CN203512048U - Horizontal balancing device for camera in air - Google Patents

Horizontal balancing device for camera in air Download PDF

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Publication number
CN203512048U
CN203512048U CN201320331894.3U CN201320331894U CN203512048U CN 203512048 U CN203512048 U CN 203512048U CN 201320331894 U CN201320331894 U CN 201320331894U CN 203512048 U CN203512048 U CN 203512048U
Authority
CN
China
Prior art keywords
camera
pipe link
spring
air
balancing device
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
CN201320331894.3U
Other languages
Chinese (zh)
Inventor
张保空
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.)
SHANGHAI ZHONGRUI GENERAL AVIATION CO Ltd
Original Assignee
SHANGHAI ZHONGRUI GENERAL AVIATION 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 SHANGHAI ZHONGRUI GENERAL AVIATION CO Ltd filed Critical SHANGHAI ZHONGRUI GENERAL AVIATION CO Ltd
Priority to CN201320331894.3U priority Critical patent/CN203512048U/en
Application granted granted Critical
Publication of CN203512048U publication Critical patent/CN203512048U/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Abstract

The utility model discloses a horizontal balancing device for a camera in the air. The horizontal balancing device for the camera in the air comprises a left balancing spring, a right balancing spring, a spring connecting rod, a camera connecting rod and the camera. By the use of the horizontal balancing device for camera in air, left to right shake of the camera during the flight can be simply eliminated with safety and reliability.

Description

A kind of aerial camera horizontal equilibrium device
Technical field
The utility model belongs to machinery and controls application, relates in particular to a kind of aerial camera horizontal equilibrium device.
Background technology
Helicopter patrol flight refer to helicopter along about transmission line of electricity, be not less than the interval of 2 times of rotor diameter, and fly can see in the situation that visual, to reach the object of inspection, information acquisition and record to transmission line of electricity, in line walking process because needs carry out videograph to electric wireline state, therefore how aloft to avoid due to rocking that flight vibrations cause, held stationary, it is the key of video airlink record, therefore need to there is a kind of balancing device of aerial camera, can offset simple, safely, reliably aloft rocking.
Summary of the invention
The purpose of this utility model is to provide a kind of aerial camera horizontal equilibrium device, for a kind of aerial camera horizontal equilibrium device is provided, can offset simple, safely, reliably aloft double swerve.
The technical scheme that realizes above-mentioned purpose is: a kind of aerial camera horizontal equilibrium device, comprising: left balance spring, right balance spring, spring pipe link, camera pipe link and camera, wherein:
Left balance spring described in top, the left side at right angle setting of described spring pipe link, right balance spring described in top, the right side at right angle setting of described spring pipe link, camera pipe link described in the central lower at right angle setting of described spring pipe link, described camera is installed in the lower end of described camera pipe link.
Owing to having adopted the utility model device, a kind of aerial camera horizontal equilibrium device is provided, can offset simple, safely, reliably aloft double swerve.
Accompanying drawing explanation
Fig. 1 is structural representation of the present utility model.
The specific embodiment
Below in conjunction with accompanying drawing, the utility model is described in further detail.
Please refer to Fig. 1, in figure, provided a kind of aerial camera horizontal equilibrium device, comprising: left balance spring 1, right balance spring 2, spring pipe link 3, camera pipe link 4 and camera 5, wherein:
The left balance spring 1 of left side top at right angle setting of spring pipe link 3, the right balance spring 2 of right side top at right angle setting of spring pipe link 3, the central lower at right angle setting camera pipe link 4 of spring pipe link 3, camera 5 is installed in the lower end of camera extension bar 4.
Principle of work of the present utility model is: the Disturbance stress that utilizes elastically-deformable counterforce counteraction flight double swerve to produce, in order to a kind of aerial camera horizontal equilibrium device to be provided, can offset simple, safely, reliably aloft double swerve.
Below embodiment has been described in detail the utility model by reference to the accompanying drawings, and those skilled in the art can make many variations example to the utility model according to the above description.Thereby some details in embodiment should not form restriction of the present utility model, the utility model will be usingd scope that appended claims defines as protection domain of the present utility model.

Claims (1)

1. an aerial camera horizontal equilibrium device, is characterized in that, comprising: left balance spring, right balance spring, spring pipe link, camera pipe link and camera, wherein:
Left balance spring described in top, the left side at right angle setting of described spring pipe link, right balance spring described in top, the right side at right angle setting of described spring pipe link, camera pipe link described in the central lower at right angle setting of described spring pipe link, described camera is installed in the lower end of described camera pipe link.
CN201320331894.3U 2013-06-08 2013-06-08 Horizontal balancing device for camera in air Expired - Fee Related CN203512048U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201320331894.3U CN203512048U (en) 2013-06-08 2013-06-08 Horizontal balancing device for camera in air

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201320331894.3U CN203512048U (en) 2013-06-08 2013-06-08 Horizontal balancing device for camera in air

Publications (1)

Publication Number Publication Date
CN203512048U true CN203512048U (en) 2014-04-02

Family

ID=50371021

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201320331894.3U Expired - Fee Related CN203512048U (en) 2013-06-08 2013-06-08 Horizontal balancing device for camera in air

Country Status (1)

Country Link
CN (1) CN203512048U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106081143A (en) * 2016-08-26 2016-11-09 马人欢 Unmanned plane is taken photo by plane camera chain

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106081143A (en) * 2016-08-26 2016-11-09 马人欢 Unmanned plane is taken photo by plane camera chain
CN106081143B (en) * 2016-08-26 2018-06-05 吴春诚 Unmanned plane camera chain

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Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20140402

Termination date: 20210608

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