CN206750169U - A kind of governor motion of unmanned plane shooting angle - Google Patents

A kind of governor motion of unmanned plane shooting angle Download PDF

Info

Publication number
CN206750169U
CN206750169U CN201720612359.3U CN201720612359U CN206750169U CN 206750169 U CN206750169 U CN 206750169U CN 201720612359 U CN201720612359 U CN 201720612359U CN 206750169 U CN206750169 U CN 206750169U
Authority
CN
China
Prior art keywords
servomotor
unmanned plane
fixed
shooting angle
governor motion
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
CN201720612359.3U
Other languages
Chinese (zh)
Inventor
黄仕平
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to CN201720612359.3U priority Critical patent/CN206750169U/en
Application granted granted Critical
Publication of CN206750169U publication Critical patent/CN206750169U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Landscapes

  • Toys (AREA)

Abstract

The utility model discloses a kind of governor motion of unmanned plane shooting angle, including fixed upper shell and the second servomotor fixing shell, the fixed upper shell is fixed on unmanned plane chassis by fixing nut, and fixed upper shell upper end inner surface is provided with the first servomotor, the second servomotor fixing shell rear end connects drive link, it connects drive link lower end and is connected with lower house terminal pad, and it is nested with bearing among connection drive link, photographic unit is installed, and photographic unit is fixed by clamp nut and lower casing body phase on the fixed bottom plate.The governor motion of the unmanned plane shooting angle is when needing fixed point to take photo by plane, pass through the servomotor of remote control control first and the second servomotor cooperating, from the shooting angle of main regulation photographic unit under unmanned plane vacant state, so as to reduce manipulation workload of the unmanned plane operator to unmanned plane, it is not necessary to which sophisticated technical staff can also complete this work.

