and the shooting parameters of the second lens module 200 are different from the shooting parameters of the first lens module 100 .
  • the shooting parameters include at least one of focal length, angle of view, and the like.
  • the focal length of the first lens module 100 is different from the focal length of the second lens module 200 .
  • the first lens module 100 is a telephoto lens module
  • the second lens module 200 is a short-focus lens module.
  • the light reaches the imaging element 30 through the lens assembly 10 and the optical path changing element 20 of the first lens module 100, which can reduce the thickness of the first lens module 100, so that the thickness of the first lens module 100 is as close as possible to that of the second lens module 100.
  • the thickness of the lens module 200 can reduce the thickness of the first lens module 100 and the second lens module 200 after assembly, and reduce the thickness and weight of the housing 301, thereby reducing the volume of the photographing device 101, which is conducive to the realization of Miniaturization of the imaging device 101 .
  • the photographing device 101 of this embodiment can further reduce the volume and weight of the connecting bracket of the gimbal 102 and reduce the power consumption of the motor of the gimbal 102 .
  • the gimbal 102 equipped with the photographing device 101 is applied to the unmanned aerial vehicle 1002
  • the weight and volume of the unmanned aerial vehicle 1002 equipped with the gimbal 102 can be further reduced, the power consumption of the unmanned aerial vehicle 1002 can be reduced, and the unmanned aerial vehicle 1002 can be extended.
  • the shooting parameters of the second lens module 200 and the shooting parameters of the first lens module 100 may also be the same.
  • the second lens module 200 is arranged in the housing 301 .
  • the first lens module 100 may be fixedly connected or detachably connected to the second lens module 200 through a buckle structure, a quick-release structure, and an adhesive layer.
  • the optical axis of the optical element 12 is parallel to the optical axis of the second lens module 200 .
  • the optical axis of the optical element 12 is parallel to the light incoming direction of the second lens module 200 .
  • the light entering direction of the optical element 12 is the same as the light entering direction of the second lens module 200 .
  • the light entering direction of the optical element 12 is the same as the light entering direction of the second lens module 200 , including: the light entering direction of the optical element 12 is the same as the light entering direction of the second lens module 200 .
  • direction is parallel.
  • the dashed lines with arrows in Figures 5 and 6 and the like represent light rays.
  • the optical axis of the light incident to the first lens module 100 and the projection of the optical axis of the light incident to the second lens module 200 in the Z direction are substantially coincident to reduce
  • the coupling deviation between the first lens module 100 and the second lens module 200 ensures the imaging quality of the photographing device 101 .
  • the light entering direction of the optical element 12 is different from the light entering direction of the second lens module 200 .
  • the included angle between the light entering direction of the optical element 12 and the light entering direction of the second lens module 200 is an acute angle, an obtuse angle or a right angle, which is not limited herein.
  • the first lens module 100 and the second lens module 200 are stacked along the first direction.
  • the imaging element 30 is provided on the first side 13 or the second side 14 of the lens assembly 10 .
  • the first side 13 and the second side 14 are opposite sides of the lens assembly 10 along a second direction, which is different from the second direction.
  • the photographing device 101 of the above-mentioned embodiment can reduce the size of the first lens module 100 along the first direction and the size of the second direction, thereby reducing the rear edge of the assembly of the first lens module 100 and the second lens module 200.
  • the size of the first direction and the size of the second direction, and the size and weight of the housing 301 are reduced, the structure of the photographing device 101 is compact, and the space utilization rate is high, thereby reducing the volume and weight of the photographing device 101, which is beneficial to the realization of the photographing device. 101 miniaturization.
  • the photographing device 101 of this embodiment can further reduce the volume and weight of the connecting bracket of the gimbal 102 and reduce the power consumption of the motor of the gimbal 102 .
  • the gimbal 102 equipped with the photographing device 101 is applied to the unmanned aerial vehicle 1002
  • the weight and volume of the unmanned aerial vehicle 1002 equipped with the gimbal 102 can be further reduced, the power consumption of the unmanned aerial vehicle 1002 can be reduced, and the unmanned aerial vehicle 1002 can be extended.
  • the first direction intersects the second direction.
  • the first direction is perpendicular to the second direction.
  • the first direction is shown as the Z direction in FIGS. 3 and 4
  • the second direction is shown as the X direction in FIGS. 3 and 4 .
  • the first direction is shown as the X direction in FIGS. 3 and 4 .
  • the second direction is shown as the Z direction in FIGS. 3 and 4 .
  • the first direction is an up-down direction
  • the second direction is a left-right direction.
  • the direction of the arrow in the Z direction in FIG. 4 is upward, and the direction opposite to the direction of the arrow in the Z direction is downward.
  • the direction of the arrow in the X direction in FIG. 4 is the left, and the direction opposite to the direction of the arrow in the X direction is the right.
  • the first direction is a left-right direction
  • the second direction is an up-down direction
  • the top of the second lens module 200 is provided with a first accommodating groove 201 for accommodating at least part of the first lens module 100 .
  • the first accommodating groove 201 is formed on the top of the second lens module 200 .
  • the size along the first direction (such as the Z direction) after the first lens module 100 and the second lens module 200 are assembled can be reduced, thereby reducing the weight of the housing 301 and the size along the first direction, thereby reducing the The volume and weight of the photographing device 101 are better suited for the gimbal 102 or the unmanned aerial vehicle 1002 .
  • the dimension of the first lens module 100 or the photographing device 101 along the Z direction in FIG. 4 is defined as the height.
  • the height extending direction, the thickness extending direction, and the width extending direction of the photographing device 101 are perpendicular to each other.
  • the photographing device 101 in the embodiment of the present application is not limited to the stacking design of the first lens module 100 and the second lens module 200 .
  • a third lens module and/or other lens modules may also be provided, and the first lens module 100 , the second lens module 200 and the third lens module are stacked and arranged.
  • the side circumference of the housing 11 includes the surface on the side where the first side 13 is located and/or the surface on the side where the second side 14 is located.
  • the photographing device 101 further includes a circuit board 302 .
  • the first lens module 100 and the second lens module 200 are both connected to the same circuit board 302 for processing signals sent by the first lens module 100 and the second lens module 200 .
  • the photographing device 101 of this embodiment can reduce the number of structural components of the photographing device 101 and reduce the volume and weight of the housing 301 . Thereby, the size and weight of the photographing device 101 are further reduced.
  • the size of the storage space 1024 of the pan-tilt 102 can be reduced, thereby reducing the volume and weight of the connecting bracket of the pan-tilt 102, thereby reducing the volume and weight of the pan-tilt assembly 1001.
  • the weight reduces the power consumption of the motor of the pan/tilt 102, so that the pan/tilt assembly 1001 can achieve miniaturization, light weight and portability.
  • the gimbal assembly 1001 is applied to the unmanned aerial vehicle 1002
  • the weight and volume of the unmanned aerial vehicle 1002 equipped with the gimbal assembly 1001 can be reduced, the power consumption of the unmanned aerial vehicle 1002 can be reduced, and the life of the unmanned aerial vehicle 1002 can be prolonged. It can be used for a long time, and it is easy to achieve miniaturization, light weight and portability.
  • the circuit board 302 is electrically connected to the imaging element 30 for processing the electrical signal converted by the imaging element 30 to realize the photographing or video recording function of the photographing device 101 .
  • the circuit board 302 is communicatively connected to the gimbal 102 or the main control board (not shown) of the unmanned aerial vehicle 1002 .
  • the gimbal 102 or the unmanned aerial vehicle 1002 can communicate with the circuit board 302 through the main control board, so as to control the operation of the photographing device 101 or receive the photographing information of the photographing device 101 .
  • the main control board may be provided on the gimbal 102, or may be provided on the unmanned aerial vehicle 1002, which is not limited herein.
  • the circuit board 302 and the imaging element 30 are disposed on opposite sides of the assembly formed by the first lens module 100 and the second lens module 200 .
  • the first lens module 100 and the second lens module 200 are assembled to form an assembly.
  • the circuit board 302 and the imaging element 30 are disposed on opposite sides of the assembly, so that the structure of the photographing device 101 is compact and the volume of the photographing device 101 is reduced, so as to be more suitable for the pan/tilt head 102 or the unmanned aerial vehicle 1002 .
  • the circuit board 302 and the imaging element 30 are disposed on opposite sides of the assembly formed by the first lens module 100 and the second lens module 200 , which can balance the center of gravity of the photographing device 101 , so that the center of gravity of the photographing device 101 is as large as possible. It is close to at least one of the pitch axis of the pitch axis assembly 1021, the pitch axis of the roll axis assembly 1022, and the pan axis of the pan axis assembly 1023, which saves the power consumption of the motor of the gimbal 102 and prolongs the power consumption of the motor of the gimbal 102. duration of use.
  • the circuit board 302 is perpendicular to the rotation axis of the motor in the pan/tilt head 102 that is fixedly connected to the photographing device 101 .
  • the center of gravity of the photographing device 101 can be as close as possible to at least one of the pitch axis of the pitch axis assembly 1021 , the pitch axis of the roll axis assembly 1022 , and the pan axis of the pan axis assembly 1023 , saving the motor of the gimbal 102
  • the power consumption of the pan/tilt head 102 is increased, and the usage time of the motor of the gimbal 102 is prolonged.
  • the pitch axis motor 10211 is fixedly connected to the photographing device 101 .
  • the circuit board 302 is perpendicular to the pitch axis of the pitch axis motor 10211 .
  • the photographing device 101 further includes a first connection structure 400 and a second connection structure 500 .
  • the first connection structure 400 is connected to the circuit board 302 and the first lens module 100 .
  • the second connection structure 500 is connected to the circuit board 302 and the second lens module 200 . Both the first connection structure 400 and the second connection structure 500 are connected to the same circuit board 302 .
  • the photographing device 101 of this embodiment can reduce the number of structural parts of the photographing device 101 and the volume and weight of the housing 301 , thereby further reducing the size and weight of the housing 301 .
  • the size and weight of the photographing device 101 are reduced so as to be more suitable for the gimbal 102 or the unmanned aerial vehicle 1002 .
  • the first connecting structure 400 includes a first flexible connecting member 401 and a second flexible connecting member 402 .
  • the first flexible connector 401 is connected to the circuit board 302 and the motor of the lens assembly 10 .
  • the second flexible connector 402 is connected to the circuit board 302 and the imaging element 30 .
  • the second connecting structure 500 includes a third flexible connecting member 501 , a fourth flexible connecting member 502 and a fifth flexible connecting member 503 .
  • the third flexible connector 501 is connected to the circuit board 302 and the imaging member of the second lens module 200 .
  • the fourth flexible connector 502 is connected to the circuit board 302 and the motor of the lens of the second lens module 200 .
  • the aperture and/or the electronic shutter of the lens of the second lens module 200 are connected to the circuit board 302 through the fourth flexible connector 502 and the fifth flexible connector 503 .
  • the first flexible connector 401, the second flexible connector 402, the third flexible connector 501, and the fourth flexible connector 502 are all connected to the same circuit board 302, and the fourth flexible connector 502 is connected to the fifth flexible connector Piece 503 is connected.
  • both the first lens module 100 and the second lens module 200 can be connected to the same circuit board 302, so as to reduce the number of structural components of the photographing device 101, reduce the volume and weight of the housing 301, and further reduce the The size and weight of the photographing device 101 are better suited for the gimbal 102 or the unmanned aerial vehicle 1002 .
  • the circuit board 302 is provided with a first electrical connection part 3021 , a second electrical connection part 3022 , a third electrical connection part 3023 and a fourth electrical connection part 3024 .
  • a fifth electrical connecting portion 5021 is formed on the fourth flexible connecting member 502 .
  • the first electrical connection portion 3021 is connected to the first flexible connection member 401 so that the circuit board 302 can be electrically connected to the motor of the lens assembly 10 .
  • the second electrical connection portion 3022 is connected to the second flexible connection member 402 so that the circuit board 302 can be electrically connected to the imaging element 30 .
  • the third electrical connection portion 3023 is connected to the third flexible connection member 501 , so that the circuit board 302 can be electrically connected to the imaging member of the second lens module 200 .
  • the fourth electrical connection portion 3024 is connected to the fourth flexible connection member 502 , so that the circuit board 302 can be electrically connected to the motor of the lens of the second lens module 200 .
  • the fifth electrical connection portion 5021 is connected with the fifth flexible connecting member 503, so as to realize the electrical connection between the fourth flexible connecting member 502 and the fifth flexible connecting member 503, and further realize the electrical connection between the circuit board 302 and the lens of the second lens module 200. Aperture and/or electronic shutter.
  • the function of the imaging member of the second lens module 200 is the same as that of the imaging element 30 of the first lens module 100 .
  • the first flexible connector 401, the second flexible connector 402, the third flexible connector 501, the fourth flexible connector 502, and the fifth flexible connector 503 each include at least one of a flexible circuit board, a flexible cable, and the like. one.
  • the optical path changing element 20 includes a first reflecting mirror 21 .
  • the light reaches the imaging element 30 through the optical element 12 and the first reflecting mirror 21 in turn.
  • the number of structural parts of the optical path changing element 20 is reduced as much as possible, so as to reduce the volume and weight of the housing 301 as much as possible, thereby reducing the size and weight of the photographing device 101 as much as possible, so as to be better applicable to the pan/tilt head 102 or Unmanned aerial vehicle 1002.
  • first included angle between the reflection surface of the first reflecting mirror 21 and the optical axis of the optical element 12 .
  • second included angle between the reflection surface of the first reflection mirror 21 and the optical axis of the imaging element 30 .
  • the first included angle is 45°; and/or the second included angle is 45°.
  • first included angle and the second included angle can also be designed according to actual requirements, for example, the first included angle and the second included angle are both acute angles (eg, between 0°-90°). any other suitable angle).
  • first included angle is 30°
  • second included angle is 60°.
  • the included angle between the optical axis of the light incident on the reflective surface of the first reflective mirror 21 and the reflective surface of the first reflective mirror 21 is an acute angle, such as 10°, 30°, 45°, 60°, 80° and any other suitable angle between 10°-80°.
  • the included angle between the optical axis of the light emitted from the reflective surface of the first reflective mirror 21 and the reflective surface of the first reflective mirror 21 is an acute angle, such as 10°, 30°, 45°, 60°, 80° and any other suitable angle between 10°-80°.
  • the included angle between the optical axis of the light emitted from the reflective surface of the first reflecting mirror 21 and the imaging element 30 is an acute angle, such as 10°, 30°, 45°, 60°, 80° and 10° Any other suitable angle between -80°.
  • the optical path changing element 20 includes a second mirror 22 and a first prism 23 .
  • the second reflector 22 is provided on the casing 11 .
  • the first prism 23 is disposed on the casing 11 .
  • the light reaches the imaging element 30 through the second reflecting mirror 22 , the optical element 12 and the first prism 23 in sequence.
  • the thickness of the first lens module 100 can be reduced as much as possible, thereby reducing the volume and weight of the housing 301 as much as possible, and further reducing the size and weight of the photographing device 101 as much as possible, so as to be better suited for The gimbal 102 or the unmanned aerial vehicle 1002 .
  • the thickness extension direction of the first lens module 100 is along the X1 direction as shown in FIG. 9 .
  • the thickness extension direction of the first lens module 100 is parallel to the optical axis of the light incident to the first lens module 100 .
  • the optical axis of the optical element 12 is parallel to the imaging element 30 .
  • the structure of the first lens module 100 is compact and the optical path design is reasonable, so as to reduce the size of the photographing device 101 , so as to be more suitable for the gimbal 102 or the unmanned aerial vehicle 1002 .
  • the included angle between the reflecting surface of the second reflecting mirror 22 and the optical axis of the optical element 12 is an acute angle.
  • the included angle between the reflective surface of the second mirror 22 and the optical axis of the optical element 12 is 10°, 30°, 45°, 60°, 80° and any other suitable angle between 10°-80° .
  • the top and the side of the second lens module 200 are respectively provided with a second accommodating groove 202 and a third accommodating groove 203 that communicate with each other, and the optical element 12 is disposed in the second accommodating groove 202 .
  • Both the second accommodating groove 202 and the third accommodating groove 203 accommodate part of the casing 11 .
  • the direction of the arrow in the Z1 direction in FIG. 9 is up, and the direction opposite to the arrow direction in the Z1 direction is down.
  • the second accommodating groove 202 is formed on the top of the second lens module 200 .
  • the optical element 12 is disposed in the second accommodating groove 202 to reduce the height of the assembled first lens module 100 and the second lens module 200 , thereby reducing the weight and height of the housing 301 .
  • the arrangement of the third accommodating groove 203 can reduce the width of the assembled first lens module 100 and the second lens module 200 , thereby reducing the weight and width of the housing 301 . Therefore, the first accommodating slot 201 and the second accommodating slot 202 can effectively reduce the volume and weight of the photographing device 101 , so as to be more suitable for the pan/tilt head 102 or the unmanned aerial vehicle 1002 .
