WO2017128797A1 - 固定支架、云台、无人飞行器及成像装置 - Google Patents

固定支架、云台、无人飞行器及成像装置 Download PDF

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Publication number
WO2017128797A1
WO2017128797A1 PCT/CN2016/104292 CN2016104292W WO2017128797A1 WO 2017128797 A1 WO2017128797 A1 WO 2017128797A1 CN 2016104292 W CN2016104292 W CN 2016104292W WO 2017128797 A1 WO2017128797 A1 WO 2017128797A1
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WO
WIPO (PCT)
Prior art keywords
fixing bracket
carrier
clamping
bracket
sleeve
Prior art date
Legal status (The legal status 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 status listed.)
Ceased
Application number
PCT/CN2016/104292
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English (en)
French (fr)
Inventor
唐尹
戴仕声
潘大虎
杨飞虎
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
SZ DJI Technology Co Ltd
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SZ DJI Technology Co Ltd
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Filing date
Publication date
Application filed by SZ DJI Technology Co Ltd filed Critical SZ DJI Technology Co Ltd
Publication of WO2017128797A1 publication Critical patent/WO2017128797A1/zh
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D47/00—Equipment not otherwise provided for
    • B64D47/08—Arrangements of cameras
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16M—FRAMES, CASINGS OR BEDS OF ENGINES, MACHINES OR APPARATUS, NOT SPECIFIC TO ENGINES, MACHINES OR APPARATUS PROVIDED FOR ELSEWHERE; STANDS; SUPPORTS
    • F16M11/00—Stands or trestles as supports for apparatus or articles placed thereon ; Stands for scientific apparatus such as gravitational force meters
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16M—FRAMES, CASINGS OR BEDS OF ENGINES, MACHINES OR APPARATUS, NOT SPECIFIC TO ENGINES, MACHINES OR APPARATUS PROVIDED FOR ELSEWHERE; STANDS; SUPPORTS
    • F16M13/00—Other supports for positioning apparatus or articles; Means for steadying hand-held apparatus or articles
    • F16M13/02—Other supports for positioning apparatus or articles; Means for steadying hand-held apparatus or articles for supporting on, or attaching to, an object, e.g. tree, gate, window-frame, cycle

Definitions

  • the invention relates to a fixed bracket, a pan/tilt head, an unmanned aerial vehicle and an imaging device.
  • the pan/tilt is connected to the unmanned aerial vehicle or other carrier and is not completely fixed on the unmanned aerial vehicle or other carrier, and relative movement between the cloud platform and the unmanned aerial vehicle or other carrier occurs during transportation, resulting in The gimbal and the objects placed on the gimbal are not protected.
  • a fixed bracket for connecting a pan/tilt or a load and a carrier carrying the pan/tilt or load includes a holding member and a clamping portion connected to the holding member, the holding portion and the clamping portion are respectively configured to detachably connect the cloud platform and the carrier, and the fixing bracket can limit the cloud The relative motion between the stage and the carrier.
  • the fixing bracket further includes a sleeve portion fixedly connected to the holding member and the clamping portion, the sleeve portion for positioning a load mounted on the cloud platform.
  • the sleeve portion is provided with a receiving portion for receiving a part of the load.
  • the fixing bracket further includes a body fixedly connected to the holding member, the sleeve portion and the clamping portion, the body is provided with a receiving portion communicating with the receiving portion, and the receiving portion is used together with the receiving portion To accommodate the load.
  • the sleeve portion has a semi-cylindrical shape or a cylindrical shape.
  • the clamping portion includes a connecting portion connected to the holding member and a clamping sleeve connected to the connecting portion, and the clamping portion can be detachably connected to the carrier through the clamping sleeve.
  • central axis of the clamping sleeve and the central axis of the sleeve are perpendicular or parallel to each other.
  • a side of the clamping sleeve facing away from the holding component is provided with a handle, and the handle is used for assisting The fixing bracket is engaged or disengaged from the carrier.
  • the clamping sleeve is provided with a through hole penetrating the clamping sleeve and a card inlet communicating with the through hole, and the carrier can be inserted or disengaged from the inlet portion of the card to make the clamping sleeve Engaged or detached from the carrier.
  • the holding member can be elastically deformed to be clamped on the platform or to be elastically deformed to be detached from the platform, and the fixing bracket is detachably connected to the platform through the holder .
  • a pan/tilt head includes a first bracket and a second bracket and a third bracket rotatably coupled to the first bracket.
  • the pan/tilt further includes a fixing bracket as described above, and the fixing bracket is detachably coupled to the second bracket and the third bracket.
  • An unmanned aerial vehicle includes a fuselage.
  • the UAV also includes a pan/tilt as described above, the unmanned aerial vehicle being a carrier; the first bracket being rotatably coupled to the fuselage.
  • the UAV further includes a stand fixedly coupled to the body, and the UAV is detachably coupled to the fixed stand by the stand.
  • the tripod comprises two connecting segments connected to the fuselage and a supporting segment connected to the two connecting segments, the clamping portion being detachably connected to the connecting segment or the supporting segment.
  • An imaging apparatus includes a carrier and a cloud platform as described above, the carrier for carrying the platform, the platform being rotatably coupled to the carrier by the first bracket.
