WO2019028871A1 - Frame assembly and unmanned aerial vehicle - Google Patents

Frame assembly and unmanned aerial vehicle Download PDF

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Publication number
WO2019028871A1
WO2019028871A1 PCT/CN2017/097188 CN2017097188W WO2019028871A1 WO 2019028871 A1 WO2019028871 A1 WO 2019028871A1 CN 2017097188 W CN2017097188 W CN 2017097188W WO 2019028871 A1 WO2019028871 A1 WO 2019028871A1
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WO
WIPO (PCT)
Prior art keywords
frame
support
support frame
center frame
center
Prior art date
Application number
PCT/CN2017/097188
Other languages
French (fr)
Chinese (zh)
Inventor
任冠男
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.)
Filing date
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/CN2017/097188 priority Critical patent/WO2019028871A1/en
Priority to CN201780005218.8A priority patent/CN108698706B/en
Publication of WO2019028871A1 publication Critical patent/WO2019028871A1/en

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Classifications

    • 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
    • B64CAEROPLANES; HELICOPTERS
    • B64C25/00Alighting gear
    • B64C25/02Undercarriages
    • B64C25/08Undercarriages non-fixed, e.g. jettisonable
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U10/00Type of UAV
    • B64U10/10Rotorcrafts
    • B64U10/13Flying platforms
    • B64U10/14Flying platforms with four distinct rotor axes, e.g. quadcopters
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U2101/00UAVs specially adapted for particular uses or applications
    • B64U2101/30UAVs specially adapted for particular uses or applications for imaging, photography or videography