  • the height extending direction of the first lens module 100 and/or the second lens module 200 is parallel to Z1 in FIG. 9 .
  • the width extension direction of the first lens module 100 and/or the second lens module 200 is parallel to Y1 in FIG. 9 .
  • the third accommodating groove 203 extends from the top to the bottom of the second lens module 200 , and the imaging element 30 is at least partially disposed in the third accommodating groove 203 and is located at a position near the bottom of the third accommodating groove 203 side.
  • the structure of the first lens module 100 is compact, and the optical path design is reasonable, so as to reduce the size of the photographing device 101 , so as to be more suitable for the gimbal 102 or the unmanned aerial vehicle 1002 .
  • the first prism 23 includes a first side surface 231 , a second side surface 232 and a third side surface 233 connected in sequence, and the first side surface 231 is perpendicular to the third side surface 233 .
  • the light reaches the imaging element 30 through the optical element 12, the first side 231, the second side 232, and the third side 233 in sequence, so that the structure of the first lens module 100 is compact, the size of the photographing device 101 is reduced, and the Applicable to the gimbal 102 or the unmanned aerial vehicle 1002 .
  • the first side surface 231 is perpendicular to the imaging element 30
  • the third side surface 233 is parallel to the imaging element 30
  • the first side surface 231 is perpendicular to the third side surface 233
  • the included angle between the first side surface 231 and the second side surface 232 is an acute angle.
  • the included angle between the third side surface 233 and the second side surface 232 is an acute angle. In this way, it can be ensured that the light emitted from the optical element 12 can reach the imaging element 30 .
  • the light path changing element 20 includes a second prism 24 and a third prism 25 .
  • the second prism 24 is disposed on the casing 11 .
  • the third prism 25 is disposed on the casing 11 .
  • the light path reaches the imaging element 30 through the optical element 12 , the second prism 24 , and the third prism 25 .
  • the thickness of the first lens module 100 can be reduced, so as to reduce the volume and weight of the housing 301 as much as possible, thereby reducing the size and weight of the photographing device 101 as much as possible, so as to be more suitable for the gimbal 102 Or UAV 1002.
  • the thickness extension direction of the first lens module 100 is along the X2 direction as shown in FIG. 10 .
  • the optical axis of the optical element 12 is perpendicular to the imaging element 30 .
  • the optical axis of the optical element 12 and the imaging element 30 may also be arranged at an acute angle.
  • the optical element 12 , the second prism 24 , the third prism 25 and the imaging element 30 are arranged on the top of the second lens module 200 to make reasonable use of the space of the second lens module 200 , Reduce the size of the assembled first lens module 100 and the second lens module 200, thereby reducing the volume and weight of the housing 301, thereby reducing the size and weight of the photographing device 101 as much as possible, so as to be more suitable for The gimbal 102 or the unmanned aerial vehicle 1002 .
  • the direction of the arrow in the Z2 direction in FIG. 10 is up, and the direction opposite to the arrow direction in the Z2 direction is down.
  • the top of the second lens module 200 is provided with a fourth accommodating groove 204 , and the third prism 25 , the imaging element 30 and the casing 11 are all accommodated at least partially in the fourth accommodating groove 204. Therefore, the assembled height of the first lens module 100 and the second lens module 200 is reduced, thereby reducing the weight and thickness of the housing 301, thereby effectively reducing the volume and weight of the photographing device 101, so as to be more suitable for the gimbal 102 or unmanned aerial vehicle 1002.
  • the second prism 24 includes a fourth side surface 241 , a fifth side surface 242 and a sixth side surface 243 which are connected in sequence.
  • the fourth side 241 is perpendicular to the sixth side 243, and the light reaches the second prism 24 through the optical element 12, the fourth side 241, the fifth side 242, and the sixth side 243, thereby ensuring that the light emitted from the optical element 12 can reach the second prism 24. Prism 24.
  • the third prism 25 includes a seventh side surface 251 , an eighth side surface 252 and a ninth side surface 253 which are connected in sequence.
  • the seventh side 251 is perpendicular to the ninth side 253, and the light reaches the imaging element 30 through the second prism 24, the seventh side 251, the eighth side 252 and the ninth side 253, thereby ensuring that the light emitted from the optical element 12 passes through the second prism 24 and the third prism 25 can reach the imaging element 30 .
  • the fourth side surface 241 and the ninth side surface 253 are both parallel to the imaging element 30 and perpendicular to the optical axis of the optical element 12 .
  • the optical path of the first lens module 100 can be folded, and the thickness of the first lens module 100 can be reduced, thereby reducing the weight and thickness of the housing 301 , thereby effectively reducing the volume and weight of the photographing device 101 to better It is suitable for the gimbal 102 and the unmanned aerial vehicle 1002 , and reduces the power consumption of the motor control of the gimbal 102 and the power consumption of the unmanned aerial vehicle 1002 .
  • the optical element 12 includes at least one lens element.
  • a side perimeter of the optical element 12 is formed with a cut edge 121 .
  • the size and weight of the optical element 12 are reduced as much as possible, thereby reducing the weight and size of the housing 301, thereby effectively reducing the volume and weight of the photographing device 101, so as to reduce the size and weight of the optical element 12 as much as possible. It is better applicable to the gimbal 102 and the unmanned aerial vehicle 1002 , and reduces the power consumption of the motor control of the gimbal 102 and the power consumption of the unmanned aerial vehicle 1002 .
  • the side perimeter of the optical element 12 includes the perimeter of the optical element 12 that is not used to direct light propagation.
  • one, two, three or more of the cut edges 121 on the optical element 12 may be provided, which is not limited herein.
  • two cut edges 121 are formed on the side circumference of the optical element 12, and the two cut edges 121 are disposed opposite to each other.
  • the side periphery of the optical device of the second lens module 200 is formed with a cut edge 121 .
  • the size and weight of the optical device are reduced as much as possible, thereby reducing the weight and size of the housing 301, thereby effectively reducing the volume and weight of the photographing device 101, so as to be more Well suited for the gimbal 102 or the unmanned aerial vehicle 1002 .
  • the function of the optical device is substantially the same as that of the optical element 12 .
  • the shape of the cut edge 121 can be designed according to actual requirements, such as a plane, a curved surface, a racetrack shape, and the like.
  • Embodiments of the present application further provide an unmanned aerial vehicle, including an unmanned aerial vehicle body and the pan/tilt assembly of any one of the foregoing embodiments.
  • the gimbal assembly is arranged on the main body of the unmanned aerial vehicle.
  • the unmanned aerial vehicle may be a rotary-wing unmanned aerial vehicle, a fixed-wing unmanned aerial vehicle, an unmanned helicopter, or a hybrid unmanned aerial vehicle of fixed-wing and rotary-wing.
  • the rotor unmanned aerial vehicle may be a single-rotor unmanned aerial vehicle or a multi-rotor unmanned aerial vehicle.
  • Multi-rotor UAVs include dual-rotor aircraft, tri-rotor aircraft, quad-rotor aircraft, hexa-rotor aircraft, octa-rotor aircraft, ten-rotor aircraft, twelve-rotor aircraft, etc.
  • the UAV body includes a fuselage, a power system.
  • the fuselage may include a center frame and one or more arms connected to the center frame, the one or more arms extending radially from the center frame.
  • the gimbal of the gimbal assembly is fixedly or detachably connected to the body.
  • the power system includes a propeller and a motor, and the motor is used to drive the propeller to rotate, thereby providing flight power for the unmanned aerial vehicle.
  • the power motor and propeller are arranged on the arm.
  • the terms “installed”, “connected” and “connected” should be understood in a broad sense, for example, it may be a fixed connection or a detachable connection connected, or integrally connected. It can be a mechanical connection or an electrical connection. It can be directly connected, or indirectly connected through an intermediate medium, and it can be the internal communication between two elements or the interaction relationship between the two elements.
  • installed should be understood in a broad sense, for example, it may be a fixed connection or a detachable connection connected, or integrally connected. It can be a mechanical connection or an electrical connection. It can be directly connected, or indirectly connected through an intermediate medium, and it can be the internal communication between two elements or the interaction relationship between the two elements.
  • a first feature "on” or “under” a second feature may include direct contact between the first and second features, or may include the first and second features Not directly but through additional features between them.
  • the first feature being “above”, “over” and “above” the second feature includes the first feature being directly above and obliquely above the second feature, or simply means that the first feature is level higher than the second feature.
  • the first feature is “below”, “below” and “below” the second feature includes the first feature being directly below and diagonally below the second feature, or simply means that the first feature has a lower level than the second feature.

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Abstract

A photographing device (101) is used for being connected to a gimbal (102), and the gimbal (102) is carried on an unmanned aerial vehicle (1002). A first lens module (100) of the photographing device (101) comprises a lens assembly (10), an optical path changing element (20) and an imaging element (30). The lens assembly (10) comprises a shell (11) and an optical element (12). The optical element (12), the optical path changing element (20) and the imaging element (30) are all arranged on the shell (11). The imaging element (30) is arranged on the side periphery of the shell (11). The optical path changing element (20) can change the transmission direction of light rays penetrating through the optical element (12), and the light rays with the transmission direction changed are received by the imaging element (30). Further disclosed are a gimbal assembly (1001), the unmanned aerial vehicle (1002) and an unmanned aerial vehicle kit (1000).

Description

拍摄装置、云台组件、无人飞行器及无人飞行器套件Cameras, gimbal components, unmanned aerial vehicles and unmanned aerial vehicle kits 技术领域technical field
本申请涉及拍摄设备技术领域,尤其涉及一种拍摄装置、云台组件、无人飞行器及无人飞行器套件。The present application relates to the technical field of photographing equipment, and in particular, to a photographing device, a gimbal assembly, an unmanned aerial vehicle and an unmanned aerial vehicle kit.
背景技术Background technique
相机等拍摄设备已经广泛应用于人们的日常生活中,为记录人们生活中的点滴提供了便捷。传统的拍摄设备,由于摄像头镜头模组的各光学元器件的布局不够合理,拍摄设备应用于云台上时,会导致拍摄设备与云台组合后的整体尺寸比较大,无法满足小型化和便携性的需求。Cameras and other shooting devices have been widely used in people's daily life, which provides convenience for recording every bit of people's life. For traditional shooting equipment, due to the unreasonable layout of the optical components of the camera lens module, when the shooting equipment is applied to the gimbal, the overall size of the shooting device and the gimbal will be relatively large, which cannot meet the requirements of miniaturization and portability. sexual needs.
发明内容SUMMARY OF THE INVENTION
本申请提供了一种拍摄装置、云台组件、无人飞行器及无人飞行器套件,旨在使得拍摄装置应用于云台或者无人飞行器时,能够满足产品的小型化设计。The present application provides a photographing device, a pan/tilt assembly, an unmanned aerial vehicle, and an unmanned aerial vehicle kit, aiming at making the photographing device applicable to a pan/tilt or unmanned aerial vehicle to meet the miniaturization design of the product.
第一方面,本申请实施例提供了一种拍摄装置,所述拍摄装置用于与云台连接,所述云台搭载在无人飞行器上,所述无人飞行器经过所述云台控制所述拍摄装置的朝向;所述拍摄装置包括第一镜头模组,所述第一镜头模组包括:In a first aspect, an embodiment of the present application provides a photographing device, the photographing device is used to connect to a pan/tilt, the pan/tilt is mounted on an unmanned aerial vehicle, and the unmanned aerial vehicle controls the The orientation of the shooting device; the shooting device includes a first lens module, and the first lens module includes:
镜头组件,包括壳体和用于接收来自拍摄场景的光线的光学元件,所述光学元件设于所述壳体上;a lens assembly, including a casing and an optical element for receiving light from a shooting scene, the optical element being arranged on the casing;
光路改变元件,设于所述壳体上;an optical path changing element, arranged on the casing;
成像元件,设于所述壳体上;an imaging element, arranged on the casing;
其中,所述成像元件设于所述壳体的侧周;所述光路改变元件能够改变透过所述光学元件的光线的传播方向,并使改变传播方向后的光线被所述成像元件所接收。Wherein, the imaging element is arranged on the side circumference of the casing; the optical path changing element can change the propagation direction of the light passing through the optical element, and make the light after changing the propagation direction to be received by the imaging element .
第二方面,本申请实施例提供了一种云台组件,包括:In a second aspect, an embodiment of the present application provides a pan-tilt assembly, including:
云台;以及PTZ; and
上述任一项所述的拍摄装置,搭载于所述云台上。The imaging device according to any one of the above is mounted on the platform.
第三方面,本申请实施例提供了一种无人飞行器,包括:In a third aspect, an embodiment of the present application provides an unmanned aerial vehicle, including:
无人飞行器主体;以及the body of the unmanned aerial vehicle; and
上述任一项所述的云台组件,设于所述无人飞行器主体上。The pan/tilt assembly described in any one of the above is provided on the main body of the unmanned aerial vehicle.
第四方面,本申请实施例提供了一种无人飞行器套件,包括:In a fourth aspect, an embodiment of the present application provides an unmanned aerial vehicle kit, including:
无人飞行器;以及unmanned aerial vehicles; and
上述任一项所述的云台组件,用于设于所述无人飞行器上。The pan/tilt assembly described in any one of the above is used to be installed on the unmanned aerial vehicle.
本申请实施例提供了一种拍摄装置、云台组件、无人飞行器及无人飞行器套件,光线依次经拍摄装置的光学元件、光路改变元件到达成像元件,如此能够减小拍摄装置的第一尺寸。当该拍摄装置应用于云台时,能够减小云台的连接支架的体积和重量,因而能够减小云台组件的体积和重量,减小云台的电机的功耗,使得云台组件实现小型化、轻量化和便携性。当该云台组件应用于无人飞行器后,能够使得搭载有云台组件的无人飞行器的重量和体积减小,能够减少无人飞行器的功耗,延长无人飞行器的使用时长,且便于实现小型化、轻量化和便携性。The embodiments of the present application provide a photographing device, a pan/tilt assembly, an unmanned aerial vehicle, and an unmanned aerial vehicle kit. The light reaches the imaging element through the optical element and the optical path changing element of the photographing device in sequence, so that the first size of the photographing device can be reduced. . When the photographing device is applied to the gimbal, the volume and weight of the connecting bracket of the gimbal can be reduced, so the volume and weight of the gimbal assembly can be reduced, and the power consumption of the motor of the gimbal can be reduced, so that the gimbal assembly can realize Miniaturization, Lightweight and Portability. When the gimbal assembly is applied to the unmanned aerial vehicle, the weight and volume of the unmanned aerial vehicle equipped with the gimbal assembly can be reduced, the power consumption of the unmanned aerial vehicle can be reduced, the use time of the unmanned aerial vehicle can be prolonged, and it is easy to realize Miniaturization, Lightweight and Portability.
应当理解的是,以上的一般描述和后文的细节描述仅是示例性和解释性的,并不能限制本申请实施例的公开内容。It should be understood that the above general description and the following detailed description are only exemplary and explanatory, and do not limit the disclosure of the embodiments of the present application.
附图说明Description of drawings
为了更清楚地说明本申请实施例的技术方案,下面将对实施例描述中所需要使用的附图作简单地介绍,显而易见地,下面描述中的附图是本申请的一些实施例,对于本领域普通技术人员来讲,在不付出创造性劳动的前提下,还可以根据这些附图获得其他的附图。In order to explain the technical solutions of the embodiments of the present application more clearly, the following briefly introduces the accompanying drawings used in the description of the embodiments. Obviously, the drawings in the following description are some embodiments of the present application. For those of ordinary skill in the art, other drawings can also be obtained from these drawings without any creative effort.
图1是本申请实施例提供的一种无人飞行器套件的结构示意图;1 is a schematic structural diagram of an unmanned aerial vehicle kit provided by an embodiment of the present application;
图2是本申请实施例提供的一种云台组件的结构示意图;2 is a schematic structural diagram of a pan-tilt assembly provided by an embodiment of the present application;
图3是本申请实施例提供的一种云台组件的分解示意图;3 is an exploded schematic diagram of a pan/tilt assembly provided by an embodiment of the present application;
图4是本申请实施例提供的一种拍摄装置的结构示意图;4 is a schematic structural diagram of a photographing device provided by an embodiment of the present application;
图5是本申请实施例提供的一种拍摄装置的分解示意图;5 is an exploded schematic diagram of a photographing device provided by an embodiment of the present application;
图6是本申请实施例提供的一种拍摄装置的剖视图;6 is a cross-sectional view of a photographing device provided by an embodiment of the present application;
图7是本申请实施例提供的一种拍摄装置的分解示意图;FIG. 7 is an exploded schematic diagram of a photographing device provided by an embodiment of the present application;
图8是本申请实施例提供的一种拍摄装置的分解示意图;8 is an exploded schematic diagram of a photographing device provided by an embodiment of the present application;
图9是本申请实施例提供的一种拍摄装置的结构示意图;9 is a schematic structural diagram of a photographing device provided by an embodiment of the present application;
图10是本申请实施例提供的一种拍摄装置的结构示意图;10 is a schematic structural diagram of a photographing device provided by an embodiment of the present application;
图11是本申请实施例提供的一种拍摄装置的部分结构示意图。FIG. 11 is a partial structural schematic diagram of a photographing apparatus provided by an embodiment of the present application.