  • the imaging device further includes an imaging element mounted on the pan/tilt, the imaging element being a load.
  • the fixing bracket includes a holding member and a clamping portion connected to the holding member, and the holding portion and the clamping portion are respectively configured for detachably connecting the platform and the carrier, and the fixing The bracket can limit the relative movement between the platform and the carrier, and protect the platform and the load mounted on the platform.
  • FIG. 1 is a perspective view of a fixing bracket provided by a first embodiment of the present invention.
  • FIG. 2 is a structural schematic view of the fixing bracket of FIG. 1 along an angle.
  • FIG. 3 is a perspective view of an unmanned aerial vehicle having the fixed bracket of FIG. 1.
  • FIG. 4 is a perspective view of the head of the UAV of FIG. 3.
  • FIG. 5 is a schematic structural view of the fixing bracket according to the second embodiment of the present invention at an angle.
  • Fig. 6 is a structural schematic view of the fixing bracket of Fig. 5 taken along another angle.
  • Figure 7 is a perspective view of an unmanned aerial vehicle having the fixed bracket of Figure 5.
  • FIG. 8 is a perspective view of a fixing bracket according to a third embodiment of the present invention.
  • Figure 9 is a structural view of the fixing bracket of Figure 8 taken along an angle.
  • Figure 10 is a perspective view of an unmanned aerial vehicle having the fixed bracket of Figure 8.
  • Second fixed surface 151 Set up department 20, 20a, 20b Housing 21, 21a, 21b Stopper twenty two Holder 30, 30a, 30b Card surface 31 Hook 32 Grip 40, 40a, 40b Connection 41 Clamping sleeve 42,42a, 42b Through hole 421,421a,421b Card entry 43,43a, 43b Import face 44 handle 45
  • a component when referred to as being "fixed” to another component, it can be directly on the other component or the component can be present.
  • a component When a component is considered to "connect” another component, it can be directly connected to another component or possibly a central component.
  • a component When a component is considered to be “set to” another component, it can be placed directly on another component or possibly with a centered component.
  • a fixing bracket 100 according to a first embodiment of the present invention includes a body 10, a sleeve portion 20, a holding member 30, and a clamping portion 40.
  • the sleeve portion 20 and the card are provided.
  • the holding member 30 and the clamping portion 40 are fixedly coupled to the body 10.
  • the fixing bracket 100 is detachably connected to the platform and the carrier carrying the platform through the holding member 30 and the clamping portion 40.
  • the fixing bracket 100 can limit the relative movement between the platform and the carrier.
  • the number of the holding members 30 and the number of the clamping portions 40 are two, and one of the two holding members 30 and one of the two clamping portions 40 are located in the body 10 .
  • One side, the other of the two holding members 30 and the other of the two holding portions 40 are located on the other side of the body 10, the holding member 30 and the holding portion on the same side 40 phase connection; it can be understood that in other embodiments, the number of the holding members 30 and the number of the clamping portions 40 can be changed according to actual needs.
  • the sleeve portion 20 is spaced apart from the two holders 30.
  • the body 10 is used to fix a connection load such as a camera, a video camera or the like.
  • the main body 10 defines a receiving portion 11 for receiving the load.
  • the accommodating portion 11 is substantially rectangular. It can be understood that in other embodiments, the accommodating portion 11 may have other shapes, such as a square shape.
  • the accommodating portion 11 is formed with a first groove wall 12, a second groove wall 13 disposed opposite the first groove wall 12, and a third groove wall 14 between the first groove wall 12 and the second groove wall 13. And a fourth groove wall 15 , the third groove wall 14 is opposite to the fourth groove wall 15 .
  • the first groove wall 12 and the second groove wall 13 are vertically fixed on the bottom surface of the accommodating portion 11 .
  • the third groove wall 14 and the fourth groove wall 15 are fixedly connected to the bottom surface of the accommodating portion 11 and the angle formed between the third groove wall 14 and the bottom surface of the accommodating portion 11 is an obtuse angle.
  • the third groove wall 14 includes a first fixing surface 141 facing away from the bottom surface of the receiving portion 11 .
  • the fourth groove wall 15 includes a second fixing surface 151 facing away from the bottom surface of the receiving portion 11 .
  • the sleeve portion 20 is fixed on the second groove wall 13 of the body 10, and the sleeve portion 20 is used for positioning the load.
  • the sleeve portion 20 is substantially semi-cylindrical; in other embodiments, the sleeve portion 20 may have other shapes, such as a cylindrical shape, a square shape, or the like.
  • the sleeve portion 20 defines a receiving portion 21 that communicates with the receiving portion 11 for receiving a portion of the load.
  • the receiving portion 21 is a groove. It can be understood that in other embodiments, the internal shape of the receiving portion 21 may be different according to the shape of the load.
  • the two holding members 30 are respectively fixed to the first fixing surface 141 and the second fixing surface 151. Two of the holding members 30 are detachably connected to the platform.
  • each of the holding members 30 is substantially curved; each of the holding members 30 includes a holding surface 31 facing away from the corresponding clamping portion 40, and the holding surface 31 is a curved surface.
  • the two holding members 30 can be elastically deformed to be held on the platform.
  • Each of the clamping portions 40 includes a connecting portion 41 and a clamping sleeve 42 .