Definitions

  • the present invention relates to the field of aircraft, and in particular to a rack assembly and a drone.
  • the drone can be used for aerial photography.
  • the fuselage of the drone is provided with a landing gear, and the landing gear supports the drone on the ground when the drone is landing.
  • the landing gear will block the camera's line of sight, affecting the camera's shooting range, and it is difficult to achieve 360-degree shooting.
  • Embodiments of the present invention provide a rack assembly and a drone.
  • the rack including a center frame, and a stand that is movably coupled to the center frame;
  • a support frame movably coupled to the stand, the support frame for carrying a load of the drone
  • connection mechanism of the support frame and the center frame Connecting a connection mechanism of the support frame and the center frame, the support frame being movably connected to the center frame by the connection mechanism, so that the support frame can be lifted and lowered relative to the center frame;
  • the tripod includes a support end for contacting the landing surface; when the support end is raised, the tripod drives the support frame to descend relative to the center frame, when the support end is lowered, The tripod drives the support frame to rise relative to the center frame;
  • the support frame drives the support end to descend
  • the connecting mechanism drives the support frame to descend relative to the center frame.
  • the support frame drives the support end to rise.
  • the support end of the stand when the support frame is lowered, the support end of the stand is raised, and when the support frame is raised, the support end of the stand is lowered, and the camera device can be mounted to the support frame.
  • the camera device When the drone is in a navigation state, the camera device is supported by the support device.
  • the frame is lowered away from the center frame, and the support end of the stand is raised close to the center frame, so that the support end of the stand does not block the line of sight of the camera when shooting, so as to achieve 360-degree shooting.
  • a power assembly mounted on the frame assembly for providing flight power.
  • the support frame when the support frame is lowered, the support end of the tripod is raised, and when the support frame is raised, the support end of the tripod is lowered, and the camera device can be mounted to the support frame.
  • the camera device When the drone is in a navigation state, the camera device is supported by the support device.
  • Rack away from the center The support end of the tripod rises close to the center frame, so that the support end of the tripod does not block the line of sight of the camera when shooting, so as to achieve 360-degree shooting.
  • FIG. 1 is a perspective view of a drone according to an embodiment of the present invention when the support frame is away from the center frame;
  • FIG. 2 is a schematic plan view of the drone of the embodiment of the present invention when the support frame is away from the center frame;
  • FIG 3 is another schematic plan view of the drone of the embodiment of the present invention when the support frame is away from the center frame;
  • FIG. 4 is a top plan view of the drone of the embodiment of the present invention when the support frame is away from the center frame;
  • FIG. 5 is a perspective view of the drone of the embodiment of the present invention when the support frame is close to the center frame;
  • FIG. 6 is a schematic plan view of the drone of the embodiment of the present invention when the support frame is close to the center frame;
  • FIG. 7 is another schematic plan view of the drone of the embodiment of the present invention when the support frame is close to the center frame;
  • Figure 8 is a bottom plan view of the drone of the embodiment of the present invention with the support frame near the center frame.
  • UAV 100 rack assembly 10, frame 12, center frame 122, stand 124, support end 1242, connection end 1244, support frame 14, connection mechanism 16, link 162, first sub-rod 1622, second The sub-rod 1624, the connecting rod 17, the extension bracket 18, the arm 19, the power unit 20, the propeller 22, the pan-tilt unit 40, the pan/tilt head 42, the shaft mechanism 422, and the camera unit 200.
  • the first feature "on” or “under” the second feature may be a direct contact of the first and second features, or the first and second features may be indirectly through an intermediate medium, unless otherwise explicitly stated and defined. contact.
  • the first feature "above”, “above” and “above” the second feature may be that the first feature is directly above or above the second feature, or only It is only indicated that the first feature level is higher than the second feature.
  • the first feature “below”, “below” and “below” the second feature may be that the first feature is directly below or obliquely below the second feature, or merely that the first feature level is less than the second feature.
  • the rack assembly 10 of the embodiment of the present invention includes a frame 12 , a support frame 14 , and a connecting mechanism 16 .
  • the frame 12 includes a center frame 122 and a stand 124 movably coupled to the center frame 122 .
  • the support frame 14 is movably coupled to the stand 124 for carrying the load of the drone 100.
  • the connecting mechanism 16 connects the support frame 14 and the center frame 122.
  • the support frame 14 is movably connected to the center frame 122 through the connecting mechanism 16 to enable the support frame 14 to be lifted and lowered relative to the center frame 122.
  • the stand 124 includes a support end 1242 for contacting the landing surface.
  • the stand 124 drives the support frame 14 to descend relative to the center frame 122.
  • the stand 124 drives the support frame 14 to rise relative to the center frame 122; or, when the connecting mechanism 16 drives the support
  • the support frame 14 drives the support end 1242 to descend.
  • the connecting mechanism 16 drives the support frame 14 to descend relative to the center frame 122, the support frame 14 drives the support end 1242 to rise.
  • the support end 1242 of the stand 124 is raised, and when the support frame 14 is raised, the support end 1242 of the stand 124 is lowered, and the camera device 200 can be mounted to the support frame 14 as a drone.
  • the camera 200 is lowered away from the center frame 122 with the support frame 14, and the support end 1242 of the stand 124 is raised closer to the center frame 122, so that the support end 1242 of the stand 124 does not block when the camera 200 is photographed.
  • the line of sight of the imaging device 200 is used to achieve 360 degree shooting.
  • the support end 1242 of the stand 124 is lowered, and the support frame 14 is raised.
  • the drone 100 descends, and the stand 124 surrounds the image pickup apparatus 200, so that the image pickup apparatus 200 can be protected.
  • the stand 124 is rotatably coupled to the center frame 122;
  • the stand 124 is slidably coupled to the center frame 122;
  • the support frame 14 is rotatably connected to the center frame 122 through the connecting mechanism 16;
  • the support frame 14 is slidably coupled to the center frame 122 by a coupling mechanism 16.
  • the support frame 14 and the support frame 14 of the stand 124 can be moved up and down relative to the center frame 122.
  • the movable connection may be a rotary connection or a sliding connection.
  • the movable connection is not limited to the above connection manner.
  • the stand 124 can be rotatably connected to the center frame 122, and the support frame 14 can be rotatably connected to the center frame 122 through the connecting mechanism 16.
  • the stand 124 can be rotatably connected to the center frame 122, and the support frame 14 can be connected.
  • the mechanism 16 is slidably connected to the center frame 122; the stand 124 can be slidably connected to the center frame 122, and the support frame 14 is rotatably connected to the center frame 122 through the connecting mechanism 16; and the stand 124 and the center frame 122 can be
  • the support frame 14 is slidably coupled to the center frame 122 by a joint mechanism 16 .
  • the stand 124 is rotatably connected to the center frame 122, and the support frame 14 is rotatably connected to the center frame 122 through the connecting mechanism 16.
  • the attachment mechanism 16 includes a link 162 that is movably coupled to the support frame 14 and the center frame 122.
  • the link 162 drives the support frame 14 up and down relative to the center frame 122.
  • the link 162 can be slidably coupled to the center frame 122, and the link 162 slides up and down to raise and lower the support frame 14 relative to the center frame 122.
  • the link 162 can also be rotatably coupled to the center frame 122, and the link 162 rotates to drive the support frame 14 up and down relative to the center frame 122. It may also be a telescopic link 162 that extends up and down to drive the support frame 14 up and down relative to the center frame 122.
  • the link 162 is rotatably coupled to the center frame 122, and the link 162 is rotated to drive the support frame 14 to move up and down relative to the center frame 122.
  • each of the links 162 includes a first sub-rod 1622 and a second sub-rod 1624, the first sub-rod 1622 and the second sub-rod 1624 are rotatably connected, the first sub- The rod 1622 is movably coupled to the center frame 122, the second sub-rod 1624 is movably coupled to the support frame 14, and the first sub-rod 1622 is rotated relative to the second sub-rod 1624 to change the distance between the support frame 14 and the center frame 122 to drive the support.
  • the frame 14 is raised and lowered for the center frame 122.
  • the link 162 is caused to move the support frame 14 up and down relative to the center frame 122 with a relatively simple structure.
  • first sub-rod 1622 is rotatably coupled to the center frame 122
  • second sub-rod 1624 is rotatably coupled to the support frame 14.
  • the first sub-rod 1622 is rotatably connected to the center frame 122, and the number of the connecting rods 162 is two, that is, the number of the first sub-rods 1622 is two, and the two first sub-rods 1622 are disposed.
  • the second sub-rod 1624 is also rotatably connected to the two first sub-rods 1622 and the other end is rotatably connected to the support frame 14 .
  • the two first sub-rods 1622 and the two second sub-bars 1624 are provided such that the strength of the connecting rod 162 is better and the carrying capacity is stronger.
  • the number of the links 162 is not limited to two, and may be one or two or more.
  • the first sub-rod 1622 is directly movably connected to the second sub-rod 1624. It can be understood that in other embodiments, an additional sub-bar may be disposed between the first sub-rod 1622 and the second sub-rod 1624 to movably connect the first sub-rod 1622 and the second sub-rod 1624.
  • the attachment mechanism 16 includes a lead screw (not shown), the screw includes a screw and a threaded member that is sleeved on the screw, one of the screw and the threaded member is coupled to the support frame 14, and the other is coupled to the center frame. 122.
  • the lead screw is extended and contracted relative to the center frame 122 to drive the support frame 14 to move up and down relative to the center frame 122.
  • the support frame 14 is lifted and lowered relative to the center frame 122 by the relative rotation of the screw and the screw.
  • it may be a screw connection support frame 14, the screw member is connected to the center frame 122, or a screw connection center frame 122, and the screw member is connected to the support frame 14.
  • the stand 124 includes a connecting end 1244 opposite the support end 1242.
  • the connecting end 1244 is movably coupled to the support frame 14.
  • the support frame 14 drives the connection end.
  • the support frame 14 drives the connection end 1244 to descend to raise the support end 1242.
  • the support end 1242 descends relative to the center frame 122; when the support frame 14 is lowered relative to the center frame 122, the support end 1242 rises relative to the center frame 122.
  • the stand 124 is rotatably coupled to the center frame 122.
  • the connection end 1244 rises with the support frame 14, and the stand 124 rotates, so that the support end 1242 descends relative to the center frame 122;
  • the connection end The 1244 descends with the support frame 14, and the stand 124 rotates, thereby causing the support end 1242 to rise relative to the center frame 122.
  • the frame assembly 10 includes a connecting rod 17 that is movably coupled to the connecting end 1244 and the support frame 14.
  • connection between the support frame 14 and the stand 124 is made more flexible.
  • the support frame 14 when the support frame 14 is raised to be closest to the center frame 122, the connecting rod 17 and the connecting end 1244 are in a locked state, and the connecting rod 17 and the supporting frame 14 are in a locked state. As such, the support frame 14 is made more stable, so that the image pickup apparatus 200 mounted on the support frame 14 is more stable.
  • the connecting rod 17 is rotatably connected to the connecting end 1244, and the connecting rod 17 is rotatably connected to the supporting frame 14.
  • the connecting rod 17 may be slidably connected to the connecting end 1244, the connecting rod 17 is rotatably connected to the supporting frame 14; the connecting rod 17 may be rotatably connected to the connecting end 1244, and the connecting rod 17 is slidably connected to the supporting frame 14; It is also possible that the connecting rod 17 is slidably connected to the connecting end 1244, and the connecting rod 17 is slidably connected to the supporting frame 14.
  • the connecting rod 17 and the stand 124 are substantially in line.
  • the first sub-rod 1622 and the second sub-rod 1624 are substantially on the same straight line, as shown in FIG. In this way, the support frame 14 is made more stable.
  • the frame assembly 10 includes an extension bracket 18 that connects the center frame 122 and the foot frame 124.
  • the connection between the extension bracket 18 and the foot frame 124 is between the connection end 1244 and the support end 1242, extending
  • the bracket 18 is movably coupled to at least one of the center frame 122 and the stand 124.
  • the structure of the frame assembly 10 is made more reasonable.
  • the active connection can be a rotary connection or a sliding connection.
  • the extension bracket 18 may be movably connected to the center frame 122, and the extension bracket 18 is fixedly connected to the base frame 124.
  • the extension bracket 18 may be fixedly connected to the center frame 122, the extension bracket 18 is movably connected to the stand 124, and may also be an extension bracket. 18 is movably coupled to the center frame 122, and the extension bracket 18 is movably coupled to the stand 124.
  • the extension bracket 18 and the center frame 122 are fixedly connected, and the extension bracket 18 and the foot frame 124 are rotatably connected.
  • the stand 124 rotates relative to the extension bracket 18 such that the support end 1242 rises or falls relative to the center frame 122.
  • the support frame 14 is lowered to the farthest from the center frame 122 when the support end 1242 is aligned with the height of the center frame 122. As shown in FIG. 2, the support frame 14 is raised to the support frame 14 when it is closest to the center frame 122. The height is higher than the height of the support end 1242, as shown in FIG.
  • the support end 1242 does not block the support frame 14, so that the image pickup apparatus 200 mounted on the support frame 14 can realize 360 shooting.
  • the support frame 14 is raised to the nearest position to the center frame 122, the support end 1242 is supported on the landing surface, and the support frame 14 is higher than the landing surface, effectively protecting the image pickup device 200 on the support frame 14 and the support frame 14.
  • the frame assembly 10 includes at least two legs 124 that are angularly distributed along the central axis X of the center frame 122.
  • the stand 124 can support the drone 100 more stably.
  • the rack assembly 10 can include two legs 124, and can also include three legs 124, and can also include any other two or more legs 124.
  • the number of the frame assemblies 10 is two, and the axis is symmetrically disposed about the central axis of the center frame 122.
  • the lifting and lowering of the support ends 1242 of the plurality of legs 124 relative to the center frame 122 is synchronous.
  • the support ends 1242 of the plurality of stand 124 are on the same level. In this way, the drone 100 can land smoothly.
  • the frame assembly 10 includes a drive assembly (not shown) that is coupled to the attachment mechanism 16 and that is used to drive the linkage mechanism 16 to move the support frame 14 up and down relative to the center frame 122.
  • the drive assembly 16 drives the connection mechanism 16 to lift and lower the support frame 14 relative to the center frame 122, and drives the support end 1242 to move up and down relative to the center frame 122, thereby facilitating automatic control, simplifying the user operation process, and improving the user experience.
  • the screw When the connecting mechanism 16 includes a screw, the screw includes a screw and a screw sleeved on the screw.
  • the driving assembly can move the screw to move up and down relative to the screw by driving the screw to drive the support frame 14 to move up and down relative to the center frame 122.
  • the drive assembly can also move the screw up and down relative to the threaded member by driving the screw member to move the support frame 14 up and down relative to the center frame 122.
  • the frame assembly 10 includes a drive assembly (not shown) that is coupled to the stand 124 and It is used to drive the support end 1242 to lift.
  • the support end 1242 is lifted and lowered relative to the center frame 122 by the driving member, and the support frame 14 is lifted and lowered relative to the center frame 122, which facilitates automatic control, simplifies the user operation process, and improves the user experience.
  • the drive assembly can be coupled to the support end 1242 of the stand 124, and the support end 1242 of the drive stand 124 can be raised or lowered relative to the center frame 122.
  • the drive assembly can also be coupled to the connection end 1244 of the stand 124.
  • the support end 1242 can be lowered or raised relative to the center frame 122 by raising or lowering the connection end 1244 of the drive stand 124 relative to the center frame 122.
  • the drive assembly includes a steering gear coupled to the stand 124.
  • the steering gear driving tripod 124 raises or lowers the support end 1242 of the tripod 124 relative to the center frame 122, and the driving method is simple and reliable.
  • a drone 100 according to an embodiment of the present invention includes the rack assembly 10 and the power assembly 20 of any of the above embodiments, and the power assembly 20 is mounted on the rack assembly 10 for providing flight. power.
  • the support frame 14 when the support frame 14 is lowered, the support end 1242 of the stand 124 is raised, and when the support frame 14 is raised, the support end 1242 of the stand 124 is lowered, and the camera 200 can be mounted to the support frame 14 as a drone.
  • the camera 200 When the 100 is in the navigation state, the camera 200 is lowered away from the center frame 122 with the support frame 14, and the support end 1242 of the stand 124 is raised closer to the center frame 122, so that the support end 1242 of the stand 124 does not block when the camera 200 is photographed.
  • the line of sight of the imaging device 200 is used to achieve 360 degree shooting.
  • the frame assembly 10 includes a boom 19 that is coupled to a center frame 122 and a power assembly 20 that is mounted to the arm 19.
  • the arm 19 provides mounting support for the power assembly 20 such that the power assembly 20 provides flight power to the drone 100.
  • the power assembly 20 includes a propeller 22 that is located furthest from the center frame 122 when the support end 1242 is located outside of the propeller 22 .
  • the support end 1242 can function to protect the propeller 22, the center frame 122, and the arm 19 when the support frame 14 is furthest from the center frame 122.
  • the support end 1242 is elongated, and the drone 100 includes four propellers 22 disposed around the central axis of the center frame 122.
  • the length of the support end 1242 is greater than the maximum distance between the ends of two adjacent propellers 22. . In this way, the propeller 22 is effectively protected, and the collision of the propeller 22 with the outside is reduced.
  • the drone 100 includes a flight controller (not shown) that is pre-set with a takeoff mode and a drop mode of the drone 100, and when the drone 100 is in a landing mode, flight control The controller is used to control the connecting mechanism 16 to drive the support frame 14 to rise relative to the center frame 122 to cause the support frame 14 to lower the support end 1242 of the stand 124; and when the drone 100 is in the take-off mode, the flight controller is used to control the connection mechanism 16 Drive the support frame 14 phase Lowering the center frame 122 to cause the support frame 14 to raise the support end 1242 of the stand 124; or
  • the flight controller When the drone 100 is in the take-off mode, the flight controller is used to control the support end 1242 of the stand 124 to rise so that the stand 124 drives the support frame 14 to descend relative to the center frame 122; and when the drone 100 is in the landing mode, The flight controller is used to control the support end 1242 of the stand 124 to descend such that the stand 124 drives the support frame 14 to rise relative to the center frame 122.
  • the rack assembly 10 includes a drive assembly.
  • the drive assembly is coupled to the attachment mechanism 16 and is used to drive the linkage mechanism 16 to cause the support frame 14 to move up and down relative to the center frame 122.
  • the flight controller is used to control the drive assembly driving connection mechanism 16 to drive the support frame 14 to rise relative to the center frame 122 to cause the support frame 14 to lower the support end 1242 of the stand 124;
  • the flight controller is used to control the drive assembly drive connection mechanism 16 to drive the support frame 14 down relative to the center frame 122 to cause the support frame 14 to raise the support end 1242 of the stand 124.
  • the drive assembly is coupled to the stand 124 and is used to drive the support end 1242 up and down.
  • the flight controller is used to control the support end 1242 of the drive assembly driving stand 124 to raise the support end 1242 so that the stand 124 drives the support frame 14 to descend relative to the center frame 122;
  • the flight controller is used to control the support end 1242 of the drive assembly driving stand 124 to lower the support end 1242 so that the stand 124 drives the support frame 14 to rise relative to the center frame 122.
  • the drone 100 includes a pan-tilt device 40 that includes a pan-tilt 42 for carrying the camera device 200, the pan-tilt 42 being mounted to the support frame 14.
  • pan/tilt head 42 provides mounting support for the imaging device 200, so that the drone device 100 can mount the imaging device 200.
  • the pan/tilt head 42 includes a spindle mechanism 422 for adjusting the angle of view of the camera device 200.
  • the spindle mechanism 422 includes at least one of the following: a pitch axis mechanism, a roll axis mechanism, and a translation axis mechanism.
  • the imaging device 200 provided on the pan/tilt head 42 can adjust the imaging angle, and the imaging device 200 can capture a wider range, and the imaging effect is better.
  • the pitch axis mechanism can be used to adjust the rotation around the x-axis of the imaging device 200; the translation axis mechanism can be used to adjust the rotation around the y-axis of the imaging device 200; the roll axis mechanism can be used to adjust the camera device 200.
  • the x-axis, the y-axis, and the z-axis are perpendicular to each other.
  • first and second are used for descriptive purposes only and are not to be construed as indicating or implying a relative importance or implicitly indicating the number of technical features indicated.
  • features defining “first” and “second” may include at least one feature, either explicitly or implicitly.
  • a plurality means at least two, for example two, three, unless specifically defined otherwise.