附图标记说明:Description of reference numbers:
1000、无人飞行器套件;1000. Unmanned aerial vehicle kit;
1001、云台组件;101、拍摄装置;1001, a pan/tilt assembly; 101, a photographing device;
100、第一镜头模组;100. The first lens module;
10、镜头组件;11、壳体;12、光学元件;121、切边;13、第一侧;14、第二侧;10, lens assembly; 11, housing; 12, optical element; 121, trimming; 13, first side; 14, second side;
20、光路改变元件;21、第一反射镜;22、第二反射镜;23、第一棱镜;231、第一侧面;232、第二侧面;233、第三侧面;24、第二棱镜;241、第四侧面;242、第五侧面;243、第六侧面;25、第三棱镜;251、第七侧面;252、第八侧面;253、第九侧面;20, optical path changing element; 21, first reflector; 22, second reflector; 23, first prism; 231, first side; 232, second side; 233, third side; 24, second prism; 241, the fourth side; 242, the fifth side; 243, the sixth side; 25, the third prism; 251, the seventh side; 252, the eighth side; 253, the ninth side;
30、成像元件;30. Imaging element;
200、第二镜头模组;201、第一容置槽;202、第二容置槽;203、第三容置槽;204、第四容置槽;200, the second lens module; 201, the first accommodating slot; 202, the second accommodating slot; 203, the third accommodating slot; 204, the fourth accommodating slot;
301、外壳;302、电路板;3021、第一电连接部;3022、第二电连接部;3023、第三电连接部;3024、第四电连接部;301, housing; 302, circuit board; 3021, first electrical connection part; 3022, second electrical connection part; 3023, third electrical connection part; 3024, fourth electrical connection part;
400、第一连接结构;401、第一柔性连接件;402、第二柔性连接件;400, a first connection structure; 401, a first flexible connection piece; 402, a second flexible connection piece;
500、第二连接结构;501、第三柔性连接件;502、第四柔性连接件;5021、第五电连接部;503、第五柔性连接件;500, the second connection structure; 501, the third flexible connection piece; 502, the fourth flexible connection piece; 5021, the fifth electrical connection part; 503, the fifth flexible connection piece;
102、云台;1021、俯仰轴组件;10211、俯仰轴电机;1022、横滚轴组件;10221、横滚轴电机;10222、第二连接支架;1023、航向轴组件;10231、航向轴电机;10232、第一连接支架;1024、收纳空间;102, PTZ; 1021, pitch axis assembly; 10211, pitch axis motor; 1022, roll axis assembly; 10221, roll axis motor; 10222, second connecting bracket; 1023, pan axis assembly; 10231, pan axis motor; 10232, the first connecting bracket; 1024, the storage space;
1002、无人飞行器。1002. Unmanned aerial vehicle.
具体实施方式Detailed ways
下面将结合本申请实施例中的附图,对本申请实施例中的技术方案进行清楚、完整地描述,显然,所描述的实施例是本申请一部分实施例,而不是全部的实施例。基于本申请中的实施例,本领域普通技术人员在没有做出创造性劳动前提下所获得的所有其他实施例,都属于本申请保护的范围。The technical solutions in the embodiments of the present application will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present application. Obviously, the described embodiments are part of the embodiments of the present application, not all of the embodiments. Based on the embodiments in the present application, all other embodiments obtained by those of ordinary skill in the art without creative efforts shall fall within the protection scope of the present application.
在本申请的描述中,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申请和简化描述,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申请的限制。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。在本申请的描述中,“多个”的含义是两个或两个以上,除非另有明确具体的限定。In the description of this application, it should be understood that the terms "center", "longitudinal", "lateral", "length", "width", "thickness", "upper", "lower", "front", " rear, left, right, vertical, horizontal, top, bottom, inside, outside, clockwise, counterclockwise, etc., or The positional relationship is based on the orientation or positional relationship shown in the accompanying drawings, which is only for the convenience of describing the present application and simplifying the description, rather than indicating or implying that the referred device or element must have a specific orientation, be constructed and operated in a specific orientation, Therefore, it should not be construed as a limitation on this application. In addition, the terms "first" and "second" are only used for descriptive purposes, and should not be construed as indicating or implying relative importance or implying the number of indicated technical features. Thus, features defined as "first", "second" may expressly or implicitly include one or more of said features. In the description of the present application, "plurality" means two or more, unless otherwise expressly and specifically defined.
还应当理解,在本申请说明书中所使用的术语仅仅是出于描述特定实施例的目的而并不意在限制本申请。如在本申请说明书和所附权利要求书中所使用的那样,除非上下文清楚地指明其它情况,否则单数形式的“一”、“一个”及“该”意在包括复数形式。It should also be understood that the terms used in the specification of the present application are for the purpose of describing particular embodiments only and are not intended to limit the present application. As used in this specification and the appended claims, the singular forms "a," "an," and "the" are intended to include the plural unless the context clearly dictates otherwise.
还应当进一步理解,在本申请说明书和所附权利要求书中使用的术语“和/或”是指相关联列出的项中的一个或多个的任何组合以及所有可能组合,并且包括这些组合。It should also be further understood that, as used in this specification and the appended claims, the term "and/or" refers to and including any and all possible combinations of one or more of the associated listed items .
传统的无人机的拍摄设备没有设反射镜,光线经透镜组沿着光轴方向达到成像传感器上,如此会导致拍摄设备的厚度尺寸较大。这种拍摄设备应用于云台中时,云台的支架也需要较大尺寸,致使拍摄设备与云台组合后的整体尺寸和重量比较大。当搭载有拍摄设备的云台应用于无人飞行器上时,会导致搭载有该拍摄设备和云台的无人飞行器的尺寸和重量也相应变大。因而传统的拍摄设备难以满足云台和无人飞行器的小型化、便携性以及轻量化的需求。The traditional UAV shooting equipment does not have a reflector, and the light reaches the imaging sensor along the optical axis direction through the lens group, which will lead to a larger thickness and size of the shooting equipment. When the photographing device is used in the gimbal, the bracket of the gimbal also needs to be larger, so that the overall size and weight of the photographing device combined with the gimbal are relatively large. When a gimbal equipped with a photographing device is applied to an unmanned aerial vehicle, the size and weight of the unmanned aerial vehicle equipped with the photographing device and the gimbal will also increase accordingly. Therefore, it is difficult for traditional photographing equipment to meet the requirements of miniaturization, portability and light weight of gimbals and unmanned aerial vehicles.
为此,本申请实施例提供了一种拍摄装置、云台组件、无人飞行器及无人飞行器套件,以使得拍摄装置应用于云台或者无人飞行器时,能够满足产品的小型化设计。To this end, embodiments of the present application provide a photographing device, a pan-tilt assembly, an unmanned aerial vehicle, and an unmanned aerial vehicle kit, so that when the photographing device is applied to a pan-tilt or unmanned aerial vehicle, the miniaturized design of the product can be satisfied.
下面结合附图,对本申请的一些实施方式作详细说明。在不冲突的情况下,下述的实施例及实施例中的特征可以相互组合。Some embodiments of the present application will be described in detail below with reference to the accompanying drawings. The embodiments described below and features in the embodiments may be combined with each other without conflict.
请参阅图1,本申请实施例提供的一种无人飞行器套件1000包括云台组件1001和无人飞行器1002。无人飞行器1002可以为旋翼无人飞行器、固定翼无人飞行器、无人直升机或者固定翼-旋翼混合的无人飞行器等。其中,旋翼无人飞行器可为单旋翼无人飞行器或者多旋翼无人飞行器。多旋翼无人飞行器包括双旋翼飞行器、三旋翼飞行器、四旋翼飞行器、六旋翼飞行器、八旋翼飞行器、十旋翼飞行器、十二旋翼飞行器等。Referring to FIG. 1 , an unmanned aerial vehicle kit 1000 provided by an embodiment of the present application includes a gimbal assembly 1001 and an unmanned aerial vehicle 1002 . The unmanned aerial vehicle 1002 may be a rotary-wing unmanned aerial vehicle, a fixed-wing unmanned aerial vehicle, an unmanned helicopter, or a hybrid fixed-wing-rotor-wing unmanned aerial vehicle, or the like. The rotor unmanned aerial vehicle may be a single-rotor unmanned aerial vehicle or a multi-rotor unmanned aerial vehicle. Multi-rotor UAVs include dual-rotor aircraft, tri-rotor aircraft, quad-rotor aircraft, hexa-rotor aircraft, octa-rotor aircraft, ten-rotor aircraft, twelve-rotor aircraft, etc.
示例性地,无人飞行器1002可以包括机身、动力系统。机身可以包括中心架以及与中心架连接的一个或多个机臂,一个或多个机臂呈辐射状从中心架延伸出。Illustratively, unmanned aerial vehicle 1002 may include a fuselage, a powertrain. The fuselage may include a center frame and one or more arms connected to the center frame, the one or more arms extending radially from the center frame.
示例性地,云台组件1001的云台102与机身固定连接或者可拆卸连接。Exemplarily, the gimbal 102 of the gimbal assembly 1001 is fixedly or detachably connected to the body.
示例性地,动力系统包括螺旋桨和电机,电机用于驱动螺旋桨旋转,从而为无人飞行器1002提供飞行动力。动力电机和螺旋桨设置在机臂上。Illustratively, the power system includes a propeller and a motor, and the motor is used to drive the propeller to rotate, thereby providing flight power for the UAV 1002 . The power motor and propeller are arranged on the arm.
示例性地,云台组件1001包括云台102和拍摄装置101。云台102搭载在无人飞行器1002上。拍摄装置101用于拍摄图片和/或视频。示例性地,无人飞行器1002经过云台102控制拍摄装置101的朝向。Exemplarily, the pan/tilt assembly 1001 includes a pan/tilt 102 and a camera 101 . The gimbal 102 is mounted on the unmanned aerial vehicle 1002 . The photographing device 101 is used for photographing pictures and/or videos. Exemplarily, the unmanned aerial vehicle 1002 controls the orientation of the photographing device 101 via the gimbal 102 .
云台102能够调节拍摄装置101的姿态,并为拍摄装置101增稳。The gimbal 102 can adjust the posture of the photographing device 101 and stabilize the photographing device 101 .
示例性地,拍摄装置101可以与云台102可拆卸连接或者不可拆卸连接。Exemplarily, the photographing device 101 may be detachably or non-detachably connected to the pan/tilt head 102 .
请参阅图2,在一些实施例中,云台102包括俯仰轴组件1021、横滚轴组件1022和航向轴组件1023中的至少一者,用于驱动拍摄装置101运动。当拍摄装置101与云台102连接时,拍摄装置101连接于俯仰轴组件1021、横滚轴组件1022、航向轴组件1023中任意一个。Referring to FIG. 2 , in some embodiments, the pan/tilt head 102 includes at least one of a pitch axis component 1021 , a roll axis component 1022 and a pan axis component 1023 for driving the camera 101 to move. When the photographing device 101 is connected to the gimbal 102 , the photographing device 101 is connected to any one of the pitch axis assembly 1021 , the roll axis assembly 1022 , and the pan axis assembly 1023 .
示例性地,云台102可以仅包括俯仰轴组件1021、横滚轴组件1022和航向轴组件1023中的其中一个。云台102也可以包括俯仰轴组件1021、横滚轴组件1022和航向轴组件1023中的任意两个。云台102还可以包括俯仰轴组件1021、横滚轴组件1022和航向轴组件1023。Exemplarily, the gimbal 102 may include only one of the pitch axis assembly 1021 , the roll axis assembly 1022 and the pan axis assembly 1023 . The gimbal 102 may also include any two of the pitch axis assembly 1021 , the roll axis assembly 1022 and the pan axis assembly 1023 . The gimbal 102 may further include a pitch axis assembly 1021 , a roll axis assembly 1022 and a pan axis assembly 1023 .
请参阅图3,示例性地,云台102包括俯仰轴组件1021、横滚轴组件1022和航向轴组件1023。航向轴组件1023包括航向轴电机10231和第一连接支架10232。横滚轴组件1022包括横滚轴电机10221和第二连接支架10222。俯仰 轴组件1021包括俯仰轴电机10211。Referring to FIG. 3 , for example, the pan/tilt head 102 includes a pitch axis assembly 1021 , a roll axis assembly 1022 and a pan axis assembly 1023 . The pan axis assembly 1023 includes a pan axis motor 10231 and a first connecting bracket 10232 . The roll axis assembly 1022 includes a roll axis motor 10221 and a second connection bracket 10222 . The pitch axis assembly 1021 includes a pitch axis motor 10211.
请参阅图3,示例性地,航向轴电机10231的转动部分通过第一连接支架10232与横滚轴电机10221的固定部分连接,用于驱动拍摄装置101绕航向轴转动。横滚轴电机10221的转动部分通过第二连接支架10222与俯仰轴电机10211的固定部分连接,用于驱动拍摄装置101绕横滚轴转动。拍摄装置101搭载在俯仰轴电机10211的转动部分上,俯仰轴电机10211用于驱动拍摄装置101绕俯仰轴转动。Referring to FIG. 3 , for example, the rotating part of the pan axis motor 10231 is connected with the fixed part of the roll axis motor 10221 through the first connecting bracket 10232 for driving the camera 101 to rotate around the pan axis. The rotating part of the roll axis motor 10221 is connected with the fixed part of the tilt axis motor 10211 through the second connecting bracket 10222, and is used to drive the photographing device 101 to rotate around the roll axis. The photographing device 101 is mounted on the rotating part of the tilt axis motor 10211, and the tilt axis motor 10211 is used to drive the photographing device 101 to rotate around the tilt axis.
示例性地,拍摄装置101可以直接搭载或者通过搭载部间接搭载在俯仰轴电机10211的转动部分上。Exemplarily, the photographing device 101 may be directly mounted or indirectly mounted on the rotating part of the pitch axis motor 10211 through the mounting portion.
在其他实施例中,拍摄装置101也可以连接于横滚轴组件1022或者航向轴组件1023,在此不作限制。In other embodiments, the photographing device 101 may also be connected to the roll axis assembly 1022 or the pan axis assembly 1023, which is not limited herein.
请参阅图2,云台102形成有收纳空间1024,用于收纳拍摄装置101。Referring to FIG. 2 , a storage space 1024 is formed on the gimbal 102 for storing the photographing device 101 .
示例性地,云台102的连接支架(包括第一连接支架10232和/或第二连接支架10222)与电机(包括俯仰轴电机10211、横滚轴电机10221和航向轴电机10231中的至少一个)配合形成收纳空间1024。拍摄装置101至少部分收纳于收纳空间1024。Exemplarily, the connection bracket (including the first connection bracket 10232 and/or the second connection bracket 10222 ) and the motor (including at least one of the pitch axis motor 10211 , the roll axis motor 10221 and the pan axis motor 10231 ) of the gimbal 102 The storage space 1024 is formed in cooperation. The imaging device 101 is at least partially accommodated in the accommodation space 1024 .
可以理解地,若收纳空间1024的大小减小,则云台102的连接支架的体积和重量也相应减小。而收纳空间1024的大小根据拍摄装置101的尺寸进行确定。It can be understood that, if the size of the storage space 1024 is reduced, the volume and weight of the connecting bracket of the pan/tilt head 102 are correspondingly reduced. The size of the storage space 1024 is determined according to the size of the imaging device 101 .
请参阅图4至图6,在一些实施例中,拍摄装置101包括第一镜头模组100。第一镜头模组100包括镜头组件10、光路改变元件20和成像元件30。镜头组件10包括壳体11和用于接收来自拍摄场景的光线的光学元件12。光学元件12设于壳体11上。光路改变元件20设于壳体11上。成像元件30设于壳体11上。Referring to FIGS. 4 to 6 , in some embodiments, the photographing device 101 includes a first lens module 100 . The first lens module 100 includes a lens assembly 10 , an optical path changing element 20 and an imaging element 30 . The lens assembly 10 includes a housing 11 and an optical element 12 for receiving light from a photographed scene. The optical element 12 is provided on the casing 11 . The optical path changing element 20 is provided on the casing 11 . The imaging element 30 is provided on the housing 11 .
其中,成像元件30设于壳体11的侧周。光路改变元件20能够改变透过光学元件12的光线的传播方向,并使改变传播方向后的光线被成像元件30所接收。Among them, the imaging element 30 is provided on the side circumference of the casing 11 . The optical path changing element 20 can change the propagation direction of the light passing through the optical element 12 , and make the light after changing the propagation direction to be received by the imaging element 30 .
