CN206494136U - A kind of UAV flight's head - Google Patents

A kind of UAV flight's head Download PDF

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Publication number
CN206494136U
CN206494136U CN201621184394.1U CN201621184394U CN206494136U CN 206494136 U CN206494136 U CN 206494136U CN 201621184394 U CN201621184394 U CN 201621184394U CN 206494136 U CN206494136 U CN 206494136U
Authority
CN
China
Prior art keywords
head
protective cover
arm
shock
absorbing ball
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.)
Expired - Fee Related
Application number
CN201621184394.1U
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Chinese (zh)
Inventor
刘东方
朱思豪
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.)
Jiangsu Cloud Intelligent Technology Co Ltd
Original Assignee
Jiangsu Cloud Intelligent Technology Co Ltd
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 Jiangsu Cloud Intelligent Technology Co Ltd filed Critical Jiangsu Cloud Intelligent Technology Co Ltd
Priority to CN201621184394.1U priority Critical patent/CN206494136U/en
Application granted granted Critical
Publication of CN206494136U publication Critical patent/CN206494136U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model belongs to unmanned air vehicle technique field, specifically related to a kind of UAV flight's head, including battery carrier bottom plate and head shock-absorbing ball connection lower plate, battery carrier bottom plate and head shock-absorbing ball connection lower plate are connected by head shock-absorbing ball, head shock-absorbing ball connection lower plate downside is fixedly connected with electric rotating machine, the rear end of arc head linking arm is fixedly connected with from steady motor, inverted U-shaped head linking arm include left arm and right arm, protective cover is provided with the inside of inverted U-shaped head linking arm, protective cover is hollow sphere structure, video camera is installed in protective cover, right arm leading inside is fixedly connected with pitching motor, the output end of pitching motor on the right side of protective cover with being fixedly connected, left arm leading inside is provided with bearing, the left end of protective cover is provided with axostylus axostyle.The purpose is to:Solve existing most UAV flight's cradle head structures complicated, it is impossible to be fully achieved 360 ° and shot without dead angle, shooting effect is poor, and when lacking urgent landing the problems such as protector for pickup camara.