Abstract

A frame assembly (10) and an unmanned aerial vehicle (100). The frame assembly (10) comprises a frame (12), a support frame (14), and a connecting mechanism (16). The frame (12) comprises a central frame (122) and struts (124) movably connected to the central frame (122). The support frame (14) is movably connected to the struts (124) and is used for bearing a load of the unmanned aerial vehicle (100). The connecting mechanism (16) is connected to the support frame (14) and the central frame (122). The support frame (14) is movably connected to the central frame (122) by the connecting mechanism (16), such that the support frame (14) can move vertically relative to the central frame (122). The struts (124) comprise support ends (1242) used for contacting with a landing surface. When the support ends (1242) of the struts (124) rise, the struts (124) lower the support frame (14) relative to the central frame (122), and when the support ends (1242) of the struts (124) are lowered, the struts (124) raise the support frame (14) relative to the central frame (122); alternatively, when the connecting mechanism (16) raises the support frame (14) relative to the central frame (122), the support frame (14) lowers the support ends (1242), and when the connecting mechanism (16) lowers the support frame (14) relative to the central frame (122), the support frame (14) raises the support ends (1242). When the unmanned aerial vehicle (100) is flying, a camera device (200) is lowered together with the support frame (14) to move away from the central frame (122), and the support ends (1242) of the struts (124) rise towards the central frame (122), such that when the camera device (200) performs image capture, the support ends (1242) of the struts (1242) do not block the line of sight of the camera device (200), thereby realizing 360-degree image capture.