与未设置反射镜的拍摄设备相比,上述实施例的拍摄装置101,光线依次经光学元件12、光路改变元件20到达成像元件30,如此能够减小第一镜头模组100的厚度,进而减小拍摄装置101的厚度,有利于实现拍摄装置101的小型化。当该拍摄装置101应用于云台102时,能够减小云台102的收纳空间1024 沿拍摄装置101的厚度,进而减小云台102的连接支架的体积和重量,因而能够减小云台组件1001的体积和重量,减小云台102的电机的功耗,使得云台组件1001实现小型化、轻量化和便携性。当该云台组件1001应用于无人飞行器1002后,能够使得搭载有云台组件1001的无人飞行器1002的重量和体积减小,能够减少无人飞行器1002的功耗,延长无人飞行器1002的使用时长,且便于实现小型化、轻量化和便携性。Compared with the photographing device without a reflector, in the photographing device 101 of the above-mentioned embodiment, the light reaches the imaging element 30 through the optical element 12 and the optical path changing element 20 in sequence, so that the thickness of the first lens module 100 can be reduced, thereby reducing the thickness of the first lens module 100 . The small thickness of the photographing device 101 is beneficial to realize the miniaturization of the photographing device 101 . When the photographing device 101 is applied to the gimbal 102, the thickness of the storage space 1024 of the gimbal 102 along the photographing device 101 can be reduced, thereby reducing the volume and weight of the connecting bracket of the gimbal 102, thereby reducing the assembly of the gimbal The volume and weight of 1001 reduce the power consumption of the motor of the pan/tilt 102, so that the pan/tilt assembly 1001 can achieve miniaturization, light weight and portability. When the gimbal assembly 1001 is applied to the unmanned aerial vehicle 1002, the weight and volume of the unmanned aerial vehicle 1002 equipped with the gimbal assembly 1001 can be reduced, the power consumption of the unmanned aerial vehicle 1002 can be reduced, and the life of the unmanned aerial vehicle 1002 can be prolonged. It can be used for a long time, and it is easy to achieve miniaturization, light weight and portability.
此外,与光线依次经反射镜(对应光路改变元件20)和透镜组(对应光学元件12)到达成像传感器(对应成像元件30)的拍摄设备相比,本申请实施例的拍摄装置101,光线经光学元件12汇聚后到达光路改变元件20,如此能够减小光路改变元件20的尺寸和重量,从而减小拍摄装置101的宽度和厚度,有利于实现拍摄装置101的小型化。当该拍摄装置101应用于云台102时,能够减小云台102的收纳空间1024的尺寸,进而减小云台102的连接支架的体积和重量,因而能够减小云台组件1001的体积和重量,减小云台102的电机的功耗,使得云台组件1001实现小型化、轻量化和便携性。当该云台组件1001应用于无人飞行器1002后,能够使得搭载有云台组件1001的无人飞行器1002的重量和体积减小,能够减少无人飞行器1002的功耗,延长无人飞行器1002的使用时长,且便于实现小型化、轻量化和便携性。In addition, compared with the photographing device in which the light reaches the imaging sensor (corresponding to the imaging element 30 ) through the reflector (corresponding to the optical path changing element 20 ) and the lens group (corresponding to the optical element 12 ) in sequence, the photographing device 101 of the embodiment of the present application, the light passing through The optical elements 12 converge to reach the optical path changing element 20 , which can reduce the size and weight of the optical path changing element 20 , thereby reducing the width and thickness of the photographing device 101 , which is conducive to realizing the miniaturization of the photographing device 101 . When the photographing device 101 is applied to the pan-tilt 102, the size of the storage space 1024 of the pan-tilt 102 can be reduced, thereby reducing the volume and weight of the connecting bracket of the pan-tilt 102, thereby reducing the volume and weight of the pan-tilt assembly 1001. The weight reduces the power consumption of the motor of the pan/tilt 102, so that the pan/tilt assembly 1001 can achieve miniaturization, light weight and portability. When the gimbal assembly 1001 is applied to the unmanned aerial vehicle 1002, the weight and volume of the unmanned aerial vehicle 1002 equipped with the gimbal assembly 1001 can be reduced, the power consumption of the unmanned aerial vehicle 1002 can be reduced, and the life of the unmanned aerial vehicle 1002 can be prolonged. It can be used for a long time, and it is easy to achieve miniaturization, light weight and portability.
示例性地,拍摄装置101的厚度延伸方向与拍摄装置101的宽度延伸方向大致垂直。Exemplarily, the thickness extending direction of the photographing device 101 is substantially perpendicular to the width extending direction of the photographing device 101 .
示例性地,请参阅图3,拍摄装置101的厚度延伸方向如图3和图4中的Y方向所示。Illustratively, referring to FIG. 3 , the thickness extension direction of the photographing device 101 is shown in the Y direction in FIG. 3 and FIG. 4 .
示例性地,拍摄装置101的厚度延伸方向与入射至第一镜头模组100的光线平行。Exemplarily, the extending direction of the thickness of the photographing device 101 is parallel to the light incident to the first lens module 100 .
示例性地,拍摄装置101的厚度延伸方向与入射至光学元件12的光轴平行。Exemplarily, the thickness extension direction of the photographing device 101 is parallel to the optical axis incident to the optical element 12 .
示例性地,拍摄装置101的厚度延伸方向与横滚轴电机10221的横滚轴平行或者重合。Exemplarily, the thickness extension direction of the photographing device 101 is parallel to or coincident with the roll axis of the roll axis motor 10221 .
示例性地,俯仰轴电机10211的数量为两个,两个俯仰轴电机10211间隔设置。拍摄装置101夹设于两个俯仰轴电机10211之间。示例性地,拍摄装置101的宽度延伸方向平行于两个俯仰轴电机10211的排列方向。Exemplarily, the number of pitch axis motors 10211 is two, and the two pitch axis motors 10211 are arranged at intervals. The photographing device 101 is sandwiched between two pitch axis motors 10211 . Exemplarily, the width extension direction of the photographing device 101 is parallel to the arrangement direction of the two pitch axis motors 10211 .
请参阅图3,示例性地,拍摄装置101的宽度延伸方向与俯仰轴电机10211 的俯仰轴平行。Referring to FIG. 3 , for example, the width extension direction of the photographing device 101 is parallel to the pitch axis of the pitch axis motor 10211 .
示例性地,拍摄装置101的宽度延伸方向如图3和图4中的X方向所示。Exemplarily, the width extension direction of the photographing device 101 is shown in the X direction in FIGS. 3 and 4 .
示例性地,入射至光学元件12的光线与横滚轴电机10221的横滚轴平行。Illustratively, the light incident to the optical element 12 is parallel to the roll axis of the roll axis motor 10221 .
示例性地,光学元件12的光轴与横滚轴电机10221的横滚轴平行或者重合。Illustratively, the optical axis of the optical element 12 is parallel to or coincident with the roll axis of the roll axis motor 10221 .
请参阅图3,在一些实施例中,拍摄装置101还包括外壳301。第一镜头模组100设于外壳301内。当拍摄装置101与云台102连接时,外壳301连接于俯仰轴组件1021、横滚轴组件1022、航向轴组件1023中任意一个。Referring to FIG. 3 , in some embodiments, the photographing device 101 further includes a housing 301 . The first lens module 100 is disposed in the casing 301 . When the photographing device 101 is connected to the gimbal 102 , the housing 301 is connected to any one of the pitch axis assembly 1021 , the roll axis assembly 1022 , and the pan axis assembly 1023 .
可以理解地,当第一镜头模组100的尺寸减小时,外壳301的尺寸和重量也能够相应减小。It can be understood that when the size of the first lens module 100 is reduced, the size and weight of the housing 301 can also be correspondingly reduced.
请参阅图5,在一些实施例中,光学元件12的光轴与成像元件30平行。如此,能够减小第一镜头模组100的厚度,由此减小外壳301的厚度和重量,因而能够减小拍摄装置101的厚度,有利于实现拍摄装置101的小型化、轻量化和便携性。当该拍摄装置101应用于云台102时,本实施例的拍摄装置101能够进一步减小云台102的连接支架的体积和重量,减小云台102的电机的功耗。当搭载有该拍摄装置101的云台102应用于无人飞行器1002时,能够进一步减小搭载有云台102的无人飞行器1002的重量和体积,减少无人飞行器1002的功耗,延长无人飞行器1002的使用时长。Referring to FIG. 5 , in some embodiments, the optical axis of the optical element 12 is parallel to the imaging element 30 . In this way, the thickness of the first lens module 100 can be reduced, thereby reducing the thickness and weight of the housing 301 , and thus the thickness of the photographing device 101 can be reduced, which is beneficial to realize the miniaturization, light weight and portability of the photographing device 101 . When the photographing device 101 is applied to the gimbal 102 , the photographing device 101 of this embodiment can further reduce the volume and weight of the connecting bracket of the gimbal 102 and reduce the power consumption of the motor of the gimbal 102 . When the gimbal 102 equipped with the photographing device 101 is applied to the unmanned aerial vehicle 1002, the weight and volume of the unmanned aerial vehicle 1002 equipped with the gimbal 102 can be further reduced, the power consumption of the unmanned aerial vehicle 1002 can be reduced, and the unmanned aerial vehicle 1002 can be extended. The duration of use of aircraft 1002.
请参阅图4和图5,成像元件30与光学元件12垂直。示例性地,成像元件30沿第一方向的延伸方向与光学元件12垂直。如此,能够减小拍摄装置101的厚度,进而减小外壳301的厚度和重量,有利于实现拍摄装置101的小型化、轻量化和便携性。当该拍摄装置101应用于云台102时,本实施例的拍摄装置101能够进一步减小云台102的连接支架的体积和重量,减小云台102的电机的功耗。当搭载有该拍摄装置101的云台102应用于无人飞行器1002时,能够进一步减小搭载有云台102的无人飞行器1002的重量和体积,减小无人飞行器1002的功耗,延长无人飞行器1002的使用时长。Referring to FIGS. 4 and 5 , the imaging element 30 is perpendicular to the optical element 12 . Illustratively, the extending direction of the imaging element 30 in the first direction is perpendicular to the optical element 12 . In this way, the thickness of the photographing device 101 can be reduced, and the thickness and weight of the casing 301 can be reduced, which is beneficial to realize the miniaturization, weight reduction and portability of the photographing device 101 . When the photographing device 101 is applied to the gimbal 102 , the photographing device 101 of this embodiment can further reduce the volume and weight of the connecting bracket of the gimbal 102 and reduce the power consumption of the motor of the gimbal 102 . When the gimbal 102 carrying the photographing device 101 is applied to the unmanned aerial vehicle 1002, the weight and volume of the unmanned aerial vehicle 1002 carrying the gimbal 102 can be further reduced, the power consumption of the unmanned aerial vehicle 1002 can be reduced, and the unmanned aerial vehicle 1002 can be extended. The duration of use of the human aircraft 1002 .
请参阅图2和图3,在一些实施例中,当拍摄装置101与云台102连接时,拍摄装置101连接于俯仰轴组件1021、横滚轴组件1022、航向轴组件1023中任意一个,成像元件30垂直于与拍摄装置101连接的俯仰轴组件1021、横滚轴组件1022或航向轴组件1023。Referring to FIG. 2 and FIG. 3 , in some embodiments, when the photographing device 101 is connected to the gimbal 102 , the photographing device 101 is connected to any one of the pitch axis assembly 1021 , the roll axis assembly 1022 , and the pan axis assembly 1023 , and the imaging The element 30 is perpendicular to the pitch axis assembly 1021 , the roll axis assembly 1022 or the pan axis assembly 1023 connected to the camera 101 .
比如,拍摄装置101连接于俯仰轴组件1021,成像元件30垂直于俯仰轴 组件1021的俯仰轴。For example, the photographing device 101 is connected to the pitch axis assembly 1021, and the imaging element 30 is perpendicular to the pitch axis of the pitch axis assembly 1021.
又如,拍摄装置101连接于横滚轴组件1022,成像元件30垂直于横滚轴组件1022的横滚轴。For another example, the photographing device 101 is connected to the roll axis assembly 1022 , and the imaging element 30 is perpendicular to the roll axis of the roll axis assembly 1022 .
再如,拍摄装置101连接于航向轴组件1023,成像元件30垂直于航向轴组件1023的航向轴。For another example, the photographing device 101 is connected to the pan axis assembly 1023 , and the imaging element 30 is perpendicular to the pan axis of the pan axis assembly 1023 .
请参阅图2,在一些实施例中,拍摄装置101固定连接于俯仰轴组件1021,成像元件30与俯仰轴组件1021的俯仰轴电机10211的俯仰轴垂直。如此,能够使得拍摄装置101的重心尽可能地接近于俯仰轴组件1021的俯仰轴、横滚轴组件1022的俯仰轴和航向轴组件1023的航向轴中的至少一者,节省云台102的电机的功耗,延长云台102的电机的使用时长。Referring to FIG. 2 , in some embodiments, the photographing device 101 is fixedly connected to the pitch axis assembly 1021 , and the imaging element 30 is perpendicular to the pitch axis of the pitch axis motor 10211 of the pitch axis assembly 1021 . In this way, the center of gravity of the photographing device 101 can be as close as possible to at least one of the pitch axis of the pitch axis assembly 1021 , the pitch axis of the roll axis assembly 1022 , and the pan axis of the pan axis assembly 1023 , saving the motor of the gimbal 102 The power consumption of the pan/tilt head 102 is increased, and the usage time of the motor of the gimbal 102 is prolonged.
示例性地,拍摄装置101可以通过可拆卸连接方式或者不可拆卸连接方式固定连接于俯仰轴电机10211的转动部分上。Exemplarily, the photographing device 101 may be fixedly connected to the rotating part of the pitch axis motor 10211 in a detachable connection manner or a non-detachable connection manner.
俯仰轴电机10211的俯仰轴可以是实轴也可以是虚轴,在此不作限制。示例性地,俯仰轴电机10211的俯仰轴的延伸方向如图3中的虚线P所示。当拍摄装置101与云台102组装后,成像元件30与虚线P垂直。The pitch axis of the pitch axis motor 10211 may be a real axis or an imaginary axis, which is not limited here. Exemplarily, the extension direction of the pitch axis of the pitch axis motor 10211 is shown by the dotted line P in FIG. 3 . After the photographing device 101 is assembled with the pan/tilt head 102 , the imaging element 30 is perpendicular to the dotted line P. As shown in FIG.
可以理解地,第一部件与第二部件垂直,包括第一部件与第二部件之间的夹角为80°、85°、90°以及80°-90°之间的任意其他合适角度的情况。It can be understood that the first part is perpendicular to the second part, including the case where the included angle between the first part and the second part is 80°, 85°, 90° and any other suitable angle between 80°-90° .
第三部件与第四部件平行,包括第三部件与第四部件之间的夹角为0°、5°、10°以及0°-10°之间的任意其他合适角度的情况。The third part is parallel to the fourth part, including the case where the included angle between the third part and the fourth part is 0°, 5°, 10° and any other suitable angle between 0°-10°.
在一些实施例中,光路改变元件20可以通过任意合适的固定结构与镜头组件10固定连接,比如光路改变元件20通过胶粘结构、卡扣结构、快拆件结构等中的至少一种与镜头组件10固定连接。In some embodiments, the optical path changing element 20 may be fixedly connected to the lens assembly 10 through any suitable fixing structure, for example, the optical path changing element 20 is connected to the lens through at least one of an adhesive structure, a snap-fit structure, a quick-release structure, etc. The assembly 10 is fixedly connected.
示例性地,成像元件30包括成像传感器,其利用光电器件的光电转换功能,将其感光面上接收到的光信号转换为与光信号对应的电信号。Exemplarily, the imaging element 30 includes an imaging sensor, which utilizes the photoelectric conversion function of the photoelectric device to convert the optical signal received on the photosensitive surface thereof into an electrical signal corresponding to the optical signal.
请参阅图4和图5,在一些实施例中,拍摄装置101还包括第二镜头模组200。第一镜头模组100与第二镜头模组200连接,第二镜头模组200的拍摄参数不同于第一镜头模组100的拍摄参数。Referring to FIGS. 4 and 5 , in some embodiments, the photographing device 101 further includes a second lens module 200 . The first lens module 100 is connected to the second lens module 200 , and the shooting parameters of the second lens module 200 are different from the shooting parameters of the first lens module 100 .
示例性地,拍摄参数包括焦距、视角等中的至少一种。Exemplarily, the shooting parameters include at least one of focal length, angle of view, and the like.
示例性地,第一镜头模组100的焦距与第二镜头模组200的焦距不同。Exemplarily, the focal length of the first lens module 100 is different from the focal length of the second lens module 200 .