Description

A kind of governor motion of unmanned plane shooting angle
Technical field
Unmanned plane accessory technical field is the utility model is related to, specially a kind of governor motion of unmanned plane shooting angle.
Background technology
Unmanned plane is unpiloted aircraft, is manipulated using radio robot and the presetting apparatus provided for oneself Not manned aircraft.Unmanned plane presses application field, can be divided into it is military with it is civilian.Military aspect, unmanned plane are divided into reconnaissance plane and target drone. Civilian aspect, unmanned plane+sector application, it is that unmanned plane has really just needed;At present take photo by plane, it is agricultural, plant protection, miniature self-timer, fast Pass transport, disaster relief, observation wild animal, monitoring infectious disease, mapping, news report, electric inspection process, the disaster relief, movies-making, The application in romance etc. field is manufactured, has greatly expanded the purposes of unmanned plane in itself, developed country is also in actively extension industry Using with developing unmanned air vehicle technique.
It is detailed to some special place progress due to needing but existing unmanned plane during taking photo by plane in real time Shooting carries out detailed shooting, it is necessary to be put over the ground from multiple angles.This just need to have very much experience and manipulation be skilled in technique it is special Industry manipulates technical staff and shot, and changing it using remote control control unmanned plane, different shooting angle is completed in the air Shoot work.
Utility model content
The purpose of this utility model is to provide a kind of governor motion of unmanned plane shooting angle, to solve above-mentioned background skill The existing unmanned plane fixed point proposed in art is taken photo by plane the problem of needing patent operator operation to complete to shoot work.
To achieve the above object, the utility model provides following technical scheme, a kind of regulation machine of unmanned plane shooting angle Structure, including fixed upper shell and the second servomotor fixing shell, the fixed upper shell are fixed on nobody by fixing nut On machine chassis, and fixed upper shell upper end inner surface is provided with the first servomotor, the first servomotor lower end and angle Adjustment housings are connected, and angular adjustment enclosure interior is provided with pulley, and the fixed upper shell side installation friend has heat emission hole, The second servomotor fixing shell lower end is connected with pulley, and is provided with second inside the second servomotor fixing shell Servomotor, the second servomotor front end is provided with drive gear, and drive gear passes through driving belt and position adjustments Gear is connected, and the second servomotor fixing shell rear end connects drive link, and it connects drive link lower end and connected with lower house Connect disk to be connected, and connect and be nested with bearing among drive link, the lower house terminal pad lower end is connected with photographic unit housing Connect, and photographic unit shell inner surface is provided with fixed bottom plate, installs photographic unit on the fixed bottom plate, and photographic unit passes through Clamp nut is fixed with lower casing body phase.
Preferably, first servomotor is connected wire using by way of being electrically connected with unmanned aerial vehicle (UAV) control mainboard Connect, the second servomotor is connected using OFDM communications with unmanned controller.
Preferably, the angular adjustment shell inner surface is provided with teeth groove, and it is adjusted by the way of engaged gears with position Section gear is mutually twisted.
Preferably, the angular adjustment housing and lower house are arc-shaped, and its radian is identical.
Preferably, the drive link is bascule, and it is along the upper and lower vertical movement of angular adjustment inner walls.
Preferably, the bearing outer ring uses soft rubber, and the diameter of bearing is bigger than through-hole diameter on lower house.
Compared with prior art, the beneficial effects of the utility model are:The governor motion of the unmanned plane shooting angle is needing Pinpoint when taking photo by plane, by the servomotor of remote control control first and the second servomotor cooperating, in unmanned plane hanging shape From the shooting angle of main regulation photographic unit under state, so as to reduce manipulation workload of the unmanned plane operator to unmanned plane, no Sophisticated technical staff is needed also to complete this work.Angular adjustment housing and lower house are arc-shaped, and its Radian is identical, is easy to the work in upper and lower shell body synchronously to carry out, and improves the regulation efficiency of shooting angle, bearing outer ring is using soft Body rubber, and the diameter of bearing is bigger than through-hole diameter on lower house, and lower house is hung using bearing, avoids it from coming off, Certain gap between angular adjustment housing lower end and fixed upper shell be present, and fixed upper shell is connected with angular adjustment housing Place is provided with limited location snap ring, between gap be easy to the rotation of angular adjustment housing, limited location snap ring is limited angle adjustment housings Position, prevent angular adjustment housing from position skew occurs.
Brief description of the drawings
Fig. 1 is the utility model structure diagram;
Fig. 2 is the utility model A points side mplifying structure schematic diagram;
Fig. 3 is the utility model A points front mplifying structure schematic diagram.
In figure:1st, fixed upper shell, 2, fixing nut, the 3, first servomotor, 4, angular adjustment housing, 5, heat emission hole, 6th, pulley, the 7, second servomotor fixing shell, the 8, second servomotor, 9, drive gear, 10, driving belt, 11, position adjusts Save gear, 12, drive link, 13, lower house terminal pad, 14, bearing, 15, photographic unit housing, 16, fixed bottom plate, 17, shooting Mechanism, 18, clamp nut, 19, lower house.
Embodiment
Below in conjunction with the accompanying drawing in the utility model embodiment, the technical scheme in the embodiment of the utility model is carried out Clearly and completely describing, it is clear that described embodiment is only the utility model part of the embodiment, rather than whole Embodiment.Based on the embodiment in the utility model, those of ordinary skill in the art are not under the premise of creative work is made The every other embodiment obtained, belong to the scope of the utility model protection.
Fig. 1-3 are referred to, the utility model provides a kind of technical scheme:A kind of governor motion of unmanned plane shooting angle, Including fixed upper shell 1, fixing nut 2, the first servomotor 3, angular adjustment housing 4, heat emission hole 5, pulley 6, the second servo Motor fixing shell 7, the second servomotor 8, drive gear 9, driving belt 10, position adjustments gear 11, drive link 12, lower casing Body terminal pad 13, bearing 14, photographic unit housing 15, fixed bottom plate 16, photographic unit 17, clamp nut 18 and lower house 19, Fixed upper shell 1 is fixed on unmanned plane chassis by fixing nut 2, and the fixed upper end inner surface of upper shell 1 is provided with first Servomotor 3, the first servomotor 3 are connected wire using by way of being electrically connected with unmanned aerial vehicle (UAV) control mainboard, and second Servomotor 8 is connected using OFDM communications with unmanned controller, the lower end of the first servomotor 3 and angular adjustment Housing 4 is connected, and pulley 6 is provided with inside angular adjustment housing 4, and angular adjustment housing 4 and lower house 19 are arc-shaped, And its radian is identical, it is easy to the work in upper and lower shell body synchronously to carry out, improves the regulation efficiency of shooting angle, angular adjustment shell Certain gap between the lower end of body 4 and fixed upper shell 1 be present, and fixed upper shell 1 is provided with the junction of angular adjustment housing 4 Limited location snap ring, between gap be easy to the rotation of angular adjustment housing 4, limited location snap ring carries out spacing to angle adjustment housings 4, prevents Position skew occurs for angle till degree adjustment housings 4, and the inner surface of angular adjustment housing 4 is provided with teeth groove, and it uses the side of engaged gears Formula is mutually twisted with position adjustments gear 11, and the fixed side of upper shell 1 installation friend has heat emission hole 5, and the second servomotor is fixed outer The lower end of shell 7 is connected with pulley 6, and the second servomotor 8, the second servo are provided with inside the second servomotor fixing shell 7 The front end of motor 8 is provided with drive gear 9, and drive gear 9 is connected by driving belt 10 with position adjustments gear 11, and second The rear end of servomotor fixing shell 7 connects drive link 12, and it connects the lower end of drive link 12 and is connected with lower house terminal pad 13, and Bearing 14 is nested among connection drive link 12, bearing 14 is relative with connection drive link 12 position to keep constant, operates, passes simultaneously Lever 12 is bascule, and it uses soft rubber along the upper and lower vertical movement of the inwall of angular adjustment housing 4, the outer ring of bearing 14, And the diameter of bearing 14 is bigger than through-hole diameter on lower house 19, lower house 19 is hung using bearing 14, avoids it from coming off, The lower end of lower house terminal pad 13 is connected with photographic unit housing 15, and the inner surface of photographic unit housing 15 is provided with fixed bottom plate 16, fix and photographic unit 17 is installed on bottom plate 16, and photographic unit 17 is fixed by clamp nut 18 and the phase of lower house 19.
Operation principle:Make in the governor motion using the unmanned plane shooting angle, photographic unit 17 is first placed on fixation On bottom plate 16, photographic unit 17 is fixed on photographic unit housing 15 using clamp nut 18, then by fixing nut 2 Fixed upper shell 1 is fixed on unmanned plane chassis, then connects the circuit connection of correlation, during unmanned plane during flying is taken photo by plane, First passing through controller control unmanned plane, level altitude spirals in the air, if only needing to adjust the bat of the horizontal direction of photographic unit 17 Angle is taken the photograph, the electric current that the first servomotor 3 can be turned on by the control mainboard of remote control control unmanned plane is allowed to work, The work of first servomotor 3 drives angular adjustment housing 4 be hinged therewith to rotate, so as to drive and the phase card of angular adjustment housing 4 The the second servomotor fixing shell 7 closed rotates, and drives lower house terminal pad 13 to rotate horizontally from there through drive link 12, so as to Adjust the horizontal shooting angle of photographic unit 17;If desired the space angle of photographic unit 17 is adjusted, it is necessary to the first servomotor 3 With the mutual cooperation work of the second servomotor 8, worked by the second servomotor of remote control control 8, the second servomotor 8 works Drive gear 9 is driven to rotate, the rotation of drive gear 9 drives position adjustments gear 11 to rotate by driving belt 10, is allowed to be engaged The teeth groove of the inner surface of angular adjustment housing 4 moves up and down, and drives photographic unit 17 to change its space from there through drive link 12 and claps Angle is taken the photograph, then coordinates the first servomotor 3 to be allowed to its angle of Level tune in space angle, so as to realize that spacial multi-angle is adjusted Section, is easy to the shooting work of photographic unit 17, and the above is the governor motion course of work of this unmanned plane shooting angle.
Although the utility model is described in detail with reference to the foregoing embodiments, come for those skilled in the art Say, it can still be modified to the technical scheme described in foregoing embodiments, or which part technical characteristic is entered Row equivalent substitution, all within the spirit and principles of the utility model, any modification, equivalent substitution and improvements made etc., all should Within the scope of protection of the utility model.