  • One end of the connecting portion 41 is fixedly connected to the body 10 and the corresponding holding member 30 , and the other end is connected to the clamping sleeve 42 .
  • the holder 40 is detachably coupled to the carrier by the clamping sleeve 42.
  • the clamping sleeve 42 is substantially semi-cylindrical, and the central axis of the clamping sleeve 42 is substantially perpendicular to the central axis of the sleeve portion 20.
  • the clamping sleeve 42 defines a through hole 421 and a card inlet 43 communicating with the through hole 421 , and the through hole 421 extends through the clamping sleeve 42 .
  • the card inlet 43 is for the card portion to be snapped into the through hole 421.
  • the card entry 43 includes two lead-in faces 44 that facilitate insertion of the carrier into the through-holes 421.
  • the two introduction faces 44 are substantially in the shape of an "eight".
  • the connecting portion 41 has a rod-like structure. It can be understood that the connecting portion 41 may be other structures such as a plate.
  • the connecting portion 41 may be made of a material such as rigidity, flexibility, or the like.
  • the unmanned aerial vehicle 200 having the fixing bracket 100 of the first embodiment of the present invention includes a body 201 and a stand 202 fixedly coupled to the body 201 , the body A platform 60 is coupled to the platform 60.
  • the mounting bracket 100 is detachably coupled to the platform 60 and the stand 202 for limiting relative movement of the platform 60 relative to the UAV 200.
  • the UAV 200 is a carrier.
  • the stand 202 is used to support the UAV 200 when the UAV 200 is landing.
  • the stand 202 is substantially in a "concave" shape, and includes two connecting segments 2021 fixedly coupled to the body 201 and a supporting portion 2022 fixedly coupled to the two connecting segments 2021.
  • the supporting segment 2022 is away from the body. 201 settings.
  • the number of the tripods 202 is two, and the two standoffs 202 are oppositely disposed.
  • the pan/tilt head 60 is located between the two standoffs 202.
  • the pan/tilt head 60 is rotatably coupled to the body 201, and the pan head 60 is mounted with an imaging element 50, which is a load.
  • the platform 60 includes a first bracket 61 rotatably coupled to the body 201 and a second bracket 62 and a third bracket 63 rotatably coupled to the first bracket 61.
  • the second bracket 62 and the third bracket 63 are opposite to each other.
  • the first bracket 61 rotates synchronously.
  • the second bracket 62 is disposed opposite to the third bracket 63.
  • the second bracket 62 includes a first supporting end 621, and the third bracket 63
  • the second support end 631 is included, and the first support end 621 and the second support end 631 are used in common to connect the imaging element 50.
  • the imaging element 50 is located between the first support end 621 and the second support end 631; the imaging element 50 is a camera.
  • the first bracket 61 of the platform 60 is rotatably coupled to the body 201 of the UAV 200.
  • the imaging element 50 is disposed on the first support end 621 of the second bracket 62 and the second support of the third bracket 63.
  • a connecting portion 2021 of each of the legs 202 is inserted into the clamping sleeve 42 of the clamping portion 40 of the fixing bracket 100 through the card inlet 43 , so that the corresponding connecting portion 2021 is received in the corresponding through hole 421 .
  • the fixing bracket 100 is detachably coupled to the UAV 200 by the clamping sleeve 42.
  • the connecting portion 2021 can be detached from the clamping sleeve 42 from the card inlet 43 by an external force, so that the clamping portion 40 is detached from the UAV 200.
  • the two holding members 30 can be elastically deformed, so that the two holding surfaces 31 are respectively supported on the first supporting end 621 and the second supporting end 631.
  • the fixing bracket 100 passes through the two holding members. 30 is detachably connected to the platform 60.
  • the two holding members 30 are elastically deformed, and the two holding surfaces 31 can be separated from the first supporting end 621 and the second supporting end 631 respectively, so that the two holding members 30 of the fixing bracket 100 are respectively Removed from the gimbal 60.
  • the fixing bracket 100 When the fixing bracket 100 is detachably connected to the platform 60 and the stand 202 of the UAV 200, the main body portion 51 of the imaging element 50 is received in the receiving portion 11 of the fixing bracket 100, and the imaging element 50 is The lens 52 is housed in the housing portion 21 of the sleeve portion 20. The imaging element 50 is fixed, and the platform 60 cannot be moved relative to the UAV 200.
  • the fixing bracket 100 can limit the relative movement of the platform 60 relative to the UAV 200, protect the PTZ 60 and the imaging element 50, and the fixing bracket 100 can be detachably connected to the PTZ 60 and the UAV 200 are easy to disassemble.
  • a fixing bracket 300 is substantially the same as the fixing bracket 100 provided by the first embodiment of the present invention.
  • the fixing bracket 300 includes a sleeve portion 20a, a holding member 30a and a clamping portion 40a.
  • the holding member 30a and the clamping portion 40a are fixedly connected to the sleeve portion 20a.
  • the number of the holding members 30a and the number of the holding portions 40a are two, and the two holding members 30a and the two holding portions 40a are respectively located on both sides of the sleeve portion 20a.
  • the holding member 30a on the same side and the holding portion 40a are connected.
  • the sleeve portion 20a is for positioning the load.
  • the sleeve portion 20a has a substantially cylindrical shape and is provided with a receiving portion 21a for accommodating a portion of the load.