示例性地,第一镜头模组100为长焦镜头模组,第二镜头模组200为短焦 镜头模组。光线经第一镜头模组100的镜头组件10、光路改变元件20到达成像元件30,能够减小第一镜头模组100的厚度,使得第一镜头模组100的厚度尽可能地接近于第二镜头模组200的厚度,从而减小第一镜头模组100和第二镜头模组200组装后的厚度,并减小外壳301的厚度和重量,进而减小拍摄装置101的体积,有利于实现拍摄装置101的小型化。Exemplarily, the first lens module 100 is a telephoto lens module, and the second lens module 200 is a short-focus lens module. The light reaches the imaging element 30 through the lens assembly 10 and the optical path changing element 20 of the first lens module 100, which can reduce the thickness of the first lens module 100, so that the thickness of the first lens module 100 is as close as possible to that of the second lens module 100. The thickness of the lens module 200 can reduce the thickness of the first lens module 100 and the second lens module 200 after assembly, and reduce the thickness and weight of the housing 301, thereby reducing the volume of the photographing device 101, which is conducive to the realization of Miniaturization of the imaging device 101 .
当该拍摄装置101应用于云台102时,本实施例的拍摄装置101能够进一步减小云台102的连接支架的体积和重量,减小云台102的电机的功耗。当搭载有该拍摄装置101的云台102应用于无人飞行器1002时,能够进一步减小搭载有云台102的无人飞行器1002的重量和体积,减少无人飞行器1002的功耗,延长无人飞行器1002的使用时长。When the photographing device 101 is applied to the gimbal 102 , the photographing device 101 of this embodiment can further reduce the volume and weight of the connecting bracket of the gimbal 102 and reduce the power consumption of the motor of the gimbal 102 . When the gimbal 102 equipped with the photographing device 101 is applied to the unmanned aerial vehicle 1002, the weight and volume of the unmanned aerial vehicle 1002 equipped with the gimbal 102 can be further reduced, the power consumption of the unmanned aerial vehicle 1002 can be reduced, and the unmanned aerial vehicle 1002 can be extended. The duration of use of aircraft 1002.
在其他实施例中,第二镜头模组200的拍摄参数与第一镜头模组100的拍摄参数也可以相同。In other embodiments, the shooting parameters of the second lens module 200 and the shooting parameters of the first lens module 100 may also be the same.
示例性地,第二镜头模组200设于外壳301内。Exemplarily, the second lens module 200 is arranged in the housing 301 .
示例性地,第一镜头模组100可以通过卡扣结构、快拆件结构、胶粘层等于第二镜头模组200固定连接或者可拆卸连接。Exemplarily, the first lens module 100 may be fixedly connected or detachably connected to the second lens module 200 through a buckle structure, a quick-release structure, and an adhesive layer.
在一些实施例中,光学元件12的光轴平行于第二镜头模组200的光轴。示例性地,光学元件12的光轴平行于第二镜头模组200的进光方向。In some embodiments, the optical axis of the optical element 12 is parallel to the optical axis of the second lens module 200 . Exemplarily, the optical axis of the optical element 12 is parallel to the light incoming direction of the second lens module 200 .
在一些实施例中,光学元件12的进光方向与第二镜头模组200的进光方向相同。请参阅图5和图6,示例性地,光学元件12的进光方向与第二镜头模组200的进光方向相同包括:光学元件12的进光方向与第二镜头模组200的进光方向平行。图5和图6等图中带箭头的虚线代表光线。In some embodiments, the light entering direction of the optical element 12 is the same as the light entering direction of the second lens module 200 . Please refer to FIGS. 5 and 6 . Exemplarily, the light entering direction of the optical element 12 is the same as the light entering direction of the second lens module 200 , including: the light entering direction of the optical element 12 is the same as the light entering direction of the second lens module 200 . direction is parallel. The dashed lines with arrows in Figures 5 and 6 and the like represent light rays.
示例性地,请参阅图5和图6,入射至第一镜头模组100的光线的光轴与入射至第二镜头模组200的光线的光轴在Z方向的投影大致重合,以减小第一镜头模组100与第二镜头模组200的耦合偏差,保证拍摄装置101的成像质量。5 and 6 , the optical axis of the light incident to the first lens module 100 and the projection of the optical axis of the light incident to the second lens module 200 in the Z direction are substantially coincident to reduce The coupling deviation between the first lens module 100 and the second lens module 200 ensures the imaging quality of the photographing device 101 .
在一些实施例中,光学元件12的进光方向与第二镜头模组200的进光方向不同。示例性地,光学元件12的进光方向与第二镜头模组200的进光方向之间的夹角为锐角、钝角或者直角,在此不作限制。In some embodiments, the light entering direction of the optical element 12 is different from the light entering direction of the second lens module 200 . Exemplarily, the included angle between the light entering direction of the optical element 12 and the light entering direction of the second lens module 200 is an acute angle, an obtuse angle or a right angle, which is not limited herein.
请参阅图4,在一些实施例中,第一镜头模组100和第二镜头模组200沿第一方向堆叠设置。成像元件30设于镜头组件10的第一侧13或者第二侧14。第一侧13与第二侧14为镜头组件10沿第二方向的相对两侧,第一方向与第二 方向不同。Referring to FIG. 4 , in some embodiments, the first lens module 100 and the second lens module 200 are stacked along the first direction. The imaging element 30 is provided on the first side 13 or the second side 14 of the lens assembly 10 . The first side 13 and the second side 14 are opposite sides of the lens assembly 10 along a second direction, which is different from the second direction.
上述实施例的拍摄装置101,能够减小第一镜头模组100的沿第一方向的尺寸和第二方向的尺寸,从而减小第一镜头模组100和第二镜头模组200组装后沿第一方向的尺寸和第二方向的尺寸,并减小外壳301的尺寸和重量,拍摄装置101的结构紧凑、空间利用率高,进而减小拍摄装置101的体积和重量,有利于实现拍摄装置101的小型化。The photographing device 101 of the above-mentioned embodiment can reduce the size of the first lens module 100 along the first direction and the size of the second direction, thereby reducing the rear edge of the assembly of the first lens module 100 and the second lens module 200. The size of the first direction and the size of the second direction, and the size and weight of the housing 301 are reduced, the structure of the photographing device 101 is compact, and the space utilization rate is high, thereby reducing the volume and weight of the photographing device 101, which is beneficial to the realization of the photographing device. 101 miniaturization.
当该拍摄装置101应用于云台102时,本实施例的拍摄装置101能够进一步减小云台102的连接支架的体积和重量,减小云台102的电机的功耗。当搭载有该拍摄装置101的云台102应用于无人飞行器1002时,能够进一步减小搭载有云台102的无人飞行器1002的重量和体积,减少无人飞行器1002的功耗,延长无人飞行器1002的使用时长。When the photographing device 101 is applied to the gimbal 102 , the photographing device 101 of this embodiment can further reduce the volume and weight of the connecting bracket of the gimbal 102 and reduce the power consumption of the motor of the gimbal 102 . When the gimbal 102 equipped with the photographing device 101 is applied to the unmanned aerial vehicle 1002, the weight and volume of the unmanned aerial vehicle 1002 equipped with the gimbal 102 can be further reduced, the power consumption of the unmanned aerial vehicle 1002 can be reduced, and the unmanned aerial vehicle 1002 can be extended. The duration of use of aircraft 1002.
示例性地,第一方向与第二方向相交。示例性地,第一方向与第二方向垂直。Illustratively, the first direction intersects the second direction. Illustratively, the first direction is perpendicular to the second direction.
示例性地,第一方向如图3和图4中的Z方向所示,第二方向如图3和图4中的X方向所示。Exemplarily, the first direction is shown as the Z direction in FIGS. 3 and 4 , and the second direction is shown as the X direction in FIGS. 3 and 4 .
示例性地,第一方向如图3和图4中的X方向所示。第二方向如图3和图4中的Z方向所示。Exemplarily, the first direction is shown as the X direction in FIGS. 3 and 4 . The second direction is shown as the Z direction in FIGS. 3 and 4 .
在一些实施例中,第一方向为上下方向,第二方向为左右方向。示例性地,以图4中的Z方向的箭头方向为上,与Z方向的箭头方向相反的方向为下。以图4中的X方向的箭头方向为左,与X方向的箭头方向相反的方向为右。In some embodiments, the first direction is an up-down direction, and the second direction is a left-right direction. Exemplarily, the direction of the arrow in the Z direction in FIG. 4 is upward, and the direction opposite to the direction of the arrow in the Z direction is downward. The direction of the arrow in the X direction in FIG. 4 is the left, and the direction opposite to the direction of the arrow in the X direction is the right.
在一些实施例中,第一方向为左右方向,第二方向为上下方向。In some embodiments, the first direction is a left-right direction, and the second direction is an up-down direction.
请参阅图4,在一些实施例中,第二镜头模组200的顶部设有用于容置至少部分第一镜头模组100的第一容置槽201。第一容置槽201形成于第二镜头模组200的顶部。如此,能够减小第一镜头模组100与第二镜头模组200组装后沿第一方向(比如Z方向)的尺寸,从而减小外壳301的重量和沿第一方向的尺寸,进而减小拍摄装置101的体积和重量,以更好地适用于云台102或者无人飞行器1002。Referring to FIG. 4 , in some embodiments, the top of the second lens module 200 is provided with a first accommodating groove 201 for accommodating at least part of the first lens module 100 . The first accommodating groove 201 is formed on the top of the second lens module 200 . In this way, the size along the first direction (such as the Z direction) after the first lens module 100 and the second lens module 200 are assembled can be reduced, thereby reducing the weight of the housing 301 and the size along the first direction, thereby reducing the The volume and weight of the photographing device 101 are better suited for the gimbal 102 or the unmanned aerial vehicle 1002 .
示例性地,第一镜头模组100或者拍摄装置101沿图4中的Z方向的尺寸定义为高度。Exemplarily, the dimension of the first lens module 100 or the photographing device 101 along the Z direction in FIG. 4 is defined as the height.
示例性地,拍摄装置101的高度延伸方向、厚度延伸方向、宽度延伸方向 两两垂直。Exemplarily, the height extending direction, the thickness extending direction, and the width extending direction of the photographing device 101 are perpendicular to each other.
可以理解地,本申请实施例的拍摄装置101不限于第一镜头模组100和第二镜头模组200堆叠设计。比如,还可以设置第三镜头模组和/或其他镜头模组等,第一镜头模组100、第二镜头模组200和第三镜头模组堆叠设置。It can be understood that the photographing device 101 in the embodiment of the present application is not limited to the stacking design of the first lens module 100 and the second lens module 200 . For example, a third lens module and/or other lens modules may also be provided, and the first lens module 100 , the second lens module 200 and the third lens module are stacked and arranged.
可以理解地,壳体11的侧周包括第一侧13所在侧的表面和/或第二侧14所在侧的表面。It can be understood that the side circumference of the housing 11 includes the surface on the side where the first side 13 is located and/or the surface on the side where the second side 14 is located.
请参阅图4和图5,在一些实施例中,拍摄装置101还包括电路板302。第一镜头模组100和第二镜头模组200均连接至同一个电路板302,用于处理第一镜头模组100与第二镜头模组200发送的信号。Referring to FIG. 4 and FIG. 5 , in some embodiments, the photographing device 101 further includes a circuit board 302 . The first lens module 100 and the second lens module 200 are both connected to the same circuit board 302 for processing signals sent by the first lens module 100 and the second lens module 200 .
与第一镜头模组100和第二镜头模组200分别与不同的基板连接相比,本实施例的拍摄装置101能够减少拍摄装置101的结构件的数量,减小外壳301的体积和重量,从而进一步减小拍摄装置101的尺寸和重量。当该拍摄装置101应用于云台102时,能够减小云台102的收纳空间1024的大小,进而减小云台102的连接支架的体积和重量,因而能够减小云台组件1001的体积和重量,减小云台102的电机的功耗,使得云台组件1001实现小型化、轻量化和便携性。当该云台组件1001应用于无人飞行器1002后,能够使得搭载有云台组件1001的无人飞行器1002的重量和体积减小,能够减少无人飞行器1002的功耗,延长无人飞行器1002的使用时长,且便于实现小型化、轻量化和便携性。Compared with the first lens module 100 and the second lens module 200 being connected to different substrates, the photographing device 101 of this embodiment can reduce the number of structural components of the photographing device 101 and reduce the volume and weight of the housing 301 . Thereby, the size and weight of the photographing device 101 are further reduced. When the photographing device 101 is applied to the pan-tilt 102, the size of the storage space 1024 of the pan-tilt 102 can be reduced, thereby reducing the volume and weight of the connecting bracket of the pan-tilt 102, thereby reducing the volume and weight of the pan-tilt assembly 1001. The weight reduces the power consumption of the motor of the pan/tilt 102, so that the pan/tilt assembly 1001 can achieve miniaturization, light weight and portability. When the gimbal assembly 1001 is applied to the unmanned aerial vehicle 1002, the weight and volume of the unmanned aerial vehicle 1002 equipped with the gimbal assembly 1001 can be reduced, the power consumption of the unmanned aerial vehicle 1002 can be reduced, and the life of the unmanned aerial vehicle 1002 can be prolonged. It can be used for a long time, and it is easy to achieve miniaturization, light weight and portability.
示例性地,电路板302与成像元件30电连接,用于对成像元件30转换得到的电信号进行处理,以实现拍摄装置101的拍照或者录像功能。Exemplarily, the circuit board 302 is electrically connected to the imaging element 30 for processing the electrical signal converted by the imaging element 30 to realize the photographing or video recording function of the photographing device 101 .
可以理解地,电路板302通信连接于云台102或者无人飞行器1002的主控板(图未示)。云台102或者无人飞行器1002可以通过主控板与电路板302进行通信,从而控制拍摄装置101工作,或者接收拍摄装置101的拍摄信息。Understandably, the circuit board 302 is communicatively connected to the gimbal 102 or the main control board (not shown) of the unmanned aerial vehicle 1002 . The gimbal 102 or the unmanned aerial vehicle 1002 can communicate with the circuit board 302 through the main control board, so as to control the operation of the photographing device 101 or receive the photographing information of the photographing device 101 .
示例性地,主控板可以设于云台102上,也可以设于无人飞行器1002上,在此不作限制。Exemplarily, the main control board may be provided on the gimbal 102, or may be provided on the unmanned aerial vehicle 1002, which is not limited herein.
请参阅图4,在一些实施例中,电路板302和成像元件30设于第一镜头模组100与第二镜头模组200所形成的组装体的相对两侧。第一镜头模组100与第二镜头模组200装配后形成组装体。电路板302和成像元件30设于该组装体的相对两侧,以使得拍摄装置101的结构紧凑,减小拍摄装置101的体积,以更好地适用于云台102或者无人飞行器1002。Referring to FIG. 4 , in some embodiments, the circuit board 302 and the imaging element 30 are disposed on opposite sides of the assembly formed by the first lens module 100 and the second lens module 200 . The first lens module 100 and the second lens module 200 are assembled to form an assembly. The circuit board 302 and the imaging element 30 are disposed on opposite sides of the assembly, so that the structure of the photographing device 101 is compact and the volume of the photographing device 101 is reduced, so as to be more suitable for the pan/tilt head 102 or the unmanned aerial vehicle 1002 .
此外,电路板302和成像元件30设于第一镜头模组100与第二镜头模组200所形成的组装体的相对两侧,能够平衡拍摄装置101的重心,使得拍摄装置101的重心尽可能地接近于俯仰轴组件1021的俯仰轴、横滚轴组件1022的俯仰轴和航向轴组件1023的航向轴中的至少一者,节省云台102的电机的功耗,延长云台102的电机的使用时长。In addition, the circuit board 302 and the imaging element 30 are disposed on opposite sides of the assembly formed by the first lens module 100 and the second lens module 200 , which can balance the center of gravity of the photographing device 101 , so that the center of gravity of the photographing device 101 is as large as possible. It is close to at least one of the pitch axis of the pitch axis assembly 1021, the pitch axis of the roll axis assembly 1022, and the pan axis of the pan axis assembly 1023, which saves the power consumption of the motor of the gimbal 102 and prolongs the power consumption of the motor of the gimbal 102. duration of use.
请参阅图2和图3,电路板302与云台102中与拍摄装置101固定连接的电机的转轴垂直。如此,能够使得拍摄装置101的重心尽可能地接近于俯仰轴组件1021的俯仰轴、横滚轴组件1022的俯仰轴和航向轴组件1023的航向轴中的至少一者,节省云台102的电机的功耗,延长云台102的电机的使用时长。Please refer to FIG. 2 and FIG. 3 , the circuit board 302 is perpendicular to the rotation axis of the motor in the pan/tilt head 102 that is fixedly connected to the photographing device 101 . In this way, the center of gravity of the photographing device 101 can be as close as possible to at least one of the pitch axis of the pitch axis assembly 1021 , the pitch axis of the roll axis assembly 1022 , and the pan axis of the pan axis assembly 1023 , saving the motor of the gimbal 102 The power consumption of the pan/tilt head 102 is increased, and the usage time of the motor of the gimbal 102 is prolonged.