Claims (6)

1. a kind of governor motion of unmanned plane shooting angle, including fixed upper shell(1)With the second servomotor fixing shell (7), it is characterised in that:The fixed upper shell(1)Pass through fixing nut(2)It is fixed on unmanned plane chassis, and fixed upper casing Body(1)Upper end inner surface is provided with the first servomotor(3), first servomotor(3)Lower end and angular adjustment housing(4) It is connected, and angular adjustment housing(4)Inside is provided with pulley(6), the fixed upper shell(1)Side installation friend has heat emission hole (5), the second servomotor fixing shell(7)Lower end and pulley(6)It is connected, and the second servomotor fixing shell(7) Inside is provided with the second servomotor(8), second servomotor(8)Front end is provided with drive gear(9), and drive gear (9)Pass through driving belt(10)With position adjustments gear(11)It is connected, the second servomotor fixing shell(7)Rear end connects Connect drive link(12), it connects drive link(12)Lower end and lower house terminal pad(13)It is connected, and connects drive link(12)In Between be nested with bearing(14), the lower house terminal pad(13)Lower end and photographic unit housing(15)It is connected, and photographic unit Housing(15)Inner surface is provided with fixed bottom plate(16), the fixed bottom plate(16)Upper installation photographic unit(17), and photographic unit (17)Pass through clamp nut(18)With lower house(19)It is mutually fixed.
A kind of 2. governor motion of unmanned plane shooting angle according to claim 1, it is characterised in that:First servo Motor(3)It is connected wire using by way of being electrically connected with unmanned aerial vehicle (UAV) control mainboard, the second servomotor(8)Using OFDM communications are connected with unmanned controller.
A kind of 3. governor motion of unmanned plane shooting angle according to claim 1, it is characterised in that:The angular adjustment Housing(4)Inner surface is provided with teeth groove, and its by the way of engaged gears with position adjustments gear(11)It is mutually twisted.
A kind of 4. governor motion of unmanned plane shooting angle according to claim 1, it is characterised in that:The angular adjustment Housing(4)And lower house(19)It is arc-shaped, and its radian is identical.
A kind of 5. governor motion of unmanned plane shooting angle according to claim 1, it is characterised in that:The drive link (12)For bascule, and it is along angular adjustment housing(4)The upper and lower vertical movement of inwall.
A kind of 6. governor motion of unmanned plane shooting angle according to claim 1, it is characterised in that:The bearing(14) Outer ring uses soft rubber, and bearing(14)Diameter compare lower house(19)Upper through-hole diameter is big.
CN201720612359.3U 2017-05-29 2017-05-29 A kind of governor motion of unmanned plane shooting angle Expired - Fee Related CN206750169U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201720612359.3U CN206750169U (en) 2017-05-29 2017-05-29 A kind of governor motion of unmanned plane shooting angle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201720612359.3U CN206750169U (en) 2017-05-29 2017-05-29 A kind of governor motion of unmanned plane shooting angle