Description

机架组件及无人机Rack assembly and drone 技术领域Technical field
本发明涉及飞行器领域,特别涉及一种机架组件及无人机。The present invention relates to the field of aircraft, and in particular to a rack assembly and a drone.
背景技术Background technique
在相关技术中,无人机可用于航拍。无人机的机身设置有起落架,当无人机降落时起落架将无人机支撑在地面上。然而机身下方设置有摄像头,在无人机航拍时,起落架会遮挡摄像头的视线,影响摄像头拍摄范围,难以实现360度拍摄。In the related art, the drone can be used for aerial photography. The fuselage of the drone is provided with a landing gear, and the landing gear supports the drone on the ground when the drone is landing. However, there is a camera under the fuselage. When the drone is aerial, the landing gear will block the camera's line of sight, affecting the camera's shooting range, and it is difficult to achieve 360-degree shooting.
发明内容Summary of the invention
本发明实施方式提供了一种机架组件及无人机。Embodiments of the present invention provide a rack assembly and a drone.
本发明实施方式的机架组件包括:The rack assembly of the embodiment of the invention includes:
机架,所述机架包括中心架、以及与所述中心架可活动连接的脚架;a rack, the rack including a center frame, and a stand that is movably coupled to the center frame;
与所述脚架可活动连接的支撑架,所述支撑架用于承载所述无人机的负载;以及a support frame movably coupled to the stand, the support frame for carrying a load of the drone;
连接所述支撑架与所述中心架的连接机构,所述支撑架通过所述连接机构与所述中心架可活动连接,以使所述支撑架能够相对于所述中心架升降;Connecting a connection mechanism of the support frame and the center frame, the support frame being movably connected to the center frame by the connection mechanism, so that the support frame can be lifted and lowered relative to the center frame;
其中,所述脚架包括用于与着陆面接触的支撑端;当所述支撑端上升时,所述脚架带动所述支撑架相对于所述中心架下降,当所述支撑端下降时,所述脚架带动所述支撑架相对于所述中心架上升;Wherein the tripod includes a support end for contacting the landing surface; when the support end is raised, the tripod drives the support frame to descend relative to the center frame, when the support end is lowered, The tripod drives the support frame to rise relative to the center frame;
或者,当所述连接机构带动所述支撑架相对于所述中心架上升时,所述支撑架带动所述支撑端下降,当所述连接机构带动所述支撑架相对于所述中心架下降时,所述支撑架带动所述支撑端上升。Or, when the connecting mechanism drives the support frame to rise relative to the center frame, the support frame drives the support end to descend, when the connecting mechanism drives the support frame to descend relative to the center frame. The support frame drives the support end to rise.
上述机架组件中,支撑架下降时脚架的支撑端上升,支撑架上升时脚架的支撑端下降,可将摄像装置安装至支撑架,当无人机处于航行状态时,摄像装置随支撑架下降远离中心架,脚架的支撑端上升靠近中心架,这样摄像装置在拍摄时,脚架的支撑端不会遮挡摄像装置的视线,以实现360度拍摄。In the above frame assembly, when the support frame is lowered, the support end of the stand is raised, and when the support frame is raised, the support end of the stand is lowered, and the camera device can be mounted to the support frame. When the drone is in a navigation state, the camera device is supported by the support device. The frame is lowered away from the center frame, and the support end of the stand is raised close to the center frame, so that the support end of the stand does not block the line of sight of the camera when shooting, so as to achieve 360-degree shooting.
本发明实施方式的一种无人机包括:A drone according to an embodiment of the present invention includes:
上述任一实施方式所述的机架组件;以及a rack assembly according to any of the above embodiments;
动力组件,所述动力组件安装在所述机架组件上,用于提供飞行动力。A power assembly mounted on the frame assembly for providing flight power.
上述无人机中,支撑架下降时脚架的支撑端上升,支撑架上升时脚架的支撑端下降,可将摄像装置安装至支撑架,当无人机处于航行状态时,摄像装置随支撑架下降远离中心 架,脚架的支撑端上升靠近中心架,这样摄像装置在拍摄时,脚架的支撑端不会遮挡摄像装置的视线,以实现360度拍摄。In the above-mentioned drone, when the support frame is lowered, the support end of the tripod is raised, and when the support frame is raised, the support end of the tripod is lowered, and the camera device can be mounted to the support frame. When the drone is in a navigation state, the camera device is supported by the support device. Rack away from the center The support end of the tripod rises close to the center frame, so that the support end of the tripod does not block the line of sight of the camera when shooting, so as to achieve 360-degree shooting.
本发明的实施方式的附加方面和优点将在下面的描述中部分给出,部分将从下面的描述中变得明显,或通过本发明的实施方式的实践了解到。The additional aspects and advantages of the embodiments of the present invention will be set forth in part in the description which follows.
附图说明DRAWINGS
本发明的上述和/或附加的方面和优点从结合下面附图对实施方式的描述中将变得明显和容易理解,其中:The above and/or additional aspects and advantages of the present invention will become apparent and readily understood from
图1是本发明实施方式的无人机在支撑架远离中心架时的立体示意图;1 is a perspective view of a drone according to an embodiment of the present invention when the support frame is away from the center frame;
图2是本发明实施方式的无人机在支撑架远离中心架时的平面示意图;2 is a schematic plan view of the drone of the embodiment of the present invention when the support frame is away from the center frame;
图3是本发明实施方式的无人机在支撑架远离中心架时的另一平面示意图;3 is another schematic plan view of the drone of the embodiment of the present invention when the support frame is away from the center frame;
图4是本发明实施方式的无人机在支撑架远离中心架时的俯视图;4 is a top plan view of the drone of the embodiment of the present invention when the support frame is away from the center frame;
图5是本发明实施方式的无人机在支撑架靠近中心架时的立体示意图;5 is a perspective view of the drone of the embodiment of the present invention when the support frame is close to the center frame;
图6是本发明实施方式的无人机在支撑架靠近中心架时的平面示意图;6 is a schematic plan view of the drone of the embodiment of the present invention when the support frame is close to the center frame;
图7是本发明实施方式的无人机在支撑架靠近中心架时的另一平面示意图;7 is another schematic plan view of the drone of the embodiment of the present invention when the support frame is close to the center frame;
图8是本发明实施方式的无人机在支撑架靠近中心架时的仰视图。Figure 8 is a bottom plan view of the drone of the embodiment of the present invention with the support frame near the center frame.
主要元件符号附图说明:The main component symbol drawing description:
无人机100,机架组件10,机架12,中心架122,脚架124,支撑端1242,连接端1244,支撑架14,连接机构16,连杆162,第一子杆1622,第二子杆1624,连接杆17,延伸支架18,机臂19,动力组件20,螺旋桨22,云台装置40,云台42,转轴机构422,摄像装置200。 UAV 100, rack assembly 10, frame 12, center frame 122, stand 124, support end 1242, connection end 1244, support frame 14, connection mechanism 16, link 162, first sub-rod 1622, second The sub-rod 1624, the connecting rod 17, the extension bracket 18, the arm 19, the power unit 20, the propeller 22, the pan-tilt unit 40, the pan/tilt head 42, the shaft mechanism 422, and the camera unit 200.
具体实施方式Detailed ways
以下结合附图对本发明的实施方式作进一步说明。附图中相同或类似的标号自始至终表示相同或类似的元件或具有相同或类似功能的元件。Embodiments of the present invention will be further described below in conjunction with the accompanying drawings. The same or similar reference numerals in the drawings denote the same or similar elements or elements having the same or similar functions.
另外,下面结合附图描述的本发明的实施方式是示例性的,仅用于解释本发明的实施方式,而不能理解为对本发明的限制。In addition, the embodiments of the present invention described below in conjunction with the accompanying drawings are merely illustrative of the embodiments of the invention, and are not to be construed as limiting.
在本发明中,除非另有明确的规定和限定,第一特征在第二特征“上”或“下”可以是第一和第二特征直接接触,或第一和第二特征通过中间媒介间接接触。而且,第一特征在第二特征“之上”、“上方”和“上面”可是第一特征在第二特征正上方或斜上方,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”可以是第一特征在第二特征正下方或斜下方,或仅仅表示第一特征水平高度小于第二特征。In the present invention, the first feature "on" or "under" the second feature may be a direct contact of the first and second features, or the first and second features may be indirectly through an intermediate medium, unless otherwise explicitly stated and defined. contact. Moreover, the first feature "above", "above" and "above" the second feature may be that the first feature is directly above or above the second feature, or only It is only indicated that the first feature level is higher than the second feature. The first feature "below", "below" and "below" the second feature may be that the first feature is directly below or obliquely below the second feature, or merely that the first feature level is less than the second feature.
请参阅图1及图5,本发明实施方式的机架组件10包括机架12、支撑架14及连接机构16,机架12包括中心架122、以及与中心架122可活动连接的脚架124。支撑架14与脚架124可活动连接,支撑架14用于承载无人机100的负载。连接机构16连接支撑架14与中心架122,支撑架14通过连接机构16与中心架122可活动连接,以使支撑架14能够相对于中心架122升降。Referring to FIGS. 1 and 5 , the rack assembly 10 of the embodiment of the present invention includes a frame 12 , a support frame 14 , and a connecting mechanism 16 . The frame 12 includes a center frame 122 and a stand 124 movably coupled to the center frame 122 . . The support frame 14 is movably coupled to the stand 124 for carrying the load of the drone 100. The connecting mechanism 16 connects the support frame 14 and the center frame 122. The support frame 14 is movably connected to the center frame 122 through the connecting mechanism 16 to enable the support frame 14 to be lifted and lowered relative to the center frame 122.
脚架124包括用于与着陆面接触的支撑端1242。当支撑端1242上升时,脚架124带动支撑架14相对于中心架122下降,当支撑端1242下降时,脚架124带动支撑架14相对于中心架122上升;或者,当连接机构16带动支撑架14相对于中心架122上升时,支撑架14带动支撑端1242下降,当连接机构16带动支撑架14相对于中心架122下降时,支撑架14带动支撑端1242上升。The stand 124 includes a support end 1242 for contacting the landing surface. When the support end 1242 is raised, the stand 124 drives the support frame 14 to descend relative to the center frame 122. When the support end 1242 is lowered, the stand 124 drives the support frame 14 to rise relative to the center frame 122; or, when the connecting mechanism 16 drives the support When the frame 14 is raised relative to the center frame 122, the support frame 14 drives the support end 1242 to descend. When the connecting mechanism 16 drives the support frame 14 to descend relative to the center frame 122, the support frame 14 drives the support end 1242 to rise.
上述机架组件10中,支撑架14下降时脚架124的支撑端1242上升,支撑架14上升时脚架124的支撑端1242下降,可将摄像装置200安装至支撑架14,当无人机100处于航行状态时,摄像装置200随支撑架14下降远离中心架122,脚架124的支撑端1242上升靠近中心架122,这样摄像装置200在拍摄时,脚架124的支撑端1242不会遮挡摄像装置200的视线,以实现360度拍摄。In the above-mentioned frame assembly 10, when the support frame 14 is lowered, the support end 1242 of the stand 124 is raised, and when the support frame 14 is raised, the support end 1242 of the stand 124 is lowered, and the camera device 200 can be mounted to the support frame 14 as a drone. When the 100 is in the navigation state, the camera 200 is lowered away from the center frame 122 with the support frame 14, and the support end 1242 of the stand 124 is raised closer to the center frame 122, so that the support end 1242 of the stand 124 does not block when the camera 200 is photographed. The line of sight of the imaging device 200 is used to achieve 360 degree shooting.
请参阅图5-8,当无人机100降落时,脚架124的支撑端1242下降,支撑架14上升。如此,当摄像装置200安装在支撑架14时,无人机100降落后,脚架124环绕摄像装置200,从而可以保护摄像装置200。Referring to FIGS. 5-8, when the drone 100 is lowered, the support end 1242 of the stand 124 is lowered, and the support frame 14 is raised. As such, when the image pickup apparatus 200 is mounted on the support frame 14, the drone 100 descends, and the stand 124 surrounds the image pickup apparatus 200, so that the image pickup apparatus 200 can be protected.
在某些实施方式中,脚架124与中心架122可转动连接;In some embodiments, the stand 124 is rotatably coupled to the center frame 122;
或者,脚架124与中心架122可滑动连接;Alternatively, the stand 124 is slidably coupled to the center frame 122;
或者,支撑架14通过连接机构16与中心架122可转动连接;Or the support frame 14 is rotatably connected to the center frame 122 through the connecting mechanism 16;
或者,支撑架14通过连接机构16与中心架122可滑动连接。Alternatively, the support frame 14 is slidably coupled to the center frame 122 by a coupling mechanism 16.
如此,使脚架124的支撑架14和支撑架14可相对于中心架122上下移动。As such, the support frame 14 and the support frame 14 of the stand 124 can be moved up and down relative to the center frame 122.
可以理解,可活动连接可以是转动连接也可以是滑动连接。当然,在其他实施方式中,可活动连接不限于上述连接方式。It will be appreciated that the movable connection may be a rotary connection or a sliding connection. Of course, in other embodiments, the movable connection is not limited to the above connection manner.
具体地,可以是脚架124与中心架122可转动连接,支撑架14通过连接机构16与中心架122可转动连接;也可以是脚架124与中心架122可转动连接,支撑架14通过连接机构16与中心架122可滑动连接;还可以是脚架124与中心架122可滑动连接,支撑架14通过连接机构16与中心架122可转动连接;还可以是脚架124与中心架122可滑动连接,支撑架14通过连接机构16与中心架122可滑动连接。 Specifically, the stand 124 can be rotatably connected to the center frame 122, and the support frame 14 can be rotatably connected to the center frame 122 through the connecting mechanism 16. Alternatively, the stand 124 can be rotatably connected to the center frame 122, and the support frame 14 can be connected. The mechanism 16 is slidably connected to the center frame 122; the stand 124 can be slidably connected to the center frame 122, and the support frame 14 is rotatably connected to the center frame 122 through the connecting mechanism 16; and the stand 124 and the center frame 122 can be The support frame 14 is slidably coupled to the center frame 122 by a joint mechanism 16 .
在本发明实施方式中,脚架124与中心架122可转动连接,支撑架14通过连接机构16与中心架122可转动连接。In the embodiment of the present invention, the stand 124 is rotatably connected to the center frame 122, and the support frame 14 is rotatably connected to the center frame 122 through the connecting mechanism 16.
请参阅图2、图3、图6及图7,在某些实施方式中,连接机构16包括连杆162,连杆162可活动连接支撑架14和中心架122。Referring to FIGS. 2, 3, 6, and 7, in some embodiments, the attachment mechanism 16 includes a link 162 that is movably coupled to the support frame 14 and the center frame 122.