示例性地,俯仰轴电机10211与拍摄装置101固定连接。电路板302与俯仰轴电机10211的俯仰轴垂直。Exemplarily, the pitch axis motor 10211 is fixedly connected to the photographing device 101 . The circuit board 302 is perpendicular to the pitch axis of the pitch axis motor 10211 .
请参阅图7,在一些实施例中,拍摄装置101还包括第一连接结构400和第二连接结构500。第一连接结构400连接于电路板302和第一镜头模组100。第二连接结构500连接于电路板302和第二镜头模组200。第一连接结构400和第二连接结构500均连接于同一个电路板302上。Referring to FIG. 7 , in some embodiments, the photographing device 101 further includes a first connection structure 400 and a second connection structure 500 . The first connection structure 400 is connected to the circuit board 302 and the first lens module 100 . The second connection structure 500 is connected to the circuit board 302 and the second lens module 200 . Both the first connection structure 400 and the second connection structure 500 are connected to the same circuit board 302 .
与第一连接结构400和第二连接结构500分别与不同的基板连接相比,本实施例的拍摄装置101能够减少拍摄装置101的结构件的数量,减小外壳301的体积和重量,从而进一步减小拍摄装置101的尺寸和重量,以更好地适用于云台102或者无人飞行器1002。Compared with the first connection structure 400 and the second connection structure 500 being connected to different substrates, the photographing device 101 of this embodiment can reduce the number of structural parts of the photographing device 101 and the volume and weight of the housing 301 , thereby further reducing the size and weight of the housing 301 . The size and weight of the photographing device 101 are reduced so as to be more suitable for the gimbal 102 or the unmanned aerial vehicle 1002 .
请参阅图7,第一连接结构400包括第一柔性连接件401和第二柔性连接件402。第一柔性连接件401连接于电路板302和镜头组件10的电机。第二柔性连接件402连接于电路板302和成像元件30。Referring to FIG. 7 , the first connecting structure 400 includes a first flexible connecting member 401 and a second flexible connecting member 402 . The first flexible connector 401 is connected to the circuit board 302 and the motor of the lens assembly 10 . The second flexible connector 402 is connected to the circuit board 302 and the imaging element 30 .
请参阅图7,第二连接结构500包括第三柔性连接件501、第四柔性连接件502和第五柔性连接件503。第三柔性连接件501连接于电路板302和第二镜头模组200的成像构件。第四柔性连接件502连接于电路板302和第二镜头模组200的镜头的电机。第二镜头模组200的镜头的光圈和/或电子快门通过第四柔性连接件502和第五柔性连接件503连接于电路板302。Referring to FIG. 7 , the second connecting structure 500 includes a third flexible connecting member 501 , a fourth flexible connecting member 502 and a fifth flexible connecting member 503 . The third flexible connector 501 is connected to the circuit board 302 and the imaging member of the second lens module 200 . The fourth flexible connector 502 is connected to the circuit board 302 and the motor of the lens of the second lens module 200 . The aperture and/or the electronic shutter of the lens of the second lens module 200 are connected to the circuit board 302 through the fourth flexible connector 502 and the fifth flexible connector 503 .
其中,第一柔性连接件401、第二柔性连接件402、第三柔性连接件501、第四柔性连接件502均连接在同一个电路板302上,第四柔性连接件502与第五柔性连接件503连接。如此,能够实现第一镜头模组100和第二镜头模组200 均连接至同一个电路板302,以减少拍摄装置101的结构件的数量,减小外壳301的体积和重量,从而进一步减小拍摄装置101的尺寸和重量,以更好地适用于云台102或者无人飞行器1002。The first flexible connector 401, the second flexible connector 402, the third flexible connector 501, and the fourth flexible connector 502 are all connected to the same circuit board 302, and the fourth flexible connector 502 is connected to the fifth flexible connector Piece 503 is connected. In this way, both the first lens module 100 and the second lens module 200 can be connected to the same circuit board 302, so as to reduce the number of structural components of the photographing device 101, reduce the volume and weight of the housing 301, and further reduce the The size and weight of the photographing device 101 are better suited for the gimbal 102 or the unmanned aerial vehicle 1002 .
请参阅图8,示例性地,电路板302上设有第一电连接部3021、第二电连接部3022、第三电连接部3023和第四电连接部3024。第四柔性连接件502上形成有第五电连接部5021。第一电连接部3021与第一柔性连接件401连接,以使得电路板302能够电连接于镜头组件10的电机。第二电连接部3022与第二柔性连接件402连接,以使得电路板302能够与成像元件30电连接。第三电连接部3023与第三柔性连接件501连接,以使得电路板302能够与第二镜头模组200的成像构件电连接。Referring to FIG. 8 , for example, the circuit board 302 is provided with a first electrical connection part 3021 , a second electrical connection part 3022 , a third electrical connection part 3023 and a fourth electrical connection part 3024 . A fifth electrical connecting portion 5021 is formed on the fourth flexible connecting member 502 . The first electrical connection portion 3021 is connected to the first flexible connection member 401 so that the circuit board 302 can be electrically connected to the motor of the lens assembly 10 . The second electrical connection portion 3022 is connected to the second flexible connection member 402 so that the circuit board 302 can be electrically connected to the imaging element 30 . The third electrical connection portion 3023 is connected to the third flexible connection member 501 , so that the circuit board 302 can be electrically connected to the imaging member of the second lens module 200 .
第四电连接部3024与第四柔性连接件502连接,以使得电路板302能够与第二镜头模组200的镜头的电机电连接。第五电连接部5021与第五柔性连接件503连接,从而实现第四柔性连接件502与第五柔性连接件503电连接,进而实现电路板302电连接于第二镜头模组200的镜头的光圈和/或电子快门。The fourth electrical connection portion 3024 is connected to the fourth flexible connection member 502 , so that the circuit board 302 can be electrically connected to the motor of the lens of the second lens module 200 . The fifth electrical connection portion 5021 is connected with the fifth flexible connecting member 503, so as to realize the electrical connection between the fourth flexible connecting member 502 and the fifth flexible connecting member 503, and further realize the electrical connection between the circuit board 302 and the lens of the second lens module 200. Aperture and/or electronic shutter.
可以理解地,第二镜头模组200的成像构件的功能与第一镜头模组100的成像元件30相同。It can be understood that the function of the imaging member of the second lens module 200 is the same as that of the imaging element 30 of the first lens module 100 .
示例性地,第一柔性连接件401、第二柔性连接件402、第三柔性连接件501、第四柔性连接件502和第五柔性连接件503均包括柔性电路板、柔性电缆等中的至少一者。Exemplarily, the first flexible connector 401, the second flexible connector 402, the third flexible connector 501, the fourth flexible connector 502, and the fifth flexible connector 503 each include at least one of a flexible circuit board, a flexible cable, and the like. one.
请参阅图5,光路改变元件20包括第一反射镜21。示例性地,光线依次经光学元件12和第一反射镜21到达成像元件30,如此,在光路设计能够使得第一镜头模组100沿Y方向(如图4)的尺寸较小的前提下,尽可能地减少光路改变元件20的结构件数量,从而尽可能地减小外壳301的体积和重量,进而尽可能地减小拍摄装置101的尺寸和重量,以更好地适用于云台102或者无人飞行器1002。Referring to FIG. 5 , the optical path changing element 20 includes a first reflecting mirror 21 . Exemplarily, the light reaches the imaging element 30 through the optical element 12 and the first reflecting mirror 21 in turn. In this way, under the premise that the optical path design can make the size of the first lens module 100 along the Y direction (as shown in FIG. 4 ) smaller, The number of structural parts of the optical path changing element 20 is reduced as much as possible, so as to reduce the volume and weight of the housing 301 as much as possible, thereby reducing the size and weight of the photographing device 101 as much as possible, so as to be better applicable to the pan/tilt head 102 or Unmanned aerial vehicle 1002.
请参阅4和图5,第一反射镜21的反射面与光学元件12的光轴之间具有第一夹角。第一反射镜21的反射面与成像元件30的光轴之间具有第二夹角。第一夹角为45°;和/或,第二夹角为45°。Please refer to FIG. 4 and FIG. 5 , there is a first included angle between the reflection surface of the first reflecting mirror 21 and the optical axis of the optical element 12 . There is a second included angle between the reflection surface of the first reflection mirror 21 and the optical axis of the imaging element 30 . The first included angle is 45°; and/or the second included angle is 45°.
可以理解地,在其他实施例中,第一夹角和第二夹角也可以根据实际需求进行设计,比如第一夹角和第二夹角均为锐角(如0°-90°之间的其他任意合 适角度)。比如,第一夹角为30°,第二夹角为60°。It can be understood that, in other embodiments, the first included angle and the second included angle can also be designed according to actual requirements, for example, the first included angle and the second included angle are both acute angles (eg, between 0°-90°). any other suitable angle). For example, the first included angle is 30°, and the second included angle is 60°.
示例性地,入射至第一反射镜21的反射面的光线的光轴与第一反射镜21的反射面之间的夹角为锐角,比如为10°、30°、45°、60°、80°以及10°-80°之间的任意其他合适角度。Exemplarily, the included angle between the optical axis of the light incident on the reflective surface of the first reflective mirror 21 and the reflective surface of the first reflective mirror 21 is an acute angle, such as 10°, 30°, 45°, 60°, 80° and any other suitable angle between 10°-80°.
示例性地,从第一反射镜21的反射面射出的光线的光轴与第一反射镜21的反射面之间的夹角为锐角,比如为10°、30°、45°、60°、80°以及10°-80°之间的任意其他合适角度。Exemplarily, the included angle between the optical axis of the light emitted from the reflective surface of the first reflective mirror 21 and the reflective surface of the first reflective mirror 21 is an acute angle, such as 10°, 30°, 45°, 60°, 80° and any other suitable angle between 10°-80°.
示例性地,从第一反射镜21的反射面射出的光线的光轴与成像元件30之间的夹角为锐角,比如为10°、30°、45°、60°、80°以及10°-80°之间的任意其他合适角度。Exemplarily, the included angle between the optical axis of the light emitted from the reflective surface of the first reflecting mirror 21 and the imaging element 30 is an acute angle, such as 10°, 30°, 45°, 60°, 80° and 10° Any other suitable angle between -80°.
请参阅图9,在一些实施例中,光路改变元件20包括第二反射镜22和第一棱镜23。第二反射镜22设于壳体11上。第一棱镜23设于壳体11上。光线依次经第二反射镜22、光学元件12、第一棱镜23到达成像元件30。如此,能够尽可能地减小第一镜头模组100的厚度,从而尽可能地减小外壳301的体积和重量,进而尽可能地减小拍摄装置101的尺寸和重量,以更好地适用于云台102或者无人飞行器1002。Referring to FIG. 9 , in some embodiments, the optical path changing element 20 includes a second mirror 22 and a first prism 23 . The second reflector 22 is provided on the casing 11 . The first prism 23 is disposed on the casing 11 . The light reaches the imaging element 30 through the second reflecting mirror 22 , the optical element 12 and the first prism 23 in sequence. In this way, the thickness of the first lens module 100 can be reduced as much as possible, thereby reducing the volume and weight of the housing 301 as much as possible, and further reducing the size and weight of the photographing device 101 as much as possible, so as to be better suited for The gimbal 102 or the unmanned aerial vehicle 1002 .
示例性地,第一镜头模组100的厚度延伸方向如图9中的沿X1方向。Exemplarily, the thickness extension direction of the first lens module 100 is along the X1 direction as shown in FIG. 9 .
示例性地,第一镜头模组100的厚度延伸方向与入射至第一镜头模组100的光线的光轴平行。Exemplarily, the thickness extension direction of the first lens module 100 is parallel to the optical axis of the light incident to the first lens module 100 .
请参阅图9,在一些实施例中,光学元件12的光轴与成像元件30平行。如此,第一镜头模组100的结构紧凑、光路设计合理,以减小拍摄装置101的尺寸,从而更好地适用于云台102或者无人飞行器1002。Referring to FIG. 9 , in some embodiments, the optical axis of the optical element 12 is parallel to the imaging element 30 . In this way, the structure of the first lens module 100 is compact and the optical path design is reasonable, so as to reduce the size of the photographing device 101 , so as to be more suitable for the gimbal 102 or the unmanned aerial vehicle 1002 .
请参阅图9,第二反射镜22的反射面与光学元件12的光轴之间的夹角为锐角。比如,第二反射镜22的反射面与光学元件12的光轴之间的夹角为10°、30°、45°、60°、80°以及10°-80°之间的任意其他合适角度。Referring to FIG. 9 , the included angle between the reflecting surface of the second reflecting mirror 22 and the optical axis of the optical element 12 is an acute angle. For example, the included angle between the reflective surface of the second mirror 22 and the optical axis of the optical element 12 is 10°, 30°, 45°, 60°, 80° and any other suitable angle between 10°-80° .
请参阅图9,第二镜头模组200的顶部和侧部分别设有相互连通的第二容置槽202和第三容置槽203,光学元件12设于第二容置槽202内,第二容置槽202和第三容置槽203均容置有部分壳体11。Please refer to FIG. 9 , the top and the side of the second lens module 200 are respectively provided with a second accommodating groove 202 and a third accommodating groove 203 that communicate with each other, and the optical element 12 is disposed in the second accommodating groove 202 . Both the second accommodating groove 202 and the third accommodating groove 203 accommodate part of the casing 11 .
示例性地,以图9中的Z1方向的箭头方向为上,与Z1方向的箭头方向相反的方向为下。第二容置槽202形成于第二镜头模组200的顶部。光学元件12 设于第二容置槽202内,减小第一镜头模组100与第二镜头模组200组装后的高度,从而减小外壳301的重量和高度。Exemplarily, the direction of the arrow in the Z1 direction in FIG. 9 is up, and the direction opposite to the arrow direction in the Z1 direction is down. The second accommodating groove 202 is formed on the top of the second lens module 200 . The optical element 12 is disposed in the second accommodating groove 202 to reduce the height of the assembled first lens module 100 and the second lens module 200 , thereby reducing the weight and height of the housing 301 .
第三容置槽203的设置,能够减小第一镜头模组100与第二镜头模组200组装后的宽度,从而减小外壳301的重量和宽度。因而,第一容置槽201和第二容置槽202能够有效减小拍摄装置101的体积和重量,以更好地适用于云台102或者无人飞行器1002。The arrangement of the third accommodating groove 203 can reduce the width of the assembled first lens module 100 and the second lens module 200 , thereby reducing the weight and width of the housing 301 . Therefore, the first accommodating slot 201 and the second accommodating slot 202 can effectively reduce the volume and weight of the photographing device 101 , so as to be more suitable for the pan/tilt head 102 or the unmanned aerial vehicle 1002 .
请参阅图9,示例性地,第一镜头模组100和/或第二镜头模组200的高度延伸方向与图9中Z1平行。Referring to FIG. 9 , for example, the height extending direction of the first lens module 100 and/or the second lens module 200 is parallel to Z1 in FIG. 9 .
请参阅图9,示例性地,第一镜头模组100和/或第二镜头模组200的宽度延伸方向与图9中Y1平行。Referring to FIG. 9 , for example, the width extension direction of the first lens module 100 and/or the second lens module 200 is parallel to Y1 in FIG. 9 .
请参阅图9,第三容置槽203从第二镜头模组200的顶部延伸至底部,成像元件30至少部分设于第三容置槽203内并位于第三容置槽203靠近底部的一侧。如此,第一镜头模组100的结构紧凑,光路设计合理,以减小拍摄装置101的尺寸,从而更好地适用于云台102或者无人飞行器1002。Please refer to FIG. 9 , the third accommodating groove 203 extends from the top to the bottom of the second lens module 200 , and the imaging element 30 is at least partially disposed in the third accommodating groove 203 and is located at a position near the bottom of the third accommodating groove 203 side. In this way, the structure of the first lens module 100 is compact, and the optical path design is reasonable, so as to reduce the size of the photographing device 101 , so as to be more suitable for the gimbal 102 or the unmanned aerial vehicle 1002 .
请参阅图9,第一棱镜23包括依次相连的第一侧面231、第二侧面232和第三侧面233,第一侧面231与第三侧面233垂直。光线依次经光学元件12、第一侧面231、第二侧面232、第三侧面233到达成像元件30,以使得第一镜头模组100的结构紧凑,减小拍摄装置101的尺寸,从而更好地适用于云台102或者无人飞行器1002。Referring to FIG. 9 , the first prism 23 includes a first side surface 231 , a second side surface 232 and a third side surface 233 connected in sequence, and the first side surface 231 is perpendicular to the third side surface 233 . The light reaches the imaging element 30 through the optical element 12, the first side 231, the second side 232, and the third side 233 in sequence, so that the structure of the first lens module 100 is compact, the size of the photographing device 101 is reduced, and the Applicable to the gimbal 102 or the unmanned aerial vehicle 1002 .