  • the housing portion 21a is a through hole.
  • the holding member 30a is substantially the same as the holding member 30. The difference is that one side of the holding member 30a is provided with a hook 32 for holding the head.
  • the clamping portion 40a is substantially the same as the clamping portion 40, except that a side of the clamping portion 42a of the clamping portion 40a facing away from the sleeve portion 20a is provided with a handle 45 for assisting the clamping. The portion 40a is detached or snapped from the carrier.
  • the present invention provides an unmanned aerial vehicle 400 having a fixed bracket 300 according to a second embodiment of the present invention.
  • the unmanned aerial vehicle 400 is substantially identical to the unmanned aerial vehicle 200.
  • the fixed bracket 300 of the unmanned aerial vehicle 400 is provided. Unlike the fixed bracket 100 of the UAV 200.
  • a pan/tilt head 60 is disposed on the body 401 of the unmanned aerial vehicle 400.
  • the fixing bracket 300 is detachably connected to the platform 60 through the holding member 30a.
  • the first bracket 61 of the pan/tilt 60 is rotatably coupled to the body 401 of the UAV 400.
  • the main body portion 51 of the camera element 50 is disposed on the first support end 621 of the second bracket 62 and the third bracket 63.
  • a connecting portion 4021 of each of the legs 402 is inserted into the clamping sleeve 42a of the clamping portion 40a of the fixing bracket 300 through the card inlet 43a, so that the corresponding connecting portion 4021 is received in the corresponding through hole 421a.
  • the fixing bracket 300 is detachably coupled to the UAV 200 through the clamping sleeve 42a.
  • the connecting portion 4021 can be detached from the clamping sleeve 42a from the card inlet 43a by the handle 45, and the clamping portion 40a is detached from the unmanned aerial vehicle 400.
  • the two holding members 30a can be elastically deformed, so that the two hooks 32 are respectively supported on the first supporting end 621 and the second supporting end 631.
  • the fixing bracket 300 is detachable through the holding member 30a. Connected to the pan/tilt 60.
  • the two holding members 30a are elastically deformed, so that the two hooks 32 are respectively separated from the first supporting end 621 and the second supporting end 631, and the holding member 30a is detached from the platform 60.
  • the lens 52 of the imaging element 50 is received in the receiving portion 21a of the sleeve portion 20a, and the imaging element 50 is Fixed, the pan/tilt 60 is also incapable of producing relative motion with respect to the unmanned aerial vehicle 400.
  • a fixing bracket 500 is substantially the same as the fixing bracket 100 provided by the first embodiment of the present invention.
  • the difference lies in the sleeve portion 20b and the clamping portion 40b.
  • the central axis of the clamping sleeve 42b is substantially parallel to the central axis of the sleeve portion 20b.
  • a stop plate 22 is disposed at one end of the sleeve portion 20b away from the body 10b, and the stop plate 22 is configured to protect the receiving portion 21b of the sleeve portion 20b.
  • the lens 52 of the imaging element 50 is disposed on a side of the clamping portion 42b of the clamping portion 40b facing away from the sleeve portion 20b. The handle 45 facilitates the disengagement or snapping of the clamping portion 40b from the carrier.
  • the present invention provides an unmanned aerial vehicle 600 having a fixed bracket 500 according to a third embodiment of the present invention.
  • the unmanned aerial vehicle 600 is substantially the same as the unmanned aerial vehicle 200 provided by the present invention, except that the unmanned aerial vehicle 200
  • the fixed bracket 500 of the aircraft 600 includes a body 601 and a stand 602 fixedly coupled to the body 601.
  • the body 601 is coupled to the platform 60.
  • the fixed bracket 500 is detachably coupled to the platform 60 and the stand 602. .
  • the imaging unit 50 is disposed on the platform 60.
  • a support section 6022 of each of the legs 602 is inserted into the clamping sleeve 42b of the clamping portion 40b through the card inlet 43b of the clamping portion 40b of the fixing bracket 500, so that the corresponding supporting section 6022 is received in the corresponding one.
  • the fixing bracket 500 is detachably connected to the UAV 600 through the clamping sleeve 42b.
  • the support section 6022 can be detached from the clip sleeve 42b from the card inlet 43b by the handle, and the grip portion 40b is detached from the unmanned aerial vehicle 600.
  • the fixing bracket includes a holding member and a clamping portion connected to the holding member, and the holding portion and the clamping portion are respectively configured for detachably connecting the platform and the carrier, and the fixing The bracket can limit the relative movement between the platform and the carrier, and protect the platform and the load mounted on the platform.

