CN205872500U - Take anti -shock function's aircraft to shoot cloud platform - Google Patents

Take anti -shock function's aircraft to shoot cloud platform Download PDF

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Publication number
CN205872500U
CN205872500U CN201620725883.7U CN201620725883U CN205872500U CN 205872500 U CN205872500 U CN 205872500U CN 201620725883 U CN201620725883 U CN 201620725883U CN 205872500 U CN205872500 U CN 205872500U
Authority
CN
China
Prior art keywords
platform
suspension holdfast
mounting plate
photographic attachment
upper mounting
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
CN201620725883.7U
Other languages
Chinese (zh)
Inventor
王波
王运安
洪稳
王显斌
朱敬春
林泽军
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.)
Anhui Qiao Sen Electrical Polytron Technologies Inc
Original Assignee
Anhui Qiao Sen Electrical Polytron Technologies Inc
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 Anhui Qiao Sen Electrical Polytron Technologies Inc filed Critical Anhui Qiao Sen Electrical Polytron Technologies Inc
Priority to CN201620725883.7U priority Critical patent/CN205872500U/en
Application granted granted Critical
Publication of CN205872500U publication Critical patent/CN205872500U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model discloses a take anti -shock function's aircraft to shoot cloud platform, hold platform, lift kits and connection dead lever including photographic arrangement, photographic arrangement hold the platform through the round pin support connnection to the lift kits, lift kits's inside upper end is provided with the controller, the controller has battery jar and micro motor through the connection of electric lines, be connected with movable gear on micro motor's the main shaft, movable gear is connected with fixed gear with gear engagement's mode, fixed gear's lower extreme fixedly connected with cushion, lift kits's surface top is provided with down the platform, be provided with a plurality of ball down on the platform, the top of ball is the upper mounting plate, be provided with a plurality of through -hole on the upper mounting plate, the both sides of upper mounting plate are provided with the connection dead lever, be provided with the bolt hole on the connection dead lever, the utility model discloses simple structure, convenient to use takes shock -absorbing function certainly, can adapt to taking photo by plane of multiple weather.