Publications (1)

Publication Number Publication Date
CN206750169U true CN206750169U (en) 2017-12-15

Family

ID=60621154

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201720612359.3U Expired - Fee Related CN206750169U (en) 2017-05-29 2017-05-29 A kind of governor motion of unmanned plane shooting angle

Country Status (1)

Country Link
CN (1) CN206750169U (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112591126A (en) * 2021-01-19 2021-04-02 广西华遥空间信息科技有限公司 Adjustable unmanned aerial vehicle capable of shipping and fixing aerial camera in multiple directions
CN113955104A (en) * 2020-07-20 2022-01-21 江苏雨能水利工程有限公司 Measure unmanned aerial vehicle linkage of hydrology
CN114264698A (en) * 2021-12-14 2022-04-01 石家庄东方热电热力工程有限公司 Photovoltaic power generation component hot spot fault point addressing device

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113955104A (en) * 2020-07-20 2022-01-21 江苏雨能水利工程有限公司 Measure unmanned aerial vehicle linkage of hydrology
CN112591126A (en) * 2021-01-19 2021-04-02 广西华遥空间信息科技有限公司 Adjustable unmanned aerial vehicle capable of shipping and fixing aerial camera in multiple directions
CN114264698A (en) * 2021-12-14 2022-04-01 石家庄东方热电热力工程有限公司 Photovoltaic power generation component hot spot fault point addressing device

Similar Documents

Publication Publication Date Title
CN206750169U (en) A kind of governor motion of unmanned plane shooting angle
US20200096844A1 (en) Method and system for motion camera with embedded gimbal
CN205554624U (en) Shooting equipment and unmanned aerial vehicle
CN205707410U (en) Multi-cam unmanned plane
CN106892097A (en) A kind of vehicle-mounted unmanned aerial vehicle for road condition monitoring
CN104859857A (en) Single-lens panoramic unmanned aerial vehicle system
WO2021098453A1 (en) Target tracking method and unmanned aerial vehicle
CN106218909A (en) Aircraft and system of taking photo by plane
CN105438488B (en) Aircraft and its control method and aerocraft system
CN107187587A (en) A kind of Intelligent unattended machine taken photo by plane for video display
CN110182375A (en) A kind of unmanned plane imaging sensor control device and its control method
CN206274111U (en) A kind of three axle panoramic shootings increase steady head
CN211167458U (en) Remote control unmanned aerial vehicle high altitude anti-wind anti-shake device
CN107416220A (en) A kind of governor motion of unmanned plane shooting angle
CN208264583U (en) A kind of moveable unmanned plane of holder
CN108995820B (en) Cloud platform, have shooting device and unmanned aerial vehicle of this cloud platform
CN106516140B (en) A kind of aircraft with aerial photography function
CN208903135U (en) A kind of wind resistance naval vessels unmanned plane dynamic target capture device based on binocular camera
CN205381413U (en) Integral type cloud platform camera and unmanned aerial vehicle
CN108860578A (en) A kind of unmanned plane surveying and mapping data acquisition device
CN205485642U (en) A mobility control device for photography equipment
CN205065226U (en) Remote control camera shooting pan -tilt
CN108639326A (en) A kind of unmanned plane for birding reproductive habit
CN215851972U (en) AI unmanned aerial vehicle test platform
CN207595281U (en) A kind of unmanned plane full angle image aerial device

Legal Events

Date Code Title Description
GR01 Patent grant
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20171215

Termination date: 20210529

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