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Handcart (AREA)
  • Studio Devices (AREA)

Abstract

一种固定支架(100，300，500)，其用于连接云台(60)或负载及承载云台(60)或负载的载体，固定支架(100，300，500)包括卡持件(30，30a，30b)及与卡持件(30，30a，30b)相连接的夹持部(40，40a，40b)，卡持件(30，30a，30b)及夹持部(40，40a，40b)分别用于可拆卸的连接云台(60)及载体，固定支架(100，300，500)能够限制云台(60)与载体之间的相对运动。以及具有固定支架(100，300，500)的云台(60)、无人飞行器(200，400，600)及成像装置。

Description

固定支架、云台、无人飞行器及成像装置 技术领域
本发明涉及一种固定支架、云台、无人飞行器及成像装置。
背景技术
一般云台连接于无人飞行器或者其他载体上且没有完全固定在该无人飞行器或者其他载体上，在运输过程中该云台与该无人飞行器或者其他载体之间会产生相对运动，导致该云台及设置在该云台上的物体得不到保护。
发明内容
有鉴于此，有必要提供一种能够限制云台晃动的固定支架。还有必要提供一种云台、无人飞行器及成像装置。
一种固定支架，其用于连接云台或负载及承载该云台或负载的载体。该固定支架包括卡持件及与该卡持件相连接的夹持部，该卡持件及该夹持部分别用于可拆卸的连接该云台及该载体，该固定支架能够限制该云台与该载体之间的相对运动。
进一步的，该固定支架还包括与该卡持件及该夹持部固定连接的套设部，该套设部用于定位安装于该云台的负载。
进一步的，该套设部开设有容纳部，该容纳部用于收容部分该负载。
进一步的，该固定支架还包括固定连接该卡持件、该套设部及该夹持部的本体，该本体开设有与该容纳部相连通的收容部，该收容部与该容纳部共同用于收容该负载。
进一步的，该套设部呈半圆筒状或者圆筒状。
进一步的，该夹持部包括与该卡持件相连接的连接部及与该连接部相连接的夹持套，该夹持部能够通过该夹持套可拆卸的连接于该载体。
进一步的，该夹持套的中心轴与该套设部的中心轴相互垂直或者相互平行。
进一步的，该夹持套背离该卡持件的一侧设置有把手，该把手用于辅助 该固定支架与该载体相卡接或者相脱离。
进一步的，该夹持套开设有贯穿该夹持套的通孔及与该通孔相连通的卡入口，该载体能够通过该卡入口部分的卡入或者脱离该通孔，使该夹持套与该载体相卡接或者相脱离。
进一步的，该卡持件能够产生弹性变形以卡持在该云台上或者恢复弹性变形以使自身能够与该云台相脱离，该固定支架通过该卡持件与该云台可拆卸的连接。
一种云台，其包括第一支架及与该第一支架转动连接的第二支架及第三支架。该云台还包括如上所述的固定支架，该固定支架可拆卸的连接于该第二支架及该第三支架。
一种无人飞行器，其包括机身。该无人飞行器还包括如上所述的云台，该无人飞行器即为载体；该第一支架转动的连接于该机身。
进一步的，该无人飞行器还包括与该机身固定连接的脚架，该无人飞行器通过该脚架与该固定支架可拆卸连接。
进一步的，该脚架包括两个连接于该机身的连接段及连接于两个该连接段的支撑段，该夹持部可拆卸的连接于该连接段或者该支撑段。
一种成像装置，其包括载体及如上所述的云台，该载体用于承载该云台，该云台通过该第一支架可转动的连接于该载体。
进一步的，该成像装置还包括拍摄元件，该拍摄元件安装在该云台上，该拍摄元件即为负载。
上述的固定支架，该固定支架包括卡持件及与该卡持件相连接的夹持部，该卡持件及该夹持部分别用于可拆卸的连接该云台及该载体，该固定支架能够限制该云台与该载体之间的相对运动，保护了该云台及安装在该云台上的负载。
附图说明
图1是本发明第一实施方式提供的固定支架的立体示意图。
图2是图1中的固定支架沿一角度的结构示意图。
图3是具有图1中的固定支架的无人飞行器的立体示意图。
图4是图3中的无人飞行器的云台的立体示意图。
图5是本发明第二实施方式提供的固定支架沿一角度的结构示意图。
图6是图5中的固定支架沿另一角度的结构示意图。
图7是具有图5中的固定支架的无人飞行器的立体示意图。
图8是本发明第三实施方式提供的固定支架的立体示意图。
图9是图8中的固定支架沿一角度的结构示意图。
图10是具有图8中的固定支架的无人飞行器的立体示意图。
主要元件符号说明
固定支架 100,300,500
本体 10，10b
收容部 11
第一槽壁 12
第二槽壁 13
第三槽壁 14
第一固定面 141
第四槽壁 15
第二固定面 151
套设部 20,20a,20b
容纳部 21,21a,21b
止挡板 22
卡持件 30,30a,30b
卡持面 31
卡钩 32
夹持部 40，40a，40b
连接部 41
夹持套 42，42a，42b
通孔 421，421a，421b
卡入口 43,43a，43b
导入面 44
把手 45
拍摄元件 50
主体部 51
镜头 52
云台 60
第一支架 61
第二支架 62
第一支撑端 621
第三支架 63
第二支撑端 631
无人飞行器 200,400,600
机身 201,401,601
脚架 202,402,602
连接段 2021,4021
支撑段 2022,4022,6022