如此,连杆162带动支撑架14相对于中心架122升降。As such, the link 162 drives the support frame 14 up and down relative to the center frame 122.
具体地,连杆162可以与中心架122可滑动连接,连杆162上下滑动使支撑架14相对于中心架122升降。连杆162也可以与中心架122转动连接,连杆162转动带动支撑架14相对于中心架122升降。也可以是伸缩连杆162,连杆162上下伸缩以带动支撑架14相对于中心架122升降。Specifically, the link 162 can be slidably coupled to the center frame 122, and the link 162 slides up and down to raise and lower the support frame 14 relative to the center frame 122. The link 162 can also be rotatably coupled to the center frame 122, and the link 162 rotates to drive the support frame 14 up and down relative to the center frame 122. It may also be a telescopic link 162 that extends up and down to drive the support frame 14 up and down relative to the center frame 122.
在本发明实施方式中,连杆162与中心架122转动连接,连杆162转动带动支撑架14相对于中心架122升降。In the embodiment of the present invention, the link 162 is rotatably coupled to the center frame 122, and the link 162 is rotated to drive the support frame 14 to move up and down relative to the center frame 122.
在某些实施方式中,连杆162为多个,每个连杆162包括第一子杆1622和第二子杆1624,第一子杆1622和第二子杆1624可转动连接,第一子杆1622与中心架122活动连接,第二子杆1624与支撑架14活动连接,第一子杆1622与第二子杆1624相对转动以改变支撑架14和中心架122之间的距离以带动支撑架14对于中心架122升降。In some embodiments, there are a plurality of links 162, each of the links 162 includes a first sub-rod 1622 and a second sub-rod 1624, the first sub-rod 1622 and the second sub-rod 1624 are rotatably connected, the first sub- The rod 1622 is movably coupled to the center frame 122, the second sub-rod 1624 is movably coupled to the support frame 14, and the first sub-rod 1622 is rotated relative to the second sub-rod 1624 to change the distance between the support frame 14 and the center frame 122 to drive the support. The frame 14 is raised and lowered for the center frame 122.
如此,以较简单地结构使连杆162带动支撑架14相对于中心架122升降。Thus, the link 162 is caused to move the support frame 14 up and down relative to the center frame 122 with a relatively simple structure.
具体地,第一子杆1622与中心架122转动连接,第二子杆1624与支撑架14转动连接。Specifically, the first sub-rod 1622 is rotatably coupled to the center frame 122, and the second sub-rod 1624 is rotatably coupled to the support frame 14.
本发明实施方式中,第一子杆1622与中心架122转动连接,连杆162的数量为两个,也就是说,第一子杆1622的数量为2个,两个第一子杆1622设置间隔设置,第二子杆1624的数量也为两个,两个第二子杆1624的一端分别与两个第一子杆1622转动连接,另一端与支撑架14转动连接。如此,设置两个第一子杆1622和两个第二子杆1624使得连杆162的强度更好,承载能力更强。In the embodiment of the present invention, the first sub-rod 1622 is rotatably connected to the center frame 122, and the number of the connecting rods 162 is two, that is, the number of the first sub-rods 1622 is two, and the two first sub-rods 1622 are disposed. The second sub-rod 1624 is also rotatably connected to the two first sub-rods 1622 and the other end is rotatably connected to the support frame 14 . As such, the two first sub-rods 1622 and the two second sub-bars 1624 are provided such that the strength of the connecting rod 162 is better and the carrying capacity is stronger.
当然,在其他实施方式中,连杆162的数量不限于2个,也可以是1个或两个以上。Of course, in other embodiments, the number of the links 162 is not limited to two, and may be one or two or more.
本实施方式中,第一子杆1622直接活动连接第二子杆1624。可以理解,在其它实施方式中,第一子杆1622和第二子杆1624之间还可设置另外的子杆来活动连接第一子杆1622和第二子杆1624。In the present embodiment, the first sub-rod 1622 is directly movably connected to the second sub-rod 1624. It can be understood that in other embodiments, an additional sub-bar may be disposed between the first sub-rod 1622 and the second sub-rod 1624 to movably connect the first sub-rod 1622 and the second sub-rod 1624.
在某些实施方式中,连接机构16包括丝杆(图未示),丝杆包括螺杆以及套设于螺杆上的螺纹件,螺杆以及螺纹件的其中一个连接支撑架14,另外一个连接中心架122,丝杆相对于中心架122伸缩以带动支撑架14相对于中心架122升降。In some embodiments, the attachment mechanism 16 includes a lead screw (not shown), the screw includes a screw and a threaded member that is sleeved on the screw, one of the screw and the threaded member is coupled to the support frame 14, and the other is coupled to the center frame. 122. The lead screw is extended and contracted relative to the center frame 122 to drive the support frame 14 to move up and down relative to the center frame 122.
如此,通过螺杆和螺纹件相对转动带动支撑架14相对于中心架122升降。Thus, the support frame 14 is lifted and lowered relative to the center frame 122 by the relative rotation of the screw and the screw.
可以理解,螺杆和螺纹件相对转动使螺杆相对螺纹件上下移动,从而使得支撑架14相对于中心架122升降。 It will be appreciated that the relative rotation of the screw and the threaded member causes the screw to move up and down relative to the threaded member, thereby causing the support frame 14 to move up and down relative to the center frame 122.
具体地,可以是螺杆连接支撑架14,螺纹件连接中心架122;也可以是螺杆连接中心架122,螺纹件连接支撑架14。Specifically, it may be a screw connection support frame 14, the screw member is connected to the center frame 122, or a screw connection center frame 122, and the screw member is connected to the support frame 14.
在某些实施方式中,脚架124包括与支撑端1242相对的连接端1244,连接端1244与支撑架14可活动地连接,支撑架14相对于中心架122上升时,支撑架14带动连接端1244上升以使支撑端1242下降,支撑架14相对于中心架122下降时,支撑架14带动连接端1244下降以使支撑端1242上升。In some embodiments, the stand 124 includes a connecting end 1244 opposite the support end 1242. The connecting end 1244 is movably coupled to the support frame 14. When the support frame 14 is raised relative to the center frame 122, the support frame 14 drives the connection end. When the 1244 is raised to lower the support end 1242 and the support frame 14 is lowered relative to the center frame 122, the support frame 14 drives the connection end 1244 to descend to raise the support end 1242.
如此,使支撑架14相对于中心架122上升时,支撑端1242相对于中心架122下降;支撑架14相对于中心架122下降时,支撑端1242相对于中心架122上升。As such, when the support frame 14 is raised relative to the center frame 122, the support end 1242 descends relative to the center frame 122; when the support frame 14 is lowered relative to the center frame 122, the support end 1242 rises relative to the center frame 122.
具体地,本实施方式中,脚架124与中心架122转动连接。支撑架14相对于中心架122上升时,连接端1244随支撑架14上升,脚架124转动,从而使得支撑端1242相对于中心架122下降;支撑架14相对于中心架122下降时,连接端1244随支撑架14下降,脚架124转动,从而使得支撑端1242相对于中心架122上升。Specifically, in the present embodiment, the stand 124 is rotatably coupled to the center frame 122. When the support frame 14 rises relative to the center frame 122, the connection end 1244 rises with the support frame 14, and the stand 124 rotates, so that the support end 1242 descends relative to the center frame 122; when the support frame 14 descends relative to the center frame 122, the connection end The 1244 descends with the support frame 14, and the stand 124 rotates, thereby causing the support end 1242 to rise relative to the center frame 122.
在某些实施方式中,机架组件10包括连接杆17,连接杆17活动连接连接端1244和支撑架14。In certain embodiments, the frame assembly 10 includes a connecting rod 17 that is movably coupled to the connecting end 1244 and the support frame 14.
如此,使支撑架14和脚架124的连接更加灵活。In this way, the connection between the support frame 14 and the stand 124 is made more flexible.
具体地,请参图6,当支撑架14上升至距中心架122最近时,连接杆17和连接端1244处于锁死状态,连接杆17和支撑架14处于锁死状态。如此,使支撑架14更稳定,从而使得安装在支撑架14的摄像装置200更稳。Specifically, referring to FIG. 6, when the support frame 14 is raised to be closest to the center frame 122, the connecting rod 17 and the connecting end 1244 are in a locked state, and the connecting rod 17 and the supporting frame 14 are in a locked state. As such, the support frame 14 is made more stable, so that the image pickup apparatus 200 mounted on the support frame 14 is more stable.
本发明实施方式中,连接杆17转动连接连接端1244,连接杆17转动连接支撑架14。当然,在其他实施方式中,也可以是连接杆17滑动连接连接端1244,连接杆17转动连接支撑架14;还可以是连接杆17转动连接连接端1244,连接杆17滑动连接支撑架14;还可以是连接杆17滑动连接连接端1244,连接杆17滑动连接支撑架14。In the embodiment of the present invention, the connecting rod 17 is rotatably connected to the connecting end 1244, and the connecting rod 17 is rotatably connected to the supporting frame 14. Of course, in other embodiments, the connecting rod 17 may be slidably connected to the connecting end 1244, the connecting rod 17 is rotatably connected to the supporting frame 14; the connecting rod 17 may be rotatably connected to the connecting end 1244, and the connecting rod 17 is slidably connected to the supporting frame 14; It is also possible that the connecting rod 17 is slidably connected to the connecting end 1244, and the connecting rod 17 is slidably connected to the supporting frame 14.
请参阅图2,在某些实施方式中,支撑架14下降至距中心架122最远时,连接杆17与脚架124基本位于同一直线上。Referring to FIG. 2, in some embodiments, when the support frame 14 is lowered to the farthest from the center frame 122, the connecting rod 17 and the stand 124 are substantially in line.
如此,使支撑架14下降至距中心架122最远时,连接杆17与脚架124处于锁死状态,脚架124结构更加稳定,避免脚架124遮挡安装在支撑架14上的摄像装置200的视线。In this way, when the support frame 14 is lowered to the farthest distance from the center frame 122, the connecting rod 17 and the stand 124 are in a locked state, and the structure of the stand 124 is more stable, and the stand 124 is prevented from blocking the camera device 200 mounted on the support frame 14. Sight.
本发明实施方式中,支撑架14下降至距中心架122最远时,第一子杆1622和第二子杆1624基本在同一直线上,如图3所示。如此,使得支撑架14更加稳定。In the embodiment of the present invention, when the support frame 14 is lowered to the farthest from the center frame 122, the first sub-rod 1622 and the second sub-rod 1624 are substantially on the same straight line, as shown in FIG. In this way, the support frame 14 is made more stable.
在某些实施方式中,机架组件10包括延伸支架18,延伸支架18连接中心架122和脚架124,延伸支架18与脚架124的连接处位于连接端1244和支撑端1242之间,延伸支架18与中心架122和脚架124中的至少一个活动连接。In some embodiments, the frame assembly 10 includes an extension bracket 18 that connects the center frame 122 and the foot frame 124. The connection between the extension bracket 18 and the foot frame 124 is between the connection end 1244 and the support end 1242, extending The bracket 18 is movably coupled to at least one of the center frame 122 and the stand 124.
如此,使机架组件10的结构更加合理。 As such, the structure of the frame assembly 10 is made more reasonable.
具体地,活动连接可以是转动连接也可以是滑动连接。可以是延伸支架18与中心架122活动连接,延伸支架18与脚架124固定连接;也可以是延伸支架18与中心架122固定连接,延伸支架18与脚架124活动连接;还可以是延伸支架18与中心架122活动连接,延伸支架18与脚架124活动连接。In particular, the active connection can be a rotary connection or a sliding connection. The extension bracket 18 may be movably connected to the center frame 122, and the extension bracket 18 is fixedly connected to the base frame 124. The extension bracket 18 may be fixedly connected to the center frame 122, the extension bracket 18 is movably connected to the stand 124, and may also be an extension bracket. 18 is movably coupled to the center frame 122, and the extension bracket 18 is movably coupled to the stand 124.
本发明实施方式中,延伸支架18和中心架122固定连接,延伸支架18和脚架124转动连接。脚架124相对于延伸支架18转动使得支撑端1242相对于中心架122上升或下降。In the embodiment of the present invention, the extension bracket 18 and the center frame 122 are fixedly connected, and the extension bracket 18 and the foot frame 124 are rotatably connected. The stand 124 rotates relative to the extension bracket 18 such that the support end 1242 rises or falls relative to the center frame 122.
在某些实施方式中,支撑架14下降至距中心架122最远时支撑端1242与中心架122的高度一致,如图2所示,支撑架14上升至距中心架122最近时支撑架14的高度高于支撑端1242的高度,如图6所示。In some embodiments, the support frame 14 is lowered to the farthest from the center frame 122 when the support end 1242 is aligned with the height of the center frame 122. As shown in FIG. 2, the support frame 14 is raised to the support frame 14 when it is closest to the center frame 122. The height is higher than the height of the support end 1242, as shown in FIG.
如此,支撑架14下降至距中心架122最远时,支撑端1242不会遮挡支撑架14,使安装在支撑架14上的摄像装置200可实现360拍摄。支撑架14上升至距中心架122最近时,支撑端1242支撑在着陆面,支撑架14高于着陆面,有效地保护支撑架14和支撑架14上的摄像装置200。Thus, when the support frame 14 is lowered to the farthest from the center frame 122, the support end 1242 does not block the support frame 14, so that the image pickup apparatus 200 mounted on the support frame 14 can realize 360 shooting. When the support frame 14 is raised to the nearest position to the center frame 122, the support end 1242 is supported on the landing surface, and the support frame 14 is higher than the landing surface, effectively protecting the image pickup device 200 on the support frame 14 and the support frame 14.
在某些实施方式中,机架组件10包括至少两个脚架124,至少两个脚架124沿中心架122的中轴线X等角度分布。In certain embodiments, the frame assembly 10 includes at least two legs 124 that are angularly distributed along the central axis X of the center frame 122.
如此,无人机100着陆时,脚架124可更加稳定地支撑无人机100。Thus, when the drone 100 is landed, the stand 124 can support the drone 100 more stably.
可以理解,机架组件10可以包括2个脚架124,也可以包括3个脚架124,还可以包括其它任意2个以上脚架124。本发明实施方式中,机架组件10的数量为2个,关于中心架122的中轴线轴对称设置。It can be understood that the rack assembly 10 can include two legs 124, and can also include three legs 124, and can also include any other two or more legs 124. In the embodiment of the present invention, the number of the frame assemblies 10 is two, and the axis is symmetrically disposed about the central axis of the center frame 122.
具体地,多个脚架124的支撑端1242相对于中心架122的升降是同步地。Specifically, the lifting and lowering of the support ends 1242 of the plurality of legs 124 relative to the center frame 122 is synchronous.