请参阅图9,第一侧面231与成像元件30垂直,第三侧面233与成像元件30平行。示例性地,第一侧面231与第三侧面233垂直。第一侧面231与第二侧面232之间的夹角为锐角。第三侧面233与第二侧面232之间的夹角为锐角。如此,能够保证从光学元件12射出的光线能够到达成像元件30。Referring to FIG. 9 , the first side surface 231 is perpendicular to the imaging element 30 , and the third side surface 233 is parallel to the imaging element 30 . Exemplarily, the first side surface 231 is perpendicular to the third side surface 233 . The included angle between the first side surface 231 and the second side surface 232 is an acute angle. The included angle between the third side surface 233 and the second side surface 232 is an acute angle. In this way, it can be ensured that the light emitted from the optical element 12 can reach the imaging element 30 .
请参阅图10,在一些实施例中,光路改变元件20包括第二棱镜24和第三棱镜25。第二棱镜24设于壳体11上。第三棱镜25设于壳体11上。光路经光学元件12、第二棱镜24、第三棱镜25到达成像元件30。如此,能够减小第一镜头模组100的厚度,从而尽可能地减小外壳301的体积和重量,进而尽可能地减小拍摄装置101的尺寸和重量,以更好地适用于云台102或者无人飞行器1002。Referring to FIG. 10 , in some embodiments, the light path changing element 20 includes a second prism 24 and a third prism 25 . The second prism 24 is disposed on the casing 11 . The third prism 25 is disposed on the casing 11 . The light path reaches the imaging element 30 through the optical element 12 , the second prism 24 , and the third prism 25 . In this way, the thickness of the first lens module 100 can be reduced, so as to reduce the volume and weight of the housing 301 as much as possible, thereby reducing the size and weight of the photographing device 101 as much as possible, so as to be more suitable for the gimbal 102 Or UAV 1002.
示例性地,第一镜头模组100的厚度延伸方向如图10中的沿X2方向。Exemplarily, the thickness extension direction of the first lens module 100 is along the X2 direction as shown in FIG. 10 .
请参阅图10,在一些实施例中,光学元件12的光轴与成像元件30垂直。在其他实施例中,光学元件12的光轴与成像元件30也可以呈锐角设置。Referring to FIG. 10 , in some embodiments, the optical axis of the optical element 12 is perpendicular to the imaging element 30 . In other embodiments, the optical axis of the optical element 12 and the imaging element 30 may also be arranged at an acute angle.
请参阅图10,在一些实施例中,光学元件12、第二棱镜24、第三棱镜25和成像元件30设于第二镜头模组200的顶部,以合理利用第二镜头模组200的空间,减小第一镜头模组100与第二镜头模组200组装后的尺寸,从而减小外壳301的体积和重量,进而尽可能地减小拍摄装置101的尺寸和重量,以更好地适用于云台102或者无人飞行器1002。Please refer to FIG. 10 , in some embodiments, the optical element 12 , the second prism 24 , the third prism 25 and the imaging element 30 are arranged on the top of the second lens module 200 to make reasonable use of the space of the second lens module 200 , Reduce the size of the assembled first lens module 100 and the second lens module 200, thereby reducing the volume and weight of the housing 301, thereby reducing the size and weight of the photographing device 101 as much as possible, so as to be more suitable for The gimbal 102 or the unmanned aerial vehicle 1002 .
示例性地,以图10中的Z2方向的箭头方向为上,与Z2方向的箭头方向相反的方向为下。Exemplarily, the direction of the arrow in the Z2 direction in FIG. 10 is up, and the direction opposite to the arrow direction in the Z2 direction is down.
请参阅图10,在一些实施例中,第二镜头模组200的顶部设有第四容置槽204,第三棱镜25、成像元件30和壳体11均至少部分容置在第四容置槽204内。从而减小第一镜头模组100与第二镜头模组200组装后高度,从而减小外壳301的重量和厚度,进而有效减小拍摄装置101的体积和重量,以更好地适用于云台102或者无人飞行器1002。Referring to FIG. 10 , in some embodiments, the top of the second lens module 200 is provided with a fourth accommodating groove 204 , and the third prism 25 , the imaging element 30 and the casing 11 are all accommodated at least partially in the fourth accommodating groove 204. Therefore, the assembled height of the first lens module 100 and the second lens module 200 is reduced, thereby reducing the weight and thickness of the housing 301, thereby effectively reducing the volume and weight of the photographing device 101, so as to be more suitable for the gimbal 102 or unmanned aerial vehicle 1002.
请参阅图10,在一些实施例中,第二棱镜24包括依次相连的第四侧面241、第五侧面242和第六侧面243。第四侧面241与第六侧面243垂直,光线经光学元件12、第四侧面241、第五侧面242、第六侧面243到达第二棱镜24,从而保证从光学元件12射出的光线能够到达第二棱镜24。Referring to FIG. 10 , in some embodiments, the second prism 24 includes a fourth side surface 241 , a fifth side surface 242 and a sixth side surface 243 which are connected in sequence. The fourth side 241 is perpendicular to the sixth side 243, and the light reaches the second prism 24 through the optical element 12, the fourth side 241, the fifth side 242, and the sixth side 243, thereby ensuring that the light emitted from the optical element 12 can reach the second prism 24. Prism 24.
请参阅图10,在一些实施例中,第三棱镜25包括依次相连的第七侧面251、第八侧面252和第九侧面253。第七侧面251与第九侧面253垂直,光线经第二棱镜24、第七侧面251、第八侧面252和第九侧面253到达成像元件30,从而保证从光学元件12射出的光线经第二棱镜24和第三棱镜25能够到达成像元件30。Referring to FIG. 10 , in some embodiments, the third prism 25 includes a seventh side surface 251 , an eighth side surface 252 and a ninth side surface 253 which are connected in sequence. The seventh side 251 is perpendicular to the ninth side 253, and the light reaches the imaging element 30 through the second prism 24, the seventh side 251, the eighth side 252 and the ninth side 253, thereby ensuring that the light emitted from the optical element 12 passes through the second prism 24 and the third prism 25 can reach the imaging element 30 .
请参阅图10,在一些实施例中,第四侧面241和第九侧面253均平行于成像元件30,并均垂直于光学元件12的光轴。如此,能够使得第一镜头模组100的光路折叠,减小第一镜头模组100的厚度,从而减小外壳301的重量和厚度,进而有效减小拍摄装置101的体积和重量,以更好地适用于云台102和者无人飞行器1002,减小云台102的电机控制的功耗和无人飞行器1002的功耗。Referring to FIG. 10 , in some embodiments, the fourth side surface 241 and the ninth side surface 253 are both parallel to the imaging element 30 and perpendicular to the optical axis of the optical element 12 . In this way, the optical path of the first lens module 100 can be folded, and the thickness of the first lens module 100 can be reduced, thereby reducing the weight and thickness of the housing 301 , thereby effectively reducing the volume and weight of the photographing device 101 to better It is suitable for the gimbal 102 and the unmanned aerial vehicle 1002 , and reduces the power consumption of the motor control of the gimbal 102 and the power consumption of the unmanned aerial vehicle 1002 .
示例性地,光学元件12包括至少一个透镜元件。Illustratively, the optical element 12 includes at least one lens element.
请参阅图11,光学元件12的侧周形成有切边121。如此,在保证光学元件 12的光学性能的情况下,尽可能地减小光学元件12的尺寸和重量,从而减小外壳301的重量和尺寸,进而有效减小拍摄装置101的体积和重量,以更好地适用于云台102和无人飞行器1002,减小云台102的电机控制的功耗和无人飞行器1002的功耗。Referring to FIG. 11 , a side perimeter of the optical element 12 is formed with a cut edge 121 . In this way, under the condition of ensuring the optical performance of the optical element 12, the size and weight of the optical element 12 are reduced as much as possible, thereby reducing the weight and size of the housing 301, thereby effectively reducing the volume and weight of the photographing device 101, so as to reduce the size and weight of the optical element 12 as much as possible. It is better applicable to the gimbal 102 and the unmanned aerial vehicle 1002 , and reduces the power consumption of the motor control of the gimbal 102 and the power consumption of the unmanned aerial vehicle 1002 .
示例性地,光学元件12的侧周包括光学元件12中非用于引导光线传播的周缘。Illustratively, the side perimeter of the optical element 12 includes the perimeter of the optical element 12 that is not used to direct light propagation.
示例性地,光学元件12上的切边121可以设置一个、两个、三个或者更多,在此不作限制。比如,光学元件12的侧周形成有两个切边121,两个切边121相对设置。Exemplarily, one, two, three or more of the cut edges 121 on the optical element 12 may be provided, which is not limited herein. For example, two cut edges 121 are formed on the side circumference of the optical element 12, and the two cut edges 121 are disposed opposite to each other.
可以理解地,第二镜头模组200的光学器件的侧周形成有切边121。如此,在保证光学元件12的光学性能的情况下,尽可能地减小光学器件的尺寸和重量,从而减小外壳301的重量和尺寸,进而有效减小拍摄装置101的体积和重量,以更好地适用于云台102或者无人飞行器1002。It can be understood that the side periphery of the optical device of the second lens module 200 is formed with a cut edge 121 . In this way, under the condition of ensuring the optical performance of the optical element 12, the size and weight of the optical device are reduced as much as possible, thereby reducing the weight and size of the housing 301, thereby effectively reducing the volume and weight of the photographing device 101, so as to be more Well suited for the gimbal 102 or the unmanned aerial vehicle 1002 .
示例性地,光学器件的功能与光学元件12的功能大致相同。Illustratively, the function of the optical device is substantially the same as that of the optical element 12 .
切边121的形状可以根据实际需求进行设计,比如为平面、曲面、跑道形等。The shape of the cut edge 121 can be designed according to actual requirements, such as a plane, a curved surface, a racetrack shape, and the like.
本申请实施例还提供一种无人飞行器,包括无人飞行器主体和上述任一个实施例的云台组件。云台组件设于无人飞行器主体上。Embodiments of the present application further provide an unmanned aerial vehicle, including an unmanned aerial vehicle body and the pan/tilt assembly of any one of the foregoing embodiments. The gimbal assembly is arranged on the main body of the unmanned aerial vehicle.
无人飞行器可以为旋翼无人飞行器、固定翼无人飞行器、无人直升机或者固定翼-旋翼混合的无人飞行器等。其中,旋翼无人飞行器可为单旋翼无人飞行器或者多旋翼无人飞行器。多旋翼无人飞行器包括双旋翼飞行器、三旋翼飞行器、四旋翼飞行器、六旋翼飞行器、八旋翼飞行器、十旋翼飞行器、十二旋翼飞行器等。The unmanned aerial vehicle may be a rotary-wing unmanned aerial vehicle, a fixed-wing unmanned aerial vehicle, an unmanned helicopter, or a hybrid unmanned aerial vehicle of fixed-wing and rotary-wing. The rotor unmanned aerial vehicle may be a single-rotor unmanned aerial vehicle or a multi-rotor unmanned aerial vehicle. Multi-rotor UAVs include dual-rotor aircraft, tri-rotor aircraft, quad-rotor aircraft, hexa-rotor aircraft, octa-rotor aircraft, ten-rotor aircraft, twelve-rotor aircraft, etc.
示例性地,无人飞行器主体包括机身、动力系统。机身可以包括中心架以及与中心架连接的一个或多个机臂,一个或多个机臂呈辐射状从中心架延伸出。Illustratively, the UAV body includes a fuselage, a power system. The fuselage may include a center frame and one or more arms connected to the center frame, the one or more arms extending radially from the center frame.
示例性地,云台组件的云台与机身固定连接或者可拆卸连接。Exemplarily, the gimbal of the gimbal assembly is fixedly or detachably connected to the body.
示例性地,动力系统包括螺旋桨和电机,电机用于驱动螺旋桨旋转,从而为无人飞行器提供飞行动力。动力电机和螺旋桨设置在机臂上。Exemplarily, the power system includes a propeller and a motor, and the motor is used to drive the propeller to rotate, thereby providing flight power for the unmanned aerial vehicle. The power motor and propeller are arranged on the arm.
在本申请的描述中,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申请中的具体含义。In the description of this application, it should be noted that, unless otherwise expressly specified and limited, the terms "installed", "connected" and "connected" should be understood in a broad sense, for example, it may be a fixed connection or a detachable connection connected, or integrally connected. It can be a mechanical connection or an electrical connection. It can be directly connected, or indirectly connected through an intermediate medium, and it can be the internal communication between two elements or the interaction relationship between the two elements. For those of ordinary skill in the art, the specific meanings of the above terms in this application can be understood according to specific situations.
在本申请中,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。In this application, unless otherwise expressly specified and defined, a first feature "on" or "under" a second feature may include direct contact between the first and second features, or may include the first and second features Not directly but through additional features between them. Also, the first feature being "above", "over" and "above" the second feature includes the first feature being directly above and obliquely above the second feature, or simply means that the first feature is level higher than the second feature. The first feature is "below", "below" and "below" the second feature includes the first feature being directly below and diagonally below the second feature, or simply means that the first feature has a lower level than the second feature.
上文的公开提供了许多不同的实施方式或例子用来实现本申请的不同结构。为了简化本申请的公开,上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申请。此外,本申请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,本申请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。The above disclosure provides many different implementations or examples for implementing different structures of the present application. To simplify the disclosure of the present application, the components and arrangements of specific examples are described above. Of course, they are only examples and are not intended to limit the application. Furthermore, this application may repeat reference numerals and/or reference letters in different instances for the purpose of simplicity and clarity, and does not in itself indicate a relationship between the various embodiments and/or arrangements discussed. In addition, this application provides examples of various specific processes and materials, but one of ordinary skill in the art will recognize the application of other processes and/or the use of other materials.
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方法步骤、特征、结构、材料或者特点包含于本申请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,描述的具体方法步骤、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。In the description of this specification, reference to the terms "one embodiment," "some embodiments," "exemplary embodiment," "example," "specific example," or "some examples", etc., is meant to incorporate the embodiments The specific method steps, features, structures, materials or characteristics described by way of example or are included in at least one embodiment or example of the present application. In this specification, schematic representations of the above terms do not necessarily refer to the same embodiment or example. Furthermore, the particular method steps, features, structures, materials or characteristics described may be combined in any suitable manner in any one or more embodiments or examples.
以上所述,仅为本申请的具体实施方式,但本申请的保护范围并不局限于此,任何熟悉本技术领域的技术人员在本申请揭露的技术范围内,可轻易想到各种等效的修改或替换,这些修改或替换都应涵盖在本申请的保护范围之内。因此,本申请的保护范围应以权利要求的保护范围为准。The above are only specific embodiments of the present application, but the protection scope of the present application is not limited thereto. Any person skilled in the art can easily think of various equivalents within the technical scope disclosed in the present application. Modifications or substitutions shall be covered by the protection scope of this application. Therefore, the protection scope of the present application shall be subject to the protection scope of the claims.

Claims (41)

  1. 一种拍摄装置,其特征在于,所述拍摄装置用于与云台连接,所述云台搭载在无人飞行器上,所述无人飞行器经过所述云台控制所述拍摄装置的朝向;所述拍摄装置包括第一镜头模组,所述第一镜头模组包括:A photographing device, characterized in that the photographing device is used for connecting with a pan/tilt, the pan/tilt is mounted on an unmanned aerial vehicle, and the unmanned aerial vehicle controls the orientation of the photographing device through the pan/tilt; the The shooting device includes a first lens module, and the first lens module includes:
    镜头组件,包括壳体和用于接收来自拍摄场景的光线的光学元件,所述光学元件设于所述壳体上;a lens assembly, including a casing and an optical element for receiving light from a shooting scene, the optical element being arranged on the casing;
    光路改变元件,设于所述壳体上;an optical path changing element, arranged on the casing;
    成像元件,设于所述壳体上;an imaging element, arranged on the casing;
    其中,所述成像元件设于所述壳体的侧周;所述光路改变元件能够改变透过所述光学元件的光线的传播方向,并使改变传播方向后的光线被所述成像元件所接收。Wherein, the imaging element is arranged on the side circumference of the casing; the optical path changing element can change the propagation direction of the light passing through the optical element, and make the light after changing the propagation direction to be received by the imaging element .
  2. 根据权利要求1所述的拍摄装置,其特征在于,所述光学元件的光轴与所述成像元件平行。The photographing device according to claim 1, wherein the optical axis of the optical element is parallel to the imaging element.
  3. 根据权利要求1所述的拍摄装置,其特征在于,所述成像元件与所述光学元件垂直。The photographing device according to claim 1, wherein the imaging element is perpendicular to the optical element.