如下具体实施方式将结合上述附图进一步说明本发明。
具体实施方式
下面将结合本发明实施例中的附图，对本发明实施例中的技术方案进行清楚、完整地描述，显然，所描述的实施例仅仅是本发明一部分实施例，而不是全部的实施例。基于本发明中的实施例，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，都属于本发明保护的范围。
需要说明的是，当组件被称为“固定于”另一个组件，它可以直接在另一个组件上或者也可以存在居中的组件。当一个组件被认为是“连接”另一个组件，它可以是直接连接到另一个组件或者可能同时存在居中组件。当一个组件被认为是“设置于”另一个组件，它可以是直接设置在另一个组件上或者可能同时存在居中组件。
除非另有定义，本文所使用的所有的技术和科学术语与属于本发明的技术领域的技术人员通常理解的含义相同。本文中在本发明的说明书中所使用的术语只是为了描述具体的实施例的目的，不是旨在于限制本发明。本文所使用的术语“及/或”包括一个或多个相关的所列项目的任意的和所有的组 合。
下面结合附图，对本发明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。
请一并参阅图1及图2，本发明第一实施方式提供的固定支架100，其包括本体10、套设部20、卡持件30及夹持部40，该套设部20、该卡持件30及该夹持部40均固定连接在该本体10上。该固定支架100通过该卡持件30及该夹持部40分别可拆卸的连接于云台及承载该云台的载体，该固定支架100能够限制该云台与该载体之间的相对运动。本实施方式中，该卡持件30的数量及该夹持部40的数量均为两个，两个该卡持件30中的一个及两个该夹持部40中的一个位于该本体10的一侧，两个该卡持件30中的另一个及两个该夹持部40中的另一个位于该本体10的另一侧，位于同一侧的该卡持件30及该夹持部40相连接；可以理解，在其他实施方式中，该卡持件30的数量及该夹持部40的数量均可以根据实际需要改变。该套设部20与两个该卡持件30间隔设置。
该本体10用于固定连接负载，如相机、摄像机等。该本体10开设有收容部11，该收容部11用于收容该负载。本实施方式中，该收容部11基本呈矩形；可以理解，在其他实施方式中，该收容部11还可以为其他形状，如方形等。该收容部11形成有第一槽壁12、与该第一槽壁12相对设置的第二槽壁13及位于该第一槽壁12及该第二槽壁13之间的第三槽壁14及第四槽壁15，该第三槽壁14与该第四槽壁15相对设置。该第一槽壁12与该第二槽壁13垂直固定在该收容部11的底面上。该第三槽壁14与该第四槽壁15固定连接该收容部11的底面，且与该收容部11的底面之间形成的夹角均为钝角。该第三槽壁14包括背离该收容部11的底面的第一固定面141。该第四槽壁15包括背离该收容部11的底面的第二固定面151。
该套设部20固定在该本体10的第二槽壁13上，该套设部20用于定位该负载。本实施方式中，该套设部20基本呈半圆筒状；可以理解，在其他实施方式中，该套设部20可以为其他形状，如圆筒状，方框状等。该套设部20开设有与该收容部11相连通的容纳部21，该容纳部21用于收容部分该负载。本实施方式中，该容纳部21为凹槽。可以理解，在其他实施方式中，该容纳部21的内部形状依据该负载的外形不同可以有所不同。
两个该卡持件30分别固定在该第一固定面141及该第二固定面151上。两个该卡持件30可拆卸的连接于该云台。本实施方式中，每个该卡持件30基本呈弧形；每个该卡持件30包括一背离对应的该夹持部40的卡持面31，该卡持面31为弧面。两个该卡持件30能够发生弹性变形以卡持在该云台上。
两个该夹持部40固定连接在该本体10上，两个该夹持部40可拆卸的连接于该载体。每个该夹持部40包括连接部41及夹持套42，该连接部41的一端固定连接于该本体10及对应的该卡持件30，另一端连接于该夹持套42，该夹持部40通过该夹持套42可拆卸的连接于该载体。本实施方式中，该夹持套42大致为半圆筒状，该夹持套42的中心轴与该套设部20的中心轴基本垂直。该夹持套42开设有通孔421及与该通孔421相连通的卡入口43，该通孔421贯穿该夹持套42。该卡入口43用于供该载体部分的卡入该通孔421内。该卡入口43包括两个导入面44，该导入面44便于该载体卡入该通孔421。本实施方式中，两个该导入面44基本呈“八”字型。本实施例中，所述连接部41为杆状结构，可以理解，所述连接部41也可以为其他如板状等结构。所述连接部41可以为刚性、柔性等材料制成。
请参阅图3及图4，本发明提供的具有本发明第一实施方式的固定支架100的无人飞行器200，其包括机身201及固定连接于该机身201的脚架202，该机身201连接有云台60，该固定支架100可拆卸的连接于该云台60及该脚架202，该固定支架100用于限制该云台60相对于该无人飞行器200的相对运动。该无人飞行器200即为载体。
该脚架202用于该无人飞行器200着陆时支撑该无人飞行器200。该脚架202基本呈“凹”字型，其包括两个固定连接于该机身201的连接段2021及与两个该连接段2021固定连接的支撑段2022，该支撑段2022远离该机身201设置。本实施方式中，该脚架202的数量为两个，两个该脚架202相对设置，该云台60位于两个该脚架202之间。
