CN203114997U - Base damper - Google Patents
Base damper Download PDFInfo
- Publication number
- CN203114997U CN203114997U CN 201220743058 CN201220743058U CN203114997U CN 203114997 U CN203114997 U CN 203114997U CN 201220743058 CN201220743058 CN 201220743058 CN 201220743058 U CN201220743058 U CN 201220743058U CN 203114997 U CN203114997 U CN 203114997U
- Authority
- CN
- China
- Prior art keywords
- shock absorbing
- base
- absorbing rubber
- fixing bolt
- damping rubber
- 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
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- Vibration Prevention Devices (AREA)
Abstract
The utility model belongs to a base damper used for aero plotting equipment and particularly applied to a camera of the aero plotting equipment. The base damper is characterized in that a fixing bolt is arranged on an airplane fixing board base, a locating sleeve, a flat washer and a butterfly nut are arranged on the fixing bolt, upper damping rubber and lower damping rubber are arranged outside the locating sleeve, and a camera fixing board is arranged between the upper damping rubber and the lower damping rubber. As the base damper utilizes damping measurements, and stability and reliability of operation of the camera are greatly improved.
Description
Technical field
The utility model belongs to employed a kind of base vibration damper on the aerial mapping equipment, specifically is on the photographic camera that is applied on the aerial mapping equipment.
Background technique
Photographic camera on the present aerial mapping equipment and the means of fixation of the base on the mapping equipment do not have vibration damper, like this owing to the high-frequency vibrations of airplane engine, have influence on the photograph effect of photographic camera, and photograph is smudgy.
Summary of the invention
The purpose of this utility model just is to overcome above-mentioned shortcoming, and a kind of base vibration damper that provides.
The utility model is achieved in that a kind of base vibration damper, it is characterized in that: at aircraft fixed plate base fixing bolt is installed, at fixing bolt setting sleeve, plain cushion and wing nut are installed, shock absorbing rubber and following shock absorbing rubber are installed in the outside of setting sleeve, between last shock absorbing rubber and following shock absorbing rubber, the photographic camera fixed plate are installed.
Description of drawings
The utility model is described in more detail below in conjunction with accompanying drawing.
Accompanying drawing is main sectional view of the present utility model.
Each label declaration is as follows among the figure:
1, fixing bolt, 2, wing nut, 3, plain cushion, 4, setting sleeve, 5, go up shock absorbing rubber, 6, shock absorbing rubber down, 7, the photographic camera fixed plate, 8, aircraft fixed plate base.
Embodiment
The utility model fixing bolt 1 adopts the M10 stainless steel bolt, its effect is stationary positioned cover 4, wing nut 2 adopts M10 stainless steel wing nut, it is 11 millimeters that plain cushion 3 adopts internal diameter, thickness is 2 millimeters stainless steel plain cushion, it is 11 millimeters that setting sleeve 4 adopts internal diameter, wall thickness is 2 millimeters Stainless Steel Tube processing and fabricating, the effect of setting sleeve 4 is fixing shock absorbing rubber 5 and following shock absorbing rubbers 6 gone up, last shock absorbing rubber 5 and following shock absorbing rubber 6, all adopt the top-quality rubber manufacturing, its effect is exactly damping, and photographic camera fixed plate 7 employing thickness are 3 millimeters corrosion resistant plate processing and fabricating, and the effect of photographic camera fixed plate 7 is exactly the reliable and stable work of fixed camera, aircraft fixed plate base 8 employing thickness are 4 millimeters corrosion resistant plate processing and fabricating, and it is reliable and stable that its effect is exactly fixed camera fixed plate 7.
In sum, the utility model is owing to having adopted glissando, so improved stability and the reliability of cameras work greatly.
Claims (1)
1. base vibration damper, it is characterized in that: at aircraft fixed plate base fixing bolt is installed, at fixing bolt setting sleeve, plain cushion and wing nut are installed, shock absorbing rubber and following shock absorbing rubber are installed in the outside of setting sleeve, between last shock absorbing rubber and following shock absorbing rubber, the photographic camera fixed plate are installed.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN 201220743058 CN203114997U (en) | 2012-12-31 | 2012-12-31 | Base damper |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN 201220743058 CN203114997U (en) | 2012-12-31 | 2012-12-31 | Base damper |
Publications (1)
Publication Number | Publication Date |
---|---|
CN203114997U true CN203114997U (en) | 2013-08-07 |
Family
ID=48895347
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN 201220743058 Expired - Fee Related CN203114997U (en) | 2012-12-31 | 2012-12-31 | Base damper |
Country Status (1)
Country | Link |
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CN (1) | CN203114997U (en) |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103758907A (en) * | 2014-01-10 | 2014-04-30 | 江苏艾锐泰克无人飞行器科技有限公司 | Damping device for unmanned aerial vehicles |
CN104214270A (en) * | 2014-06-27 | 2014-12-17 | 中航飞机股份有限公司西安飞机分公司 | Shock absorption structure of pull rod suspension device |
CN104379959A (en) * | 2014-03-31 | 2015-02-25 | 深圳市大疆创新科技有限公司 | Damping device and aircraft employing same |
CN107630960A (en) * | 2017-09-29 | 2018-01-26 | 北京动力机械研究所 | A kind of electronic product damper assembly structure using Anti-fall measure |
CN111071930A (en) * | 2019-12-20 | 2020-04-28 | 湖南中联重科建筑起重机械有限责任公司 | Camera device, lifting hook assembly and tower crane |
CN111958633A (en) * | 2020-08-17 | 2020-11-20 | 宁波肯倍机器人科技有限公司 | 10 kg all-purpose robot |
-
2012
- 2012-12-31 CN CN 201220743058 patent/CN203114997U/en not_active Expired - Fee Related
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103758907A (en) * | 2014-01-10 | 2014-04-30 | 江苏艾锐泰克无人飞行器科技有限公司 | Damping device for unmanned aerial vehicles |
CN103758907B (en) * | 2014-01-10 | 2015-09-16 | 江苏艾锐泰克无人飞行器科技有限公司 | The damping device of unmanned vehicle |
CN104379959A (en) * | 2014-03-31 | 2015-02-25 | 深圳市大疆创新科技有限公司 | Damping device and aircraft employing same |
CN104379959B (en) * | 2014-03-31 | 2016-09-28 | 深圳市大疆创新科技有限公司 | Damping device and the aircraft of the described damping device of application |
CN104214270A (en) * | 2014-06-27 | 2014-12-17 | 中航飞机股份有限公司西安飞机分公司 | Shock absorption structure of pull rod suspension device |
CN107630960A (en) * | 2017-09-29 | 2018-01-26 | 北京动力机械研究所 | A kind of electronic product damper assembly structure using Anti-fall measure |
CN111071930A (en) * | 2019-12-20 | 2020-04-28 | 湖南中联重科建筑起重机械有限责任公司 | Camera device, lifting hook assembly and tower crane |
CN111958633A (en) * | 2020-08-17 | 2020-11-20 | 宁波肯倍机器人科技有限公司 | 10 kg all-purpose robot |
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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: 20130807 Termination date: 20151231 |
|
EXPY | Termination of patent right or utility model |