Description

A kind of UAV flight's head
Technical field
The utility model belongs to radio robot technical field, and in particular to a kind of UAV flight's head.
Background technology
UAV referred to as " unmanned plane ", is manipulated using radio robot and the presetting apparatus provided for oneself Not manned aircraft.Unmanned plane has that small volume, lightweight, expense are low, operation is flexible, it is safe the characteristics of, extensive use In taking photo by plane, detect, search and rescue, the field such as resource exploration.
Existing most UAV flight's cradle head structures are complicated, it is impossible to be fully achieved 360 ° and shot without dead angle, while unmanned plane It can produce and rock in flight operation process, video camera is waved up and down with unmanned plane, cause video camera often to catch not To target, the effect taken pictures is poor, and protector for pickup camara when lacking urgent landing, once unmanned plane promptly lands, takes the photograph Camera is very easy to be damaged.
Utility model content
The purpose of this utility model is:A kind of UAV flight's head is aimed to provide, for solving existing most unmanned planes Carry cradle head structure complicated, it is impossible to be fully achieved 360 ° and shot without dead angle, shooting effect is poor, and video camera when lacking urgent landing The problems such as protection device.
To realize above-mentioned technical purpose, the technical solution adopted in the utility model is as follows:
A kind of UAV flight's head, including battery carrier bottom plate and head shock-absorbing ball the connection lower plate be arrangeding in parallel, it is described Multiple head shock-absorbing balls are connected between battery carrier bottom plate and head shock-absorbing ball connection lower plate, the head shock-absorbing ball connects lower plate Downside is removably connected with electric rotating machine, and the clutch end of the electric rotating machine is connected with arc head linking arm, described The free end of arc head linking arm is removably connected with from steady motor, and the clutch end from steady motor is connected with down U Shape head linking arm, the inverted U-shaped head linking arm includes left arm, lateral connection arm and right arm, the power from steady motor Output end is connected with the middle part of lateral connection arm, and protective cover, the protective cover are provided with the inside of the inverted U-shaped head linking arm For hollow sphere structure, it is provided with the protective cover in connecting plate, the protective cover and is removably connected with video camera, it is described anti- Shield front end offers bar-shaped trough, and the camera of the video camera is located in bar-shaped trough, and the protective cover is removable by connecting plate Unload and be connected with pitching motor, clutch end and the right arm of the pitching motor are detachably connected, the left arm leading inside is set Have a bearing, the left end of the protective cover is provided with axostylus axostyle, and the outer ring of the bearing is fixedly connected with left arm, the inner ring of the bearing and Axostylus axostyle is connected.
Using the utility model of above-mentioned technical proposal, battery carrier bottom plate and head shock-absorbing ball connection lower plate pass through head damping Ball is connected, and head shock-absorbing ball does cushioning effect, stable, the guarantor that can also keep video camera to shoot when rocking when unmanned plane, tilt, accelerating Demonstrate,prove shooting effect;Video camera is controlled simultaneously by electric rotating machine, from steady motor and pitching motor, reaches that 360 ° of video camera is clapped without dead angle The purpose taken the photograph, video camera is arranged in protective cover, can be to taking the photograph using protective cover as the protection device of video camera during urgent landing Camera plays a good protective effect.
Further limit, the number of the head shock-absorbing ball is uniformly distributed for eight and along the rotary shaft of electric rotating machine, this The structure design of sample, can strengthen the self-stability energy of head.
Further limit, be uniformly provided with multiple slotted eyes in battery carrier bottom plate and head shock-absorbing ball the connection lower plate, so Structure design, can mitigate the weight of head, mitigate the burden of unmanned plane.
Further limit, battery carrier bottom plate and head shock-absorbing ball the connection lower plate is carbon plate, and such structure design can Further to mitigate the weight of head, mitigate the burden of unmanned plane.
Further limit, the video camera and protective cover are bolted to connection, such structure design, dismounting side Just, cost can also be simplified, it is cost-effective.
Brief description of the drawings
The nonlimiting examples that the utility model can be provided by accompanying drawing are further illustrated;
Fig. 1 is a kind of structural representation of UAV flight's head embodiment of the utility model;
Fig. 2 is the decomposition texture schematic diagram of part in Fig. 1;
Main element symbol description is as follows:
Battery carrier bottom plate 1, head shock-absorbing ball connection lower plate 2, head shock-absorbing ball 3, electric rotating machine 4, arc head linking arm 5th, from steady motor 6, inverted U-shaped head linking arm 7, left arm 71, right arm 72, pitching motor 8, protective cover 9, bar-shaped trough 91, connecting plate 92nd, bearing 10.
Embodiment
In order that the utility model may be better understood in those skilled in the art, it is right with reference to the accompanying drawings and examples Technical solutions of the utility model are further illustrated.
As depicted in figs. 1 and 2, a kind of UAV flight's head of the present embodiment, including the battery carrier bottom plate 1 be arrangeding in parallel Lower plate 2 is connected with head shock-absorbing ball, multiple head dampings are connected between battery carrier bottom plate 1 and head shock-absorbing ball connection lower plate 2 Ball 3, head shock-absorbing ball connection lower plate 2 downside is removably connected with electric rotating machine 4, the clutch end connection of electric rotating machine 4 There is arc head linking arm 5, the free end of arc head linking arm 5 is removably connected with from steady motor 6, from the dynamic of steady motor 6 Power output end is connected with inverted U-shaped head linking arm 7, and inverted U-shaped head linking arm 7 includes left arm 71, lateral connection arm and right arm 72, It is connected from the clutch end of steady motor 6 with the middle part of lateral connection arm, the inverted U-shaped inner side of head linking arm 7 is provided with protection Cover 9, protective cover 9 is to be provided with connecting plate 92, protective cover 9 to be removably connected with shooting in hollow sphere structure, protective cover 9 Machine, the front end of protective cover 9 offers bar-shaped trough 91, and the camera of video camera is located in bar-shaped trough 91, and protective cover 9 passes through connecting plate 92 Pitching motor 8 is removably connected with, clutch end and the right arm 72 of pitching motor 8 are detachably connected, the leading inside of left arm 71 Provided with bearing 10, the left end of protective cover 9 is provided with axostylus axostyle, and the outer ring of bearing 10 is fixedly connected with left arm 71, the inner ring of bearing 10 and Axostylus axostyle is connected, and the number of head shock-absorbing ball 3 is eight and is uniformly distributed along the rotary shaft of electric rotating machine 4, battery carrier bottom plate 1 and head shock-absorbing ball connection lower plate 2 on be uniformly provided with multiple slotted eyes, battery carrier bottom plate 1 and head shock-absorbing ball connection lower plate 2 are carbon Plate material, video camera and protective cover 9 are bolted to connection.
In the present embodiment, battery carrier bottom plate 1 and head shock-absorbing ball connection lower plate 2 are connected by head shock-absorbing ball 3, and head subtracts Shake ball 3 does cushioning effect, can also keep video camera to shoot stably when rocking when unmanned plane, tilt, accelerating, it is ensured that shooting effect; Video camera is controlled simultaneously by electric rotating machine 4, from steady motor 6 and pitching motor 8, reaches the mesh that 360 ° of video camera is shot without dead angle , video camera is arranged in protective cover 9, can be to video camera using protective cover 9 as the protection device of video camera during urgent landing Play a good protective effect.
It is preferred that the number of head shock-absorbing ball 3 is eight and is uniformly distributed along the rotary shaft of electric rotating machine 4, such structure Design, can strengthen the self-stability energy of head.In fact, also can be according to actual conditions, the specific quantity for considering head shock-absorbing ball 3 And distribution mode.
Multiple slotted eyes are uniformly provided with preferred battery frame bottom plate 1 and head shock-absorbing ball connection lower plate 2, such structure is set Meter, can mitigate the weight of head, mitigate the burden of aircraft.In fact, can also consider that other mitigate according to actual conditions The mode of weight.
It is carbon plate material, such structure design, Ke Yijin that preferred battery frame bottom plate 1 and head shock-absorbing ball, which connect lower plate 2, One step mitigates the weight of head, mitigates the burden of aircraft.In fact, can also consider that other mitigate weight according to actual conditions Mode.
It is preferred that video camera and protective cover 9 are bolted to connection, such structure design, convenient disassembly can also simplify Cost, it is cost-effective.In fact, also can be according to actual conditions, it is considered to other fixed forms, it be detachably connected as long as can realize .
A kind of UAV flight's head that the utility model is provided is described in detail above.Specific embodiment is said It is bright to be only intended to help and understand method of the present utility model and its core concept.It should be pointed out that for the common of the art For technical staff, on the premise of the utility model principle is not departed from, can also to the utility model carry out it is some improvement and Modification, these are improved and modification is also fallen into the utility model scope of the claims.