  4. 根据权利要求1-3任一项所述的拍摄装置,其特征在于,所述云台包括俯仰轴组件、横滚轴组件、航向轴组件中的至少一个,当所述拍摄装置与云台连接时,所述拍摄装置连接于俯仰轴组件、横滚轴组件、航向轴组件中任意一个,所述成像元件垂直于与所述拍摄装置连接的俯仰轴组件、横滚轴组件或航向轴组件;和/或,所述光路改变元件通过胶粘结构、卡扣结构中的至少一种与所述镜头组件固定连接。The photographing device according to any one of claims 1-3, wherein the pan/tilt head comprises at least one of a pitch axis assembly, a roll axis assembly, and a pan axis assembly, and when the photographing device is connected to the pan/tilt head When the photographing device is connected to any one of the pitch axis assembly, the roll axis assembly and the pan axis assembly, the imaging element is perpendicular to the pitch axis assembly, the roll axis assembly or the pan axis assembly connected to the photographing device; And/or, the optical path changing element is fixedly connected to the lens assembly through at least one of an adhesive structure and a snap structure.
  5. 根据权利要求1-4任一项所述的拍摄装置,其特征在于,所述拍摄装置还包括:The photographing device according to any one of claims 1-4, wherein the photographing device further comprises:
    第二镜头模组,所述第一镜头模组与所述第二镜头模组连接,所述第二镜头模组的拍摄参数不同于所述第一镜头模组的拍摄参数。A second lens module, the first lens module is connected to the second lens module, and the shooting parameters of the second lens module are different from the shooting parameters of the first lens module.
  6. 根据权利要求1-4任一项所述的拍摄装置,其特征在于,所述拍摄装置还包括第二镜头模组,所述第一镜头模组和所述第二镜头模组沿第一方向堆叠设置,所述成像元件设于所述镜头组件的第一侧或者第二侧,所述第一侧与所 述第二侧为所述镜头组件沿第二方向的相对两侧,所述第一方向与所述第二方向不同。The photographing device according to any one of claims 1-4, wherein the photographing device further comprises a second lens module, and the first lens module and the second lens module are along a first direction stacking arrangement, the imaging element is arranged on the first side or the second side of the lens assembly, the first side and the second side are opposite sides of the lens assembly along the second direction, the first side and the second side are opposite sides of the lens assembly along the second direction, the first One direction is different from the second direction.
  7. 根据权利要求6所述的拍摄装置,其特征在于,所述第一方向与所述第二方向垂直。The photographing device according to claim 6, wherein the first direction is perpendicular to the second direction.
  8. 根据权利要求6所述的拍摄装置,其特征在于,所述第一方向为上下方向,所述第二方向为左右方向;或者,所述第一方向为左右方向,所述第二方向为上下方向。The photographing device according to claim 6, wherein the first direction is an up-down direction, and the second direction is a left-right direction; or, the first direction is a left-right direction, and the second direction is an up-down direction direction.
  9. 根据权利要求5-8任一项所述的拍摄装置,其特征在于,所述第二镜头模组的顶部设有用于容置至少部分所述第一镜头模组的第一容置槽。The photographing device according to any one of claims 5-8, wherein the top of the second lens module is provided with a first accommodating groove for accommodating at least part of the first lens module.
  10. 根据权利要求5-8任一项所述的拍摄装置,其特征在于,所述拍摄装置还包括:The photographing device according to any one of claims 5-8, wherein the photographing device further comprises:
    电路板,所述第一镜头模组和所述第二镜头模组均连接至同一个所述电路板,用于处理所述第一镜头模组与所述第二镜头模组发送的信号。A circuit board, wherein the first lens module and the second lens module are both connected to the same circuit board for processing signals sent by the first lens module and the second lens module.
  11. 根据权利要求10所述的拍摄装置,其特征在于,所述电路板和所述成像元件设于所述第一镜头模组与所述第二镜头模组所形成的组装体的相对两侧。The photographing device according to claim 10, wherein the circuit board and the imaging element are disposed on opposite sides of the assembly formed by the first lens module and the second lens module.
  12. 根据权利要求10或11所述的拍摄装置,其特征在于,所述电路板与云台中与所述拍摄装置固定连接的电机的俯仰轴垂直。The photographing device according to claim 10 or 11, wherein the circuit board is perpendicular to a pitch axis of a motor in the pan/tilt head that is fixedly connected to the photographing device.
  13. 根据权利要求10-12任一项所述的拍摄装置,其特征在于,所述拍摄装置还包括:The photographing device according to any one of claims 10-12, wherein the photographing device further comprises:
    第一连接结构,连接于所述电路板和所述第一镜头模组;a first connection structure, connected to the circuit board and the first lens module;
    第二连接结构,连接于所述电路板和所述第二镜头模组,且所述第一连接结构和所述第二连接结构均连接于同一个所述电路板上。The second connection structure is connected to the circuit board and the second lens module, and the first connection structure and the second connection structure are both connected to the same circuit board.
  14. 根据权利要求13所述的拍摄装置,其特征在于,所述第一连接结构包括:The photographing device according to claim 13, wherein the first connection structure comprises:
    第一柔性连接件,连接于所述电路板和所述镜头组件的电机;a first flexible connector, connected to the circuit board and the motor of the lens assembly;
    第二柔性连接件,连接于所述电路板和所述成像元件。The second flexible connector is connected to the circuit board and the imaging element.
  15. 根据权利要求14所述的拍摄装置,其特征在于,所述第二连接结构包括:The photographing device according to claim 14, wherein the second connection structure comprises:
    第三柔性连接件,连接于所述电路板和所述第二镜头模组的成像构件;a third flexible connector connected to the circuit board and the imaging member of the second lens module;
    第四柔性连接件,连接于所述电路板和所述第二镜头模组的镜头的电机;a fourth flexible connector, connected to the circuit board and the motor of the lens of the second lens module;
    第五柔性连接件,所述第二镜头模组的镜头的光圈和/或电子快门通过所述第四柔性连接件和所述第五柔性连接件连接于所述电路板;a fifth flexible connector, wherein the aperture and/or electronic shutter of the lens of the second lens module is connected to the circuit board through the fourth flexible connector and the fifth flexible connector;
    其中,所述第一柔性连接件、所述第二柔性连接件、所述第三柔性连接件和所述第四柔性连接件均连接在同一个所述电路板上,第四柔性连接件与第五柔性连接件连接。Wherein, the first flexible connecting piece, the second flexible connecting piece, the third flexible connecting piece and the fourth flexible connecting piece are all connected on the same circuit board, and the fourth flexible connecting piece is connected to the same circuit board. The fifth flexible connector is connected.
  16. 根据权利要求1-15任一项所述的拍摄装置,其特征在于,所述光路改变元件包括第一反射镜。The photographing device according to any one of claims 1-15, wherein the optical path changing element comprises a first reflecting mirror.
  17. 根据权利要求16所述的拍摄装置,其特征在于,所述第一反射镜的反射面与所述光学元件的光轴之间具有第一夹角,所述第一反射镜的反射面与所述成像元件的光轴之间具有第二夹角,所述第一夹角为45°;和/或,所述第二夹角为45°。The photographing device according to claim 16, wherein a first included angle exists between the reflection surface of the first reflection mirror and the optical axis of the optical element, and the reflection surface of the first reflection mirror and the optical axis of the optical element have a first included angle. There is a second included angle between the optical axes of the imaging elements, and the first included angle is 45°; and/or the second included angle is 45°.
  18. 根据权利要求5-15任一项所述的拍摄装置,其特征在于,所述光路改变元件包括:The photographing device according to any one of claims 5-15, wherein the optical path changing element comprises:
    第二反射镜,设于所述壳体上;a second reflector, arranged on the casing;
    第一棱镜,设于所述壳体上,光线依次经所述第二反射镜、所述光学元件、所述第一棱镜到达所述成像元件。The first prism is arranged on the casing, and the light reaches the imaging element through the second reflecting mirror, the optical element and the first prism in sequence.
  19. 根据权利要求18所述的拍摄装置,其特征在于,所述光学元件的光轴与所述成像元件平行。The photographing device according to claim 18, wherein the optical axis of the optical element is parallel to the imaging element.
  20. 根据权利要求18或19所述的拍摄装置,其特征在于,所述第二反射镜的反射面与所述光学元件的光轴之间的夹角为锐角。The photographing device according to claim 18 or 19, wherein the included angle between the reflection surface of the second reflecting mirror and the optical axis of the optical element is an acute angle.
  21. 根据权利要求18-20任一项所述的拍摄装置,其特征在于,所述第二镜头模组的顶部和侧部分别设有相互连通的第二容置槽和第三容置槽,所述光学元件设于所述第二容置槽内,所述第二容置槽和所述第三容置槽均容置有部分所述壳体。The photographing device according to any one of claims 18-20, wherein the top and the side of the second lens module are respectively provided with a second accommodating groove and a third accommodating groove that communicate with each other, so The optical element is arranged in the second accommodating groove, and both the second accommodating groove and the third accommodating groove accommodate part of the casing.
  22. 根据权利要求21所述的拍摄装置,其特征在于,所述第三容置槽从所述第二镜头模组的顶部延伸至底部,所述成像元件至少部分设于所述第三容置槽内并位于所述第三容置槽靠近所述底部的一侧。The photographing device according to claim 21, wherein the third accommodating groove extends from the top to the bottom of the second lens module, and the imaging element is at least partially disposed in the third accommodating groove inside and located on the side of the third accommodating groove close to the bottom.
  23. 根据权利要求18-22任一项所述的拍摄装置,其特征在于,所述第一棱镜包括依次相连的第一侧面、第二侧面和第三侧面,所述第一侧面与所述第三侧面垂直,光线依次经所述光学元件、所述第一侧面、所述第二侧面、所述 第三侧面到达所述成像元件。The photographing device according to any one of claims 18-22, wherein the first prism comprises a first side surface, a second side surface and a third side surface which are connected in sequence, and the first side surface and the third side surface are connected in sequence. The side surfaces are vertical, and the light reaches the imaging element sequentially through the optical element, the first side surface, the second side surface, and the third side surface.
  24. 根据权利要求23所述的拍摄装置,其特征在于,所述第一侧面与所述成像元件垂直,所述第三侧面与所述成像元件平行。The photographing device according to claim 23, wherein the first side surface is perpendicular to the imaging element, and the third side surface is parallel to the imaging element.
  25. 根据权利要求5-15任一项所述的拍摄装置,其特征在于,所述光路改变元件包括:The photographing device according to any one of claims 5-15, wherein the optical path changing element comprises:
    第二棱镜,设于所述壳体上;a second prism, arranged on the casing;
    第三棱镜,设于所述壳体上;光路经所述光学元件、所述第二棱镜、所述第三棱镜到达所述成像元件。The third prism is arranged on the casing; the light path reaches the imaging element through the optical element, the second prism, and the third prism.
  26. 根据权利要求25所述的拍摄装置,其特征在于,所述光学元件的光轴与所述成像元件垂直。The photographing device according to claim 25, wherein the optical axis of the optical element is perpendicular to the imaging element.
  27. 根据权利要求25或26所述的拍摄装置,其特征在于,所述光学元件、所述第二棱镜、所述第三棱镜和所述成像元件设于所述第二镜头模组的顶部。The photographing device according to claim 25 or 26, wherein the optical element, the second prism, the third prism and the imaging element are arranged on the top of the second lens module.
  28. 根据权利要求25-27任一项所述的拍摄装置,其特征在于,所述第二镜头模组的顶部设有第四容置槽,所述第三棱镜、所述成像元件和所述壳体均至少部分容置在所述第四容置槽内。The photographing device according to any one of claims 25-27, wherein a fourth accommodating groove is provided on the top of the second lens module, the third prism, the imaging element and the casing are at least partially accommodated in the fourth accommodating groove.
  29. 根据权利要求25-28任一项所述的拍摄装置,其特征在于,所述第二棱镜包括依次相连的第四侧面、第五侧面和第六侧面,所述第四侧面与所述第六侧面垂直,光线经所述光学元件、所述第四侧面、所述第五侧面、所述第六侧面到达所述第二棱镜。The photographing device according to any one of claims 25-28, wherein the second prism comprises a fourth side surface, a fifth side surface and a sixth side surface which are connected in sequence, and the fourth side surface is connected to the sixth side surface. The side surfaces are vertical, and the light reaches the second prism through the optical element, the fourth side surface, the fifth side surface, and the sixth side surface.
  30. 根据权利要求29所述的拍摄装置,其特征在于,所述第三棱镜包括依次相连的第七侧面、第八侧面和第九侧面,所述第七侧面与所述第九侧面垂直,光线经所述第二棱镜、所述第七侧面、所述第八侧面和所述第九侧面到达所述成像元件。The photographing device according to claim 29, wherein the third prism comprises a seventh side surface, an eighth side surface and a ninth side surface which are connected in sequence, the seventh side surface is perpendicular to the ninth side surface, and the light passes through the The second prism, the seventh side, the eighth side and the ninth side reach the imaging element.
  31. 根据权利要求30所述的拍摄装置,其特征在于,所述第四侧面和所述第九侧面均平行于所述成像元件,并均垂直于所述光学元件的光轴。The photographing device according to claim 30, wherein the fourth side surface and the ninth side surface are both parallel to the imaging element, and both are perpendicular to the optical axis of the optical element.
  32. 根据权利要求1-31任一项所述的拍摄装置,其特征在于,所述光学元件的侧周形成有切边;和/或,所述拍摄装置包括第二镜头模组,所述第二镜头模组的光学器件的侧周形成有切边。The photographing device according to any one of claims 1-31, characterized in that, a side circumference of the optical element is formed with a cut edge; and/or, the photographing device comprises a second lens module, the second lens module The side periphery of the optical device of the lens module is formed with a cut edge.
  33. 根据权利要求5-31任一项所述的拍摄装置,其特征在于,所述光学元件的光轴平行于所述第二镜头模组的光轴。The photographing device according to any one of claims 5-31, wherein the optical axis of the optical element is parallel to the optical axis of the second lens module.
  34. 根据权利要求5-31任一项所述的拍摄装置,其特征在于,所述光学元件的进光方向与所述第二镜头模组的进光方向相同。The photographing device according to any one of claims 5-31, wherein the light entering direction of the optical element is the same as the light entering direction of the second lens module.
  35. 根据权利要求5-31任一项所述的拍摄装置,其特征在于,所述光学元件的进光方向与所述第二镜头模组的进光方向不同。The photographing device according to any one of claims 5-31, wherein the light entering direction of the optical element is different from the light entering direction of the second lens module.
  36. 根据权利要求5-31任一项所述的拍摄装置,其特征在于,所述拍摄参数包括焦距、视角中的至少一种。The photographing device according to any one of claims 5-31, wherein the photographing parameter includes at least one of a focal length and a viewing angle.
  37. 一种云台组件,其特征在于,包括:A pan-tilt assembly, comprising:
    云台;以及PTZ; and
    1-36任一项所述的拍摄装置,搭载于所述云台上。The imaging device according to any one of 1-36, which is mounted on the platform.
  38. 根据权利要求37所述的云台组件,其特征在于,所述云台包括俯仰轴组件、横滚轴组件和航向轴组件中的至少一者,用于驱动所述拍摄装置运动。The pan/tilt assembly according to claim 37, wherein the pan/tilt comprises at least one of a pitch axis assembly, a roll axis assembly and a pan axis assembly for driving the camera to move.
  39. 根据权利要求38所述的云台组件,其特征在于,所述拍摄装置固定连接于所述俯仰轴组件,所述成像元件与所述俯仰轴组件的俯仰轴电机的俯仰轴垂直。The pan/tilt assembly according to claim 38, wherein the photographing device is fixedly connected to the pitch axis assembly, and the imaging element is perpendicular to the pitch axis of the pitch axis motor of the pitch axis assembly.
  40. 一种无人飞行器,其特征在于,包括:A kind of unmanned aerial vehicle, is characterized in that, comprises:
    无人飞行器主体;以及the body of the unmanned aerial vehicle; and
    权利要求37-39任一项所述的云台组件,设于所述无人飞行器主体上。The pan/tilt assembly according to any one of claims 37-39, provided on the main body of the unmanned aerial vehicle.
  41. 一种无人飞行器套件,其特征在于,包括:An unmanned aerial vehicle kit, comprising:
    无人飞行器;以及unmanned aerial vehicles; and
    权利要求37-39任一项所述的云台组件,用于设于所述无人飞行器上。The pan/tilt assembly according to any one of claims 37-39, which is used to be installed on the unmanned aerial vehicle.
PCT/CN2020/142437 2020-12-31 2020-12-31 Photographing device, gimbal assembly, unmanned aerial vehicle and unmanned aerial vehicle kit WO2022141537A1 (en)

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US20090284644A1 (en) * 2008-05-12 2009-11-19 Flir Systems, Inc. Optical Payload with Folded Telescope and Cryocooler
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US20090284644A1 (en) * 2008-05-12 2009-11-19 Flir Systems, Inc. Optical Payload with Folded Telescope and Cryocooler
CN107941204A (en) * 2016-10-07 2018-04-20 莱卡地球系统公开股份有限公司 Flight sensor
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