Description

A kind of aircraft shooting tripod head of band function of seismic resistance
Technical field
This utility model relates to a kind of aircraft shooting field, the aircraft shooting cloud of a kind of band function of seismic resistance Platform.
Background technology
Common air craft carried shooting tripod head refers to the support works platform for installing imaging device, this imaging device bag Including video camera or photographing unit, imaging device is arranged on The Cloud Terrace, then by the adjustment to The Cloud Terrace, reaches to adjust imaging device Camera lens, the purpose of the correct shooting to target of realization, but owing to the motor bearings of existing The Cloud Terrace is by connected whole machine Frame and the weight of imaging device even load, due to long-term load, easily cause motor shaft deformation or damage, causing The Cloud Terrace to lose Surely, puzzlement is brought to shooting.
Utility model content
The purpose of this utility model is to provide the aircraft shooting tripod head of a kind of band function of seismic resistance, to solve above-mentioned background The problem proposed in technology.
For achieving the above object, the following technical scheme of this utility model offer:
The aircraft shooting tripod head of a kind of band function of seismic resistance, fixes including photographic attachment placing table, suspension holdfast and connection Bar;Described photographic attachment placing table is connected on suspension holdfast by pin;Described pin is welded as with photographic attachment placing table One entirety;Pin is flexibly connected with suspension holdfast;Pin is provided with pad with the junction of suspension holdfast;Described suspension holdfast Inner upper end be provided with controller;Described controller is connected by electric wire battery case and micromachine;Described battery case is solid Surely the top of photographic attachment placing table it is arranged on;Described micromachine is arranged on the right-hand member of controller;On the main shaft of micromachine Connect and have free gear;Described free gear connects in the way of gear engagement fixed gear;The lower end of described fixed gear It is fixedly connected with cushion block;Described cushion block is arranged on the top of photographic attachment placing table;Cushion block is fixing with photographic attachment placing table even Connecing is an entirety;Cushion block is the rigid material that hardness is higher;The outer surface top of suspension holdfast is provided with lower platform;Under described Platform and suspension holdfast are fixedly connected as an entirety;Several balls it are provided with on lower platform;Being arranged above of described ball Platform;Several through holes it are provided with on described upper mounting plate;The both sides of upper mounting plate are provided with the fixing bar of connection;Bar is fixed in described connection On be provided with bolt hole.
As further program of the utility model: described photographic attachment placing table is hollow frame structure.
As further program of the utility model: described suspension holdfast is inverted U-shaped.
As further program of the utility model: described ball is elastic rubber material.
As this utility model further scheme: described upper mounting plate is hexagonal.
Compared with prior art, the beneficial effects of the utility model are:
This utility model simple in construction, easy to use, the rubber ball that it is arranged can be good at reducing aircraft and flies Vibrations during row caused The Cloud Terrace, are conducive to the stability taken photo by plane, are provided with the micromachine in regulation direction, energy simultaneously in The Cloud Terrace Enough carry out multi-angle to take photo by plane, it is adaptable to the shooting under multiple weather.
Accompanying drawing explanation
Fig. 1 is the structural representation of the aircraft shooting tripod head of band function of seismic resistance.
Fig. 2 be band function of seismic resistance aircraft shooting tripod head in the structural representation of left view.
Fig. 3 be band function of seismic resistance aircraft shooting tripod head in the structural representation of top view.
In figure: 1-photographic attachment placing table, 2-suspension holdfast, 3-connects fixing bar, 4-pin, 5-pad, 6-cushion block, 7- Fixed gear, 8-battery case, 9-electric wire, 10-controller, 11-free gear, 12-micromachine, 13-lower platform, 14-ball, 15-upper mounting plate, 16-bolt hole, 17-through hole.
Detailed description of the invention
Below in conjunction with detailed description of the invention, the technical scheme of this patent is described in more detail.
Refer to Fig. 1-3, the aircraft shooting tripod head of a kind of band function of seismic resistance, including photographic attachment placing table 1, hang and prop up Frame 2 and the fixing bar 3 of connection;Described photographic attachment placing table 1 is hollow frame structure, is used for holding camera head and is acquired Photograph or image;Photographic attachment placing table 1 is connected on suspension holdfast 2 by pin 4;Described pin 4 is contained with photographic attachment Put platform 1 to be welded as a whole;Pin 4 is flexibly connected with suspension holdfast 2;Pin 4 is provided with pad with the junction of suspension holdfast 2 Sheet 5, in case excessive wear between pin 4 and suspension holdfast 2;Described suspension holdfast 2 is in inverted U-shaped;The inside of suspension holdfast 2 Upper end is provided with controller 10;Described controller 10 is connected by electric wire 9 battery case 8 and micromachine 12;Described battery case 8 It is fixedly installed on the top of photographic attachment placing table 1;Described micromachine 12 is arranged on the right-hand member of controller 10;Micromachine 12 Main shaft on connect have free gear 11;Described free gear 11 connects in the way of gear engagement fixed gear 7;Described solid The lower end of fixed gear 7 is fixedly connected with cushion block 6;Described cushion block 6 is arranged on the top of photographic attachment placing table 1;Cushion block 6 and photography Device placing table 1 is fixedly connected as an entirety;Cushion block 6 is the rigid material that hardness is higher, in order to avoid gear is engaged rotating Time deform;The outer surface top of suspension holdfast 2 is provided with lower platform 13;Described lower platform 13 is fixing with suspension holdfast 2 even Connecing is an entirety;Several balls 14 it are provided with on lower platform 13;Described ball 14 is elastic rubber material;Ball 14 upper Side is upper mounting plate 15;The described hexagonal shape of upper mounting plate 15;Several through holes 17 it are provided with, in order to reduce flight on upper mounting plate 15 Drag effect when device takes off;The both sides of upper mounting plate 15 are provided with the fixing bar 3 of connection;Described connection is fixed and is provided with spiral shell on bar 3 Keyhole 16, in order to be attached with aircraft.
Above the better embodiment of this patent is explained in detail, but this patent is not limited to above-mentioned embodiment party Formula, in the ken that one skilled in the relevant art is possessed, it is also possible on the premise of without departing from this patent objective Make a variety of changes.