Claims (1)

1. a kind of UAV flight's head, it is characterised in that:Connect including the battery carrier bottom plate (1) be arrangeding in parallel and head shock-absorbing ball Lower plate (2) is connect, multiple head shock-absorbing balls are connected between the battery carrier bottom plate (1) and head shock-absorbing ball connection lower plate (2) (3), described head shock-absorbing ball connection lower plate (2) downside is removably connected with electric rotating machine (4), the electric rotating machine (4) Clutch end is connected with arc head linking arm (5), and the free end of the arc head linking arm (5) is removably connected with certainly Steady motor (6), the clutch end from steady motor (6) is connected with inverted U-shaped head linking arm (7), and the inverted U-shaped head connects Connecing arm (7) includes left arm (71), lateral connection arm and right arm (72), and the clutch end from steady motor (6) is with laterally connecting Connect and be provided with protective cover (9) on the inside of the middle part connection of arm, the inverted U-shaped head linking arm (7), during the protective cover (9) is It is provided with empty spherical structure, the protective cover (9) in connecting plate (92), the protective cover (9) and is removably connected with video camera, Protective cover (9) front end offers bar-shaped trough (91), and the camera of the video camera is located in bar-shaped trough (91), the protection Cover (9) is removably connected with pitching motor (8), the clutch end and right arm of the pitching motor (8) by connecting plate (92) (72) it is detachably connected, left arm (71) leading inside is provided with bearing (10), the left end of the protective cover (9) is provided with axostylus axostyle, The outer ring of the bearing (10) is fixedly connected with left arm (71), and inner ring and the axostylus axostyle of the bearing (10) are connected, the cloud The number of platform shock-absorbing ball (3) is eight and is uniformly distributed along the rotary shaft of electric rotating machine (4), the battery carrier bottom plate (1) and cloud Multiple slotted eyes, the battery carrier bottom plate (1) and head shock-absorbing ball connection lower plate are uniformly provided with platform shock-absorbing ball connection lower plate (2) (2) it is carbon plate, the video camera and protective cover (9) are bolted.
CN201621184394.1U 2016-10-27 2016-10-27 A kind of UAV flight's head Expired - Fee Related CN206494136U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201621184394.1U CN206494136U (en) 2016-10-27 2016-10-27 A kind of UAV flight's head

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201621184394.1U CN206494136U (en) 2016-10-27 2016-10-27 A kind of UAV flight's head

Publications (1)

Publication Number Publication Date
CN206494136U true CN206494136U (en) 2017-09-15

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Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107380473A (en) * 2017-09-18 2017-11-24 中国气象局兰州干旱气象研究所 A kind of vertical stable clouds terrace system and unmanned plane
CN107985617A (en) * 2017-10-27 2018-05-04 成都云瞰科技有限公司 A kind of double light photoelectric nacelles
CN108058839A (en) * 2017-12-25 2018-05-22 陈益德 A kind of multiaxis freely adjusts unmanned machine head
CN109178311A (en) * 2018-09-27 2019-01-11 广州市华科尔科技股份有限公司 A kind of double holder unmanned planes that shooting visual angle is wide
CN110293584A (en) * 2019-07-29 2019-10-01 韩城韩韩文旅产业发展集团有限公司 A kind of holder of video display Te Pai robot without dead angle

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107380473A (en) * 2017-09-18 2017-11-24 中国气象局兰州干旱气象研究所 A kind of vertical stable clouds terrace system and unmanned plane
CN107985617A (en) * 2017-10-27 2018-05-04 成都云瞰科技有限公司 A kind of double light photoelectric nacelles
CN108058839A (en) * 2017-12-25 2018-05-22 陈益德 A kind of multiaxis freely adjusts unmanned machine head
CN109178311A (en) * 2018-09-27 2019-01-11 广州市华科尔科技股份有限公司 A kind of double holder unmanned planes that shooting visual angle is wide
CN109178311B (en) * 2018-09-27 2024-02-20 广州市华科尔科技股份有限公司 Shooting visual angle is wide two cloud platform unmanned aerial vehicle
CN110293584A (en) * 2019-07-29 2019-10-01 韩城韩韩文旅产业发展集团有限公司 A kind of holder of video display Te Pai robot without dead angle

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GR01 Patent grant
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CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20170915

Termination date: 20181027

CF01 Termination of patent right due to non-payment of annual fee