较佳地,支撑架14上升至距中心架122最近时,多个脚架124的支撑端1242在同一水平面上。如此,使无人机100可以平稳地着陆。Preferably, when the support frame 14 is raised to the closest to the center frame 122, the support ends 1242 of the plurality of stand 124 are on the same level. In this way, the drone 100 can land smoothly.
在某些实施方式中,机架组件10包括驱动组件(图未示),驱动组件连接连接机构16,并用于驱动连接机构16带动支撑架14相对于中心架122升降。In some embodiments, the frame assembly 10 includes a drive assembly (not shown) that is coupled to the attachment mechanism 16 and that is used to drive the linkage mechanism 16 to move the support frame 14 up and down relative to the center frame 122.
如此,通过驱动组件驱动连接机构16使支撑架14相对于中心架122升降,并带动支撑端1242相对于中心架122升降,有助于实现自动化控制,简化用户操作过程,提升用户体验。In this way, the drive assembly 16 drives the connection mechanism 16 to lift and lower the support frame 14 relative to the center frame 122, and drives the support end 1242 to move up and down relative to the center frame 122, thereby facilitating automatic control, simplifying the user operation process, and improving the user experience.
连接机构16包括丝杆时,丝杆包括螺杆以及套设于螺杆上的螺纹件,驱动组件可以通过驱动螺杆转动使螺纹件相对于螺杆上下移动从而带动支撑架14相对于中心架122升降。驱动组件也可以通过驱动螺纹件转动使螺杆相对于螺纹件上下移动从而带动支撑架14相对于中心架122升降。When the connecting mechanism 16 includes a screw, the screw includes a screw and a screw sleeved on the screw. The driving assembly can move the screw to move up and down relative to the screw by driving the screw to drive the support frame 14 to move up and down relative to the center frame 122. The drive assembly can also move the screw up and down relative to the threaded member by driving the screw member to move the support frame 14 up and down relative to the center frame 122.
在某些实施方式中,机架组件10包括驱动组件(图未示),驱动组件连接脚架124并 用于驱动支撑端1242升降。In certain embodiments, the frame assembly 10 includes a drive assembly (not shown) that is coupled to the stand 124 and It is used to drive the support end 1242 to lift.
如此,通过驱动件使支撑端1242相对于中心架122升降,并带动支撑架14相对于中心架122升降,有助于实现自动化控制,简化用户操作过程,提升用户体验。In this way, the support end 1242 is lifted and lowered relative to the center frame 122 by the driving member, and the support frame 14 is lifted and lowered relative to the center frame 122, which facilitates automatic control, simplifies the user operation process, and improves the user experience.
具体地,驱动组件可以连接脚架124的支撑端1242,驱动脚架124的支撑端1242相对于中心架122上升或下降。驱动组件也可以连接脚架124的连接端1244,通过驱动脚架124的连接端1244相对于中心架122上升或下降带动支撑端1242相对于中心架122下降或上升。Specifically, the drive assembly can be coupled to the support end 1242 of the stand 124, and the support end 1242 of the drive stand 124 can be raised or lowered relative to the center frame 122. The drive assembly can also be coupled to the connection end 1244 of the stand 124. The support end 1242 can be lowered or raised relative to the center frame 122 by raising or lowering the connection end 1244 of the drive stand 124 relative to the center frame 122.
在某些实施方式中,驱动组件包括与脚架124连接的舵机。In certain embodiments, the drive assembly includes a steering gear coupled to the stand 124.
如此,舵机驱动脚架124使脚架124的支撑端1242相对于中心架122上升或下降,驱动方式简单,可靠。In this manner, the steering gear driving tripod 124 raises or lowers the support end 1242 of the tripod 124 relative to the center frame 122, and the driving method is simple and reliable.
请参阅图1-图8,本发明实施方式的一种无人机100包括上述任一实施方式的机架组件10和动力组件20,动力组件20安装在机架组件10上,用于提供飞行动力。Referring to FIGS. 1-8, a drone 100 according to an embodiment of the present invention includes the rack assembly 10 and the power assembly 20 of any of the above embodiments, and the power assembly 20 is mounted on the rack assembly 10 for providing flight. power.
上述无人机100中,支撑架14下降时脚架124的支撑端1242上升,支撑架14上升时脚架124的支撑端1242下降,可将摄像装置200安装至支撑架14,当无人机100处于航行状态时,摄像装置200随支撑架14下降远离中心架122,脚架124的支撑端1242上升靠近中心架122,这样摄像装置200在拍摄时,脚架124的支撑端1242不会遮挡摄像装置200的视线,以实现360度拍摄。In the above-mentioned drone 100, when the support frame 14 is lowered, the support end 1242 of the stand 124 is raised, and when the support frame 14 is raised, the support end 1242 of the stand 124 is lowered, and the camera 200 can be mounted to the support frame 14 as a drone. When the 100 is in the navigation state, the camera 200 is lowered away from the center frame 122 with the support frame 14, and the support end 1242 of the stand 124 is raised closer to the center frame 122, so that the support end 1242 of the stand 124 does not block when the camera 200 is photographed. The line of sight of the imaging device 200 is used to achieve 360 degree shooting.
在某些实施方式中,机架组件10包括机臂19,机臂19与中心架122连接,动力组件20安装在机臂19。In certain embodiments, the frame assembly 10 includes a boom 19 that is coupled to a center frame 122 and a power assembly 20 that is mounted to the arm 19.
如此,机臂19为动力组件20提供安装支撑,使动力组件20为无人机100提供飞行动力。As such, the arm 19 provides mounting support for the power assembly 20 such that the power assembly 20 provides flight power to the drone 100.
请参阅图4,在某些实施方式中,动力组件20包括螺旋桨22,支撑架14距中心架122最远时支撑端1242位于螺旋桨22的外侧。Referring to FIG. 4 , in some embodiments, the power assembly 20 includes a propeller 22 that is located furthest from the center frame 122 when the support end 1242 is located outside of the propeller 22 .
如此,支撑架14距中心架122最远时,支撑端1242可起到保护螺旋桨22、中心架122和机臂19的作用。As such, the support end 1242 can function to protect the propeller 22, the center frame 122, and the arm 19 when the support frame 14 is furthest from the center frame 122.
具体地,支撑端1242呈长条状,无人机100包括环绕中心架122中心轴设置在四个螺旋桨22,支撑端1242的长度大于两个相邻的螺旋桨22的端部之间的最大距离。如此,有效地保护螺旋桨22,减少螺旋桨22与外界的碰撞。Specifically, the support end 1242 is elongated, and the drone 100 includes four propellers 22 disposed around the central axis of the center frame 122. The length of the support end 1242 is greater than the maximum distance between the ends of two adjacent propellers 22. . In this way, the propeller 22 is effectively protected, and the collision of the propeller 22 with the outside is reduced.
在某些实施方式中,无人机100包括飞行控制器(图未示),飞行控制器预设有无人机100的起飞模式和降落模式,当无人机100处于降落模式时,飞行控制器用于控制连接机构16带动支撑架14相对于中心架122上升以使支撑架14带动脚架124的支撑端1242下降;和当无人机100处于起飞模式时,飞行控制器用于控制连接机构16带动支撑架14相 对于中心架122下降以使支撑架14带动脚架124的支撑端1242上升;或In some embodiments, the drone 100 includes a flight controller (not shown) that is pre-set with a takeoff mode and a drop mode of the drone 100, and when the drone 100 is in a landing mode, flight control The controller is used to control the connecting mechanism 16 to drive the support frame 14 to rise relative to the center frame 122 to cause the support frame 14 to lower the support end 1242 of the stand 124; and when the drone 100 is in the take-off mode, the flight controller is used to control the connection mechanism 16 Drive the support frame 14 phase Lowering the center frame 122 to cause the support frame 14 to raise the support end 1242 of the stand 124; or
当无人机100处于起飞模式时,飞行控制器用于控制脚架124的支撑端1242上升以使脚架124带动支撑架14相对于中心架122下降;和当无人机100处于降落模式时,飞行控制器用于控制脚架124的支撑端1242下降以使脚架124带动支撑架14相对于中心架122上升。When the drone 100 is in the take-off mode, the flight controller is used to control the support end 1242 of the stand 124 to rise so that the stand 124 drives the support frame 14 to descend relative to the center frame 122; and when the drone 100 is in the landing mode, The flight controller is used to control the support end 1242 of the stand 124 to descend such that the stand 124 drives the support frame 14 to rise relative to the center frame 122.
如此,通过飞行控制器实现自动化控制,当无人机100降落时支撑端1242自动下降,有效地保护支撑架14安装在支撑架14的其他结构。也能够减少手动操作步骤,提升用户体验。As such, automatic control is achieved by the flight controller, and the support end 1242 automatically descends when the drone 100 is lowered, effectively protecting the other structure in which the support frame 14 is mounted on the support frame 14. It also reduces manual steps and improves the user experience.
具体地,机架组件10包括驱动组件。Specifically, the rack assembly 10 includes a drive assembly.
在一个例子中,驱动组件连接连接机构16,并用于驱动连接机构16带动支撑架14相对于中心架122升降。当无人机100处于降落模式时,飞行控制器用于控制驱动组件驱动连接机构16带动支撑架14相对于中心架122上升以使支撑架14带动脚架124的支撑端1242下降;和当无人机100处于起飞模式时,飞行控制器用于控制驱动组件驱动连接机构16带动支撑架14相对于中心架122下降以使支撑架14带动脚架124的支撑端1242上升。In one example, the drive assembly is coupled to the attachment mechanism 16 and is used to drive the linkage mechanism 16 to cause the support frame 14 to move up and down relative to the center frame 122. When the drone 100 is in the landing mode, the flight controller is used to control the drive assembly driving connection mechanism 16 to drive the support frame 14 to rise relative to the center frame 122 to cause the support frame 14 to lower the support end 1242 of the stand 124; When the machine 100 is in the take-off mode, the flight controller is used to control the drive assembly drive connection mechanism 16 to drive the support frame 14 down relative to the center frame 122 to cause the support frame 14 to raise the support end 1242 of the stand 124.
在另一个例子中,驱动组件连接脚架124并用于驱动支撑端1242升降。当无人机100处于起飞模式时,飞行控制器用于控制驱动组件驱动脚架124的支撑端1242使支撑端1242上升从而使脚架124带动支撑架14相对于中心架122下降;和当无人机100处于降落模式时,飞行控制器用于控制驱动组件驱动脚架124的支撑端1242使支撑端1242下降从而使脚架124带动支撑架14相对于中心架122上升。In another example, the drive assembly is coupled to the stand 124 and is used to drive the support end 1242 up and down. When the drone 100 is in the take-off mode, the flight controller is used to control the support end 1242 of the drive assembly driving stand 124 to raise the support end 1242 so that the stand 124 drives the support frame 14 to descend relative to the center frame 122; When the machine 100 is in the landing mode, the flight controller is used to control the support end 1242 of the drive assembly driving stand 124 to lower the support end 1242 so that the stand 124 drives the support frame 14 to rise relative to the center frame 122.
在某些实施方式中,无人机100包括云台装置40,云台装置40包括用于承载摄像装置200的云台42,云台42安装于支撑架14。In some embodiments, the drone 100 includes a pan-tilt device 40 that includes a pan-tilt 42 for carrying the camera device 200, the pan-tilt 42 being mounted to the support frame 14.
如此,云台42为摄像装置200提供安装支撑,使无人机100可以搭载摄像装置200。In this manner, the pan/tilt head 42 provides mounting support for the imaging device 200, so that the drone device 100 can mount the imaging device 200.
在某些实施方式中,云台42包括用于调节摄像装置200的拍摄视角的转轴机构422,转轴机构422包括如下至少一种:俯仰轴机构,横滚轴机构,平移轴机构。In some embodiments, the pan/tilt head 42 includes a spindle mechanism 422 for adjusting the angle of view of the camera device 200. The spindle mechanism 422 includes at least one of the following: a pitch axis mechanism, a roll axis mechanism, and a translation axis mechanism.
如此,使设置在云台42上的摄像装置200可调整拍摄角度,使摄像装置200拍摄到的范围更广,拍摄效果更好。In this manner, the imaging device 200 provided on the pan/tilt head 42 can adjust the imaging angle, and the imaging device 200 can capture a wider range, and the imaging effect is better.
具体地,如图5所示,俯仰轴机构可用于调节摄像装置200的绕x轴旋转;平移轴机构可用于调节摄像装置200的绕y轴旋转;横滚轴机构可用于调节摄像装置200的绕z轴旋转。其中x轴、y轴和z轴两两垂直。Specifically, as shown in FIG. 5, the pitch axis mechanism can be used to adjust the rotation around the x-axis of the imaging device 200; the translation axis mechanism can be used to adjust the rotation around the y-axis of the imaging device 200; the roll axis mechanism can be used to adjust the camera device 200. Rotate around the z axis. The x-axis, the y-axis, and the z-axis are perpendicular to each other.
在本说明书的描述中,参考术语“某些实施方式”、“一个实施方式”、“一些实施方式”、“示例”、“具体示例”、或“一些示例”等的描述意指结合该实施例或示例描述的具体特征、结构、材料或者特点包含于本发明的至少一个实施例或示例中。在本说明书中,对上述术 语的示意性表述不必须针对的是相同的实施例或示例。而且,描述的具体特征、结构、材料或者特点可以在任一个或多个实施例或示例中以合适的方式结合。此外,在不相互矛盾的情况下,本领域的技术人员可以将本说明书中描述的不同实施例或示例以及不同实施例或示例的特征进行结合和组合。In the description of the present specification, the description with reference to the terms "some embodiments", "one embodiment", "some embodiments", "example", "specific example", or "some examples", etc. Particular features, structures, materials or features described in the examples or examples are included in at least one embodiment or example of the invention. In this specification, the above surgery The schematic representation of the language is not necessarily directed to the same embodiment or example. Furthermore, the particular features, structures, materials, or characteristics described may be combined in a suitable manner in any one or more embodiments or examples. In addition, various embodiments or examples described in the specification and features of various embodiments or examples may be combined and combined without departing from the scope of the invention.
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至少一个特征。在本发明的描述中,“多个”的含义是至少两个,例如两个,三个,除非另有明确具体的限定。Moreover, the terms "first" and "second" are used for descriptive purposes only and are not to be construed as indicating or implying a relative importance or implicitly indicating the number of technical features indicated. Thus, features defining "first" and "second" may include at least one feature, either explicitly or implicitly. In the description of the present invention, "a plurality" means at least two, for example two, three, unless specifically defined otherwise.
尽管上面已经示出和描述了本发明的实施例,可以理解的是,上述实施例是示例性的,不能理解为对本发明的限制,本领域的普通技术人员在本发明的范围内可以对上述实施例进行变化、修改、替换和变型,本发明的范围由权利要求及其等同物限定。 Although the embodiments of the present invention have been shown and described, it is understood that the above-described embodiments are illustrative and are not to be construed as limiting the scope of the invention. The scope of the invention is defined by the claims and their equivalents.