Claims (5)

1. an aircraft shooting tripod head for band function of seismic resistance, fixes bar including photographic attachment placing table, suspension holdfast and connection; It is characterized in that, described photographic attachment placing table is connected on suspension holdfast by pin;Described pin holds with photographic attachment Platform is welded as a whole;Pin is flexibly connected with suspension holdfast;Pin is provided with pad with the junction of suspension holdfast;Described The inner upper end of suspension holdfast is provided with controller;Described controller is connected by electric wire battery case and micromachine;Described Battery case is fixedly installed on the top of photographic attachment placing table;Described micromachine is arranged on the right-hand member of controller;Micromachine Main shaft on connect have free gear;Described free gear connects in the way of gear engagement fixed gear;Described fixing tooth The lower end of wheel is fixedly connected with cushion block;Described cushion block is arranged on the top of photographic attachment placing table;Cushion block holds with photographic attachment Platform is fixedly connected as an entirety;Cushion block is the rigid material that hardness is higher;The outer surface top of suspension holdfast is provided with lower flat Platform;Described lower platform and suspension holdfast are fixedly connected as an entirety;Several balls it are provided with on lower platform;Described ball It is arranged above upper mounting plate;Several through holes it are provided with on described upper mounting plate;The both sides of upper mounting plate are provided with the fixing bar of connection;Described company Connect and be provided with bolt hole on fixing bar.
The aircraft shooting tripod head of band function of seismic resistance the most according to claim 1, it is characterised in that described photographic attachment is contained Putting platform is hollow frame structure.
The aircraft shooting tripod head of band function of seismic resistance the most according to claim 1, it is characterised in that described suspension holdfast in Inverted U-shaped.
The aircraft shooting tripod head of band function of seismic resistance the most according to claim 1, it is characterised in that described ball is elastic Elastomeric material.
The aircraft shooting tripod head of band function of seismic resistance the most according to claim 1, it is characterised in that described upper mounting plate is six Limit shape.
CN201620725883.7U 2016-07-11 2016-07-11 Take anti -shock function's aircraft to shoot cloud platform Expired - Fee Related CN205872500U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201620725883.7U CN205872500U (en) 2016-07-11 2016-07-11 Take anti -shock function's aircraft to shoot cloud platform

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201620725883.7U CN205872500U (en) 2016-07-11 2016-07-11 Take anti -shock function's aircraft to shoot cloud platform

Publications (1)

Publication Number Publication Date
CN205872500U true CN205872500U (en) 2017-01-11

Family

ID=57695467

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201620725883.7U Expired - Fee Related CN205872500U (en) 2016-07-11 2016-07-11 Take anti -shock function's aircraft to shoot cloud platform

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CN (1) CN205872500U (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107856871A (en) * 2017-10-18 2018-03-30 国网上海市电力公司 A kind of electric power unmanned plane inspection carrying head and unmanned plane
CN108609194A (en) * 2017-05-03 2018-10-02 李秀荣 A kind of unmanned plane

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108609194A (en) * 2017-05-03 2018-10-02 李秀荣 A kind of unmanned plane
CN109018399A (en) * 2017-05-03 2018-12-18 李秀荣 A kind of unmanned plane
CN107856871A (en) * 2017-10-18 2018-03-30 国网上海市电力公司 A kind of electric power unmanned plane inspection carrying head and unmanned plane

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Legal Events

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

Granted publication date: 20170111

Termination date: 20170711

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