该云台60可转动地连接于该机身201，该云台60上安装有拍摄元件50，该拍摄元件50为负载。该云台60包括与该机身201转动连接的第一支架61及与该第一支架61转动连接的第二支架62及第三支架63，该第二支架62及该第三支架63能够相对于该第一支架61同步转动。该第二支架62与该第三支架63相对设置，该第二支架62包括第一支撑端621，该第三支架63 包括第二支撑端631，该第一支撑端621及该第二支撑端631共同用于连接该拍摄元件50。本实施方式中，该拍摄元件50位于该第一支撑端621及该第二支撑端631之间；该拍摄元件50为相机。
该云台60的第一支架61转动的连接于该无人飞行器200的机身201，该拍摄元件50设置在该第二支架62的第一支撑端621及该第三支架63的第二支撑端631上。每个该脚架202的一个连接段2021通过该卡入口43卡入该固定支架100的夹持部40的夹持套42，使对应的该连接段2021收容在对应的该通孔421内，该固定支架100通过该夹持套42可拆卸的连接于该无人飞行器200。当然，该连接段2021可以在外力作用下自该卡入口43脱离该夹持套42，从而使该夹持部40自该无人飞行器200上拆卸下来。
两个该卡持件30能够发生弹性变形，使两个该卡持面31分别卡持在该第一支撑端621及该第二支撑端631上，该固定支架100通过两个该卡持件30可拆卸的连接于该云台60。当然，两个该卡持件30恢复弹性变形，两个该卡持面31能够分别脱离该第一支撑端621及该第二支撑端631，使该固定支架100的两个该卡持件30自该云台60拆卸下来。该固定支架100可拆卸的连接于该云台60及该无人飞行器200的脚架202时，该拍摄元件50的主体部51收容在该固定支架100的收容部11内，该拍摄元件50的镜头52收容在该套设部20的容纳部21内，该拍摄元件50被固定，该云台60亦不能相对于该无人飞行器200产生相对运动。
本实施方式中，该固定支架100能够限制该云台60相对于该无人飞行器200的相对运动，保护了该云台60及该拍摄元件50，且该固定支架100能够拆卸的连接该云台60及该无人飞行器200，拆卸方便。
请参阅图5及图6，本发明第二实施方式提供的固定支架300，该固定支架300与本发明第一实施方式提供的固定支架100基本相同。该固定支架300包括套设部20a、卡持件30a及夹持部40a，该卡持件30a及该夹持部40a固定连接在该套设部20a上。本实施方式中，该卡持件30a的数量及该夹持部40a的数量均为两个，两个该卡持件30a及两个该夹持部40a分别位于该套设部20a的两侧，位于同一侧的该卡持件30a及该夹持部40a相连接。
该套设部20a用于定位该负载。该套设部20a基本呈圆筒状，其开设有容纳部21a，该容纳部21a用于收容部分该负载。本实施方式中，该容纳部 21a为通孔。
该卡持件30a与该卡持件30基本相同，不同点在于该卡持件30a的一侧设置有卡钩32，该卡钩32用于卡持该云台。该夹持部40a与该夹持部40基本相同，不同点在于该夹持部40a的夹持套42a背离该套设部20a的一侧设置有把手45，该把手45用于辅助该夹持部40a与该载体的脱离或者卡接。
请参阅图7，本发明提供的具有本发明第二实施方式提供的固定支架300的无人飞行器400，该无人飞行器400与该无人飞行器200基本相同，该无人飞行器400的固定支架300不同于该无人飞行器200的固定支架100。
该无人飞行器400的机身401上设置有云台60。该固定支架300通过该卡持件30a可拆卸的连接于该云台60。该云台60的第一支架61转动的连接于该无人飞行器400的机身401，该拍摄元件50的主体部51设置在该第二支架62的第一支撑端621及该第三支架63的第二支撑端631上。每个该脚架402的一个连接段4021通过该卡入口43a卡入该固定支架300的夹持部40a的夹持套42a，使对应的该连接段4021收容在对应的该通孔421a内，该固定支架300通过该夹持套42a可拆卸的连接于该无人飞行器200。当然，该连接段4021可以通过该把手45自该卡入口43a脱离该夹持套42a，该夹持部40a自该无人飞行器400上拆卸下来。
两个该卡持件30a能够发生弹性变形，使两个该卡钩32分别卡持在该第一支撑端621及该第二支撑端631上，该固定支架300通过该卡持件30a可拆卸的连接于该云台60。当然，两个该卡持件30a恢复弹性变形，使两个该卡钩32分别脱离该第一支撑端621及该第二支撑端631，该卡持件30a自该云台60拆卸下来。该固定支架300可拆卸的连接于该云台60及该无人飞行器400的脚架402时，该拍摄元件50的镜头52收容在该套设部20a的容纳部21a内，该拍摄元件50被固定，该云台60亦不能相对于该无人飞行器400产生相对运动。
请参阅图8及图9，本发明第三实施方式提供的固定支架500，该固定支架500与本发明第一实施方式提供的固定支架100基本相同。不同点在于该套设部20b及该夹持部40b。本实施方式中，该夹持套42b的中心轴与该套设部20b的中心轴基本平行。该套设部20b远离该本体10b的一端设置有一止挡板22，该止挡板22用于保护收容在该套设部20b的容纳部21b内的 该拍摄元件50的镜头52。该夹持部40b的夹持套42b背离该套设部20b的一侧设置有把手45，该把手45便于该夹持部40b与该载体的脱离或者卡接。