Claims (20)

  1. 一种机架组件,用于无人机,其特征在于,所述机架组件包括:A rack assembly for a drone, characterized in that the rack assembly comprises:
    机架,所述机架包括中心架、以及与所述中心架可活动连接的脚架;a rack, the rack including a center frame, and a stand that is movably coupled to the center frame;
    与所述脚架可活动连接的支撑架,所述支撑架用于承载所述无人机的负载;以及a support frame movably coupled to the stand, the support frame for carrying a load of the drone;
    连接所述支撑架与所述中心架的连接机构,所述支撑架通过所述连接机构与所述中心架可活动连接,以使所述支撑架能够相对于所述中心架升降;Connecting a connection mechanism of the support frame and the center frame, the support frame being movably connected to the center frame by the connection mechanism, so that the support frame can be lifted and lowered relative to the center frame;
    其中,所述脚架包括用于与着陆面接触的支撑端;当所述支撑端上升时,所述脚架带动所述支撑架相对于所述中心架下降,当所述支撑端下降时,所述脚架带动所述支撑架相对于所述中心架上升;Wherein the tripod includes a support end for contacting the landing surface; when the support end is raised, the tripod drives the support frame to descend relative to the center frame, when the support end is lowered, The tripod drives the support frame to rise relative to the center frame;
    或者,当所述连接机构带动所述支撑架相对于所述中心架上升时,所述支撑架带动所述支撑端下降,当所述连接机构带动所述支撑架相对于所述中心架下降时,所述支撑架带动所述支撑端上升。Or, when the connecting mechanism drives the support frame to rise relative to the center frame, the support frame drives the support end to descend, when the connecting mechanism drives the support frame to descend relative to the center frame. The support frame drives the support end to rise.
  2. 根据权利要求1所述的机架组件,其特征在于,所述脚架与所述中心架可转动连接;The rack assembly of claim 1 wherein said stand is rotatably coupled to said center frame;
    或者,所述脚架与所述中心架可滑动连接;Or the tripod is slidably connected to the center frame;
    或者,所述支撑架通过所述连接机构与所述中心架可转动连接;Or the support frame is rotatably connected to the center frame by the connecting mechanism;
    或者,所述支撑架通过所述连接机构与所述中心架可滑动连接。Alternatively, the support frame is slidably coupled to the center frame by the connecting mechanism.
  3. 根据权利要求1所述的机架组件,其特征在于,所述连接机构包括连杆,所述连杆可活动连接所述支撑架和所述中心架。The frame assembly of claim 1 wherein said attachment mechanism includes a link that is movably coupled to said support frame and said center frame.
  4. 根据权利要求3所述的机架组件,其特征在于,所述连杆为多个,每个所述连杆包括第一子杆和第二子杆,所述第一子杆和所述第二子杆可转动连接,所述第一子杆与所述中心架活动连接,所述第二子杆与所述支撑架活动连接,所述第一子杆与所述第二子杆相对转动以改变所述支撑架和所述中心架之间的距离以带动所述支撑架对于所述中心架升降。The frame assembly according to claim 3, wherein said plurality of links are each, and said link includes a first sub-bar and a second sub-bar, said first sub-rod and said first The two sub-rods are rotatably connected, the first sub-rod is movably connected to the center frame, the second sub-rod is movably connected to the support frame, and the first sub-rod is opposite to the second sub-rod To change the distance between the support frame and the center frame to drive the support frame to lift and lower the center frame.
  5. 根据权利要求1所述的机架组件,其特征在于,所述连接机构包括丝杆,所述丝杆包括螺杆以及套设于所述螺杆上的螺纹件,所述螺杆以及所述螺纹件的其中一个连接所述支撑架,另外一个连接所述中心架,所述丝杆相对于所述中心架伸缩以带动所述支撑架相对于所述中心架升降。The frame assembly of claim 1 wherein said attachment mechanism comprises a lead screw, said lead screw comprising a screw and a threaded member threaded over said screw, said screw and said threaded member One of the brackets is connected to the other, and the other is connected to the center frame, and the screw rod is telescoped relative to the center frame to drive the support frame to move up and down relative to the center frame.
  6. 根据权利要求1所述的机架组件,其特征在于,所述脚架包括与所述支撑端相对的连接端,所述连接端与所述支撑架可活动地连接,The frame assembly of claim 1 wherein said foot frame includes a connector end opposite said support end, said connector end being movably coupled to said support frame,
    所述支撑架相对于所述中心架上升时,所述支撑架带动所述连接端上升以使所述支撑端下降,所述支撑架相对于所述中心架下降时,所述支撑架带动所述连接端下降以使所述 支撑端上升。When the support frame is raised relative to the center frame, the support frame drives the connection end to rise to lower the support end, and when the support frame is lowered relative to the center frame, the support frame drives the support frame Said connection is lowered to enable said The support end rises.
  7. 根据权利要求6所述的机架组件,其特征在于,所述机架组件包括连接杆,所述连接杆活动连接所述连接端和所述支撑架。The frame assembly of claim 6 wherein said frame assembly includes a connecting rod that movably connects said connecting end and said support frame.
  8. 根据权利要求7所述的机架组件,其特征在于,所述支撑架下降至距所述中心架最远时,所述连接杆与所述脚架基本位于同一直线上。The frame assembly of claim 7 wherein said connecting rod is substantially co-located with said foot when said support frame is lowered to the farthest from said center frame.
  9. 根据权利要求6所述的机架组件,其特征在于,所述机架组件包括延伸支架,所述延伸支架连接所述中心架和所述脚架,所述延伸支架与所述脚架的连接处位于所述连接端和所述支撑端之间,所述延伸支架与所述中心架和所述脚架中的至少一个活动连接。The frame assembly of claim 6 wherein said frame assembly includes an extension bracket connecting said center frame and said stand, said extension bracket being coupled to said stand Located between the connecting end and the supporting end, the extension bracket is movably connected to at least one of the center frame and the stand.
  10. 根据权利要求1所述的机架组件,其特征在于,所述支撑架下降至距所述中心架最远时所述支撑端与所述中心架的高度一致,所述支撑架上升至距所述中心架最近时所述支撑架的高度高于所述支撑端的高度。The frame assembly according to claim 1, wherein the support frame is lowered to a distance from the center frame when the support end is at the same height as the center frame, and the support frame is raised to a distance The height of the support frame when the center frame is closest is higher than the height of the support end.
  11. 根据权利要求1所述的机架组件,其特征在于,所述机架组件包括至少两个所述脚架,至少两个所述脚架沿所述中心架的中轴线等角度分布。The frame assembly of claim 1 wherein said frame assembly includes at least two said legs, at least two of said legs being equiangularly distributed along a central axis of said center frame.
  12. 根据权利要求1所述的机架组件,其特征在于,所述机架组件包括驱动组件,所述驱动组件连接所述连接机构,并用于驱动所述连接机构带动所述支撑架相对于所述中心架升降。The rack assembly of claim 1 wherein said frame assembly includes a drive assembly coupled to said attachment mechanism and for driving said attachment mechanism to drive said support frame relative to said The center frame is raised and lowered.
  13. 根据权利要求1所述的机架组件,其特征在于,所述机架组件包括驱动组件,所述驱动组件连接所述脚架并用于驱动所述支撑端升降。The frame assembly of claim 1 wherein said frame assembly includes a drive assembly coupled to said stand and for driving said support end to lift.
  14. 根据权利要求14所述的机架组件,其特征在于,所述驱动组件包括与所述脚架连接的舵机。The frame assembly of claim 14 wherein said drive assembly includes a steering gear coupled to said stand.
  15. 一种无人机,其特征在于包括:A drone characterized by comprising:
    权利要求1-14任意一项所述的机架组件;以及The frame assembly of any of claims 1-14;
    动力组件,所述动力组件安装在所述机架组件上,用于提供飞行动力。A power assembly mounted on the frame assembly for providing flight power.
  16. 根据权利要求15所述的无人机,其特征在于,所述机架组件包括机臂,所述机臂与所述中心架连接,所述动力组件安装在所述机臂。The drone according to claim 15, wherein said frame assembly includes a robot arm, said arm being coupled to said center frame, and said power assembly being mounted to said arm.
  17. 根据权利要求16所述的无人机,其特征在于,所述动力组件包括螺旋浆,所述支撑架距所述中心架最远时所述支撑端位于所述螺旋浆的外侧。The drone according to claim 16, wherein said power assembly comprises a propeller, said support end being located outside said propeller when said support frame is furthest from said center frame.
  18. 根据权利要求15所述的无人机,其特征在于,所述无人机包括飞行控制器,所述飞行控制器预设有所述无人机的起飞模式和降落模式,The drone according to claim 15, wherein the drone includes a flight controller, and the flight controller is pre-set with a take-off mode and a landing mode of the drone.
    当所述无人机处于所述降落模式时,所述飞行控制器用于控制所述连接机构带动所述支撑架相对于所述中心架上升以使所述支撑架带动所述支撑端下降;和当所述无人机处于所述起飞模式时,所述飞行控制器用于控制所述连接机构带动所述支撑架相对于所述中心 架下降以使所述支撑架带动所述支撑端上升;When the drone is in the landing mode, the flight controller is configured to control the connecting mechanism to drive the support frame to rise relative to the center frame to cause the support frame to drive the support end to descend; and The flight controller is configured to control the connecting mechanism to drive the support frame relative to the center when the drone is in the takeoff mode Lowering the frame to cause the support frame to drive the support end to rise;
    or
    当所述无人机处于所述起飞模式时,所述飞行控制器用于控制所述支撑端上升以使所述脚架带动所述支撑架相对于所述中心架下降;和当所述无人机处于所述降落模式时,所述飞行控制器用于控制所述支撑端下降以使所述脚架带动所述支撑架相对于所述中心架上升。When the drone is in the take-off mode, the flight controller is configured to control the support end to rise to cause the stand to drive the support frame to descend relative to the center frame; and when the unmanned When the machine is in the landing mode, the flight controller is configured to control the support end to descend such that the tripod drives the support frame to rise relative to the center frame.
  19. 根据权利要求15所述的无人机,其特征在于,所述无人机包括云台装置,所述云台装置包括用于承载拍摄装置的云台,所述云台安装于所述支撑架。The drone according to claim 15, wherein the drone includes a pan-tilt device, the pan-tilt device includes a pan/tilt for carrying a photographing device, and the pan-tilt is mounted on the support frame .
  20. 根据权利要求19所述的无人机,其特征在于,所述云台包括用于调节所述拍摄装置的拍摄视角的转轴机构,所述转轴机构包括如下至少一种:俯仰轴机构,横滚轴机构,平移轴机构。 The drone according to claim 19, wherein the pan/tilt head includes a rotating shaft mechanism for adjusting a shooting angle of view of the photographing device, and the rotating shaft mechanism includes at least one of: a pitch axis mechanism, a roll Shaft mechanism, translation shaft mechanism.
PCT/CN2017/097188 2017-08-11 2017-08-11 Frame assembly and unmanned aerial vehicle WO2019028871A1 (en)