请参阅图10，本发明提供的具有本发明第三实施方式提供的固定支架500的无人飞行器600，该无人飞行器600与本发明提供的无人飞行器200基本相同，不同点在于该无人飞行器600的固定支架500。该无人飞行器600包括机身601及固定连接于该机身601的脚架602，该机身601连接有云台60，该固定支架500可拆卸的连接于该云台60及该脚架602。该云台60上设置有该拍摄元件50。每个该脚架602的一个支撑段6022通过该固定支架500的夹持部40b的卡入口43b卡入该夹持部40b的夹持套42b，使对应的该支撑段6022收容在对应的该通孔421b内，该固定支架500通过该夹持套42b可拆卸的连接于该无人飞行器600。当然，该支撑段6022可以通过该把手自该卡入口43b脱离该夹持套42b，该夹持部40b自该无人飞行器600上拆卸下来。
上述的固定支架，该固定支架包括卡持件及与该卡持件相连接的夹持部，该卡持件及该夹持部分别用于可拆卸的连接该云台及该载体，该固定支架能够限制该云台与该载体之间的相对运动，保护了该云台及安装在该云台上的负载。
另外，本技术领域的普通技术人员应当认识到，以上的实施方式仅是用来说明本发明，而并非用作为对本发明的限定，只要在本发明的实质精神范围之内，对以上实施例所作的适当改变和变化都落在本发明要求保护的范围之内。

Claims (16)

  1. 一种固定支架，其用于连接云台或负载及承载该云台或负载的载体，其特征在于：该固定支架包括卡持件及与该卡持件相连接的夹持部，该卡持件及该夹持部分别用于可拆卸的连接该云台及该载体，该固定支架能够限制该云台与该载体之间的相对运动。
  2. 如权利要求1所述的固定支架，其特征在于：该固定支架还包括与该卡持件及该夹持部固定连接的套设部，该套设部用于定位安装于该云台的负载。
  3. 如权利要求2所述的固定支架，其特征在于：该套设部开设有容纳部，该容纳部用于收容部分该负载。
  4. 如权利要求3所述的固定支架，其特征在于：该固定支架还包括固定连接该卡持件、该套设部及该夹持部的本体，该本体开设有与该容纳部相连通的收容部，该收容部与该容纳部共同用于收容该负载。
  5. 如权利要求2所述的固定支架，其特征在于：该套设部呈半圆筒状或者圆筒状。
  6. 如权利要求2所述的固定支架，其特征在于：该夹持部包括与该卡持件相连接的连接臂及与该连接臂相连接的夹持套，该夹持部能够通过该夹持套可拆卸的连接于该载体。
  7. 如权利要求6所述的固定支架，其特征在于：该夹持套的中心轴与该套设部的中心轴相互垂直或者相互平行。
  8. 如权利要求6所述的固定支架，其特征在于：该夹持套背离该卡持件的一侧设置有把手，该把手用于辅助该固定支架与该载体相卡接或者相脱离。
  9. 如权利要求6所述的固定支架，其特征在于：该夹持套开设有贯穿该夹持套的通孔及与该通孔相连通的卡入口，该载体能够通过该卡入口卡入或者脱离该通孔，使该夹持套与该载体相卡接或者相脱离。
  10. 如权利要求1所述的固定支架，其特征在于：该卡持件能够产生弹性变形以卡持在该云台上或者恢复弹性变形以使自身能够与该云台相脱离，该固定支架通过该卡持件与该云台可拆卸的连接。
  11. 一种云台，其包括第一支架及与该第一支架转动连接的第二支架及第三支架，其特征在于：该云台还包括如权利要求1-10任一项所述的固定支架，该固定支架可拆卸的连接于该第二支架及该第三支架。
  12. 一种无人飞行器，其包括机身，其特征在于：该无人飞行器还包括如权利要求11所述的云台，该无人飞行器即为载体；该第一支架转动的连接于该机身。
  13. 如权利要求12所述的无人飞行器，其特征在于：该无人飞行器还包括与该机身固定连接的脚架，该无人飞行器通过该脚架与该固定支架可拆卸连接。
  14. 如权利要求13所述的无人飞行器，其特征在于：该脚架包括两个连接于该机身的连接段及连接于两个该连接段的支撑段，该夹持部可拆卸的连接于该连接段或者该支撑段。
  15. 一种成像装置，其包括载体及如权利要求11所述的云台，该载体用于承载该云台，该云台通过该第一支架可转动的连接于该载体。
  16. 如权利要求15所述的成像装置，其特征在于：该成像装置还包括拍摄元件，该拍摄元件安装在该云台上，该拍摄元件即为负载。
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CN106715268B (zh) * 2016-09-21 2019-04-23 深圳市大疆灵眸科技有限公司 云台固定架及具有该云台固定架的无人机
CN106794903B (zh) * 2016-09-23 2020-07-07 深圳市大疆创新科技有限公司 减震板及具有该减震板的无人飞行器
CN215475711U (zh) * 2020-11-09 2022-01-11 深圳市大疆创新科技有限公司 无人飞行器
CN115230976A (zh) * 2022-07-05 2022-10-25 港珠澳大桥管理局 无人机载荷快速拆装装置
CN115560214B (zh) * 2022-08-29 2026-02-27 中国航空无线电电子研究所 一种直升机试飞用自适应悬挂相机支架机构

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