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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111746813A (en) * 2019-03-27 2020-10-09 东汉太阳能无人机技术有限公司 Lifting system for small-sized unmanned aerial vehicle
US10822082B2 (en) 2017-04-07 2020-11-03 Mark Holbrook Hanna Distributed-battery aerial vehicle and a powering method therefor
CN113739043A (en) * 2021-08-25 2021-12-03 四川公众项目咨询管理有限公司 Automatic change electric power construction supervision system
CN117533543A (en) * 2024-01-09 2024-02-09 山东国建土地房地产评估测绘有限公司 Territory space planning topography measuring device

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2020205833A1 (en) * 2019-04-01 2020-10-08 Elbit Systems Of America, Llc Landing strobe and landing zone designation system
WO2023272445A1 (en) * 2021-06-28 2023-01-05 深圳市大疆创新科技有限公司 Frame, stand, and unmanned aerial vehicle
CN113928535A (en) * 2021-10-08 2022-01-14 中科信同科技集团有限公司 Folding arm of unmanned aerial vehicle and unmanned aerial vehicle

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN203246584U (en) * 2012-11-15 2013-10-23 深圳市大疆创新科技有限公司 Drive device for aircraft using tripod, landing gear and aircraft
CN103754355A (en) * 2014-01-10 2014-04-30 江苏艾锐泰克无人飞行器科技有限公司 Retractable landing gear and unmanned aerial vehicle
CN104760690A (en) * 2015-04-23 2015-07-08 零度智控(北京)智能科技有限公司 Retractable landing gear of unmanned aircraft
US20160144954A1 (en) * 2014-11-26 2016-05-26 Skymetro UAV Technology Inc. Unmanned aerial vehicle
CN105775151A (en) * 2016-01-29 2016-07-20 上海云舞网络科技有限公司 360 degree panoramic aerial photographing and video recording unmanned aerial vehicle and rack frame
CN106081141A (en) * 2016-06-08 2016-11-09 朱新科 Many rotor wing unmanned aerial vehicles

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20170197714A1 (en) * 2016-01-13 2017-07-13 Wolf-Tek, Llc Drone capable of operating in an aqueous environment
CN107914891B (en) * 2016-10-09 2020-03-31 比亚迪股份有限公司 Unmanned plane
CN206155807U (en) * 2016-11-17 2017-05-10 袁红泉 Current surveying unmanned aerial vehicle that makes a video recording
CN206265292U (en) * 2016-11-18 2017-06-20 捷西迪(广州)光学科技有限公司 A kind of unmanned aerial vehicle with retractable landing gear device

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN203246584U (en) * 2012-11-15 2013-10-23 深圳市大疆创新科技有限公司 Drive device for aircraft using tripod, landing gear and aircraft
CN103754355A (en) * 2014-01-10 2014-04-30 江苏艾锐泰克无人飞行器科技有限公司 Retractable landing gear and unmanned aerial vehicle
US20160144954A1 (en) * 2014-11-26 2016-05-26 Skymetro UAV Technology Inc. Unmanned aerial vehicle
CN104760690A (en) * 2015-04-23 2015-07-08 零度智控(北京)智能科技有限公司 Retractable landing gear of unmanned aircraft
CN105775151A (en) * 2016-01-29 2016-07-20 上海云舞网络科技有限公司 360 degree panoramic aerial photographing and video recording unmanned aerial vehicle and rack frame
CN106081141A (en) * 2016-06-08 2016-11-09 朱新科 Many rotor wing unmanned aerial vehicles

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10822082B2 (en) 2017-04-07 2020-11-03 Mark Holbrook Hanna Distributed-battery aerial vehicle and a powering method therefor
US11811224B2 (en) 2017-04-07 2023-11-07 Mark Holbrook Hanna Distributed-battery aerial vehicle and a powering method therefor
CN111746813A (en) * 2019-03-27 2020-10-09 东汉太阳能无人机技术有限公司 Lifting system for small-sized unmanned aerial vehicle
CN113739043A (en) * 2021-08-25 2021-12-03 四川公众项目咨询管理有限公司 Automatic change electric power construction supervision system
CN117533543A (en) * 2024-01-09 2024-02-09 山东国建土地房地产评估测绘有限公司 Territory space planning topography measuring device
CN117533543B (en) * 2024-01-09 2024-03-29 山东国建土地房地产评估测绘有限公司 Territory space planning topography measuring device

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