CN105626758B - A kind of MR vibration damper for helicopter high-definition camera installation and debugging - Google Patents
A kind of MR vibration damper for helicopter high-definition camera installation and debugging Download PDFInfo
- Publication number
- CN105626758B CN105626758B CN201610164680.XA CN201610164680A CN105626758B CN 105626758 B CN105626758 B CN 105626758B CN 201610164680 A CN201610164680 A CN 201610164680A CN 105626758 B CN105626758 B CN 105626758B
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- CN
- China
- Prior art keywords
- vibration damper
- receiving portion
- pedestal
- connecting portion
- cell body
- 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.)
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Links
- 238000009434 installation Methods 0.000 title claims abstract description 8
- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 claims abstract description 22
- 239000007788 liquid Substances 0.000 claims abstract description 15
- 210000005056 cell body Anatomy 0.000 claims description 19
- 239000000463 material Substances 0.000 claims description 8
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 5
- 229910052782 aluminium Inorganic materials 0.000 claims description 5
- 239000004411 aluminium Substances 0.000 claims description 4
- 238000004073 vulcanization Methods 0.000 claims description 4
- 238000013016 damping Methods 0.000 description 12
- 239000006096 absorbing agent Substances 0.000 description 2
- 238000010276 construction Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 229910000831 Steel Inorganic materials 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000005266 casting Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000005672 electromagnetic field Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000012530 fluid Substances 0.000 description 1
- 238000011900 installation process Methods 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
- 230000006641 stabilisation Effects 0.000 description 1
- 238000011105 stabilization Methods 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F9/00—Springs, vibration-dampers, shock-absorbers, or similarly-constructed movement-dampers using a fluid or the equivalent as damping medium
- F16F9/32—Details
- F16F9/53—Means for adjusting damping characteristics by varying fluid viscosity, e.g. electromagnetically
- F16F9/535—Magnetorheological [MR] fluid dampers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
- B64D47/08—Arrangements of cameras
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Electromagnetism (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Vibration Prevention Devices (AREA)
Abstract
The present invention discloses a kind of MR vibration damper for helicopter high-definition camera installation and debugging, and MR vibration damper includes：Pedestal, coil and magnetic flow liquid；Pedestal includes the first connecting portion being connected with camera and the second connecting portion affixed with helicopter；First connecting portion includes the first receiving portion for accommodating coil and the second receiving portion for accommodating magnetic flow liquid, and the first receiving portion is looped around the periphery of the second receiving portion.The MR vibration damper of the present invention is compact-sized, and reliability is high, and weight is small.
Description
Technical field
The present invention relates to fluid damper technical field.It is used to helicopter high-definition camera more particularly, to one kind pacify
The MR vibration damper of adjustment examination.
Background technology
Aviation machine construction environment is severe, and job status is complicated, and the requirement to pass heavy parts is very high.High-definition camera subtracts
Device is shaken as one of important Parts in aviation machine, it is desirable to which it is conveniently applicable, structure is light, reliability is high.High-definition camera uses
During, helicopter vibration is big, has very big interference to the shooting effect of camera, and the image of camera shooting is smudgy,
Therefore the mounting shock absorber between camera and helicopter is needed, reduces influence of the helicopter vibration to camera.Market at present
On damper typically have air bump, rubber absorbers and steel rope damper etc..Its elasticity after these dampers dispatch from the factory
Determined that with damping, it is impossible to change is adjusted again, and height is can guarantee that, it is necessary to install in the installation process of high-definition camera
Clear camera photographs the damper with suitable elasticity and damping of clear picture effect, and in order to install suitable high-definition camera
Damper needed for head work, then it is it needs to be determined that required during high-definition camera shooting clear picture under helicopter flight state
The elasticity and damping parameter of damper, then according to the parameter of determination, suitable damper is installed, therefore in order to reduce test work
That makees is convenient and swift, it is necessary to design the damper of low-cost and high-performance convenient use.
The content of the invention
It is an object of the invention to provide a kind of MR vibration damper for helicopter high-definition camera installation and debugging, side
Just the elasticity between camera and helicopter and damping are adjusted.
To reach above-mentioned purpose, the present invention uses following technical proposals：
A kind of MR vibration damper for helicopter high-definition camera installation and debugging, the MR vibration damper include：
Pedestal, coil and magnetic flow liquid；
The pedestal includes the first connecting portion being connected with camera and the second connecting portion affixed with helicopter；Described
One connecting portion includes accommodating the first receiving portion of coil and accommodates the second receiving portion of magnetic flow liquid, and first receiving portion is surround
In the periphery of second receiving portion.
Further, the MR vibration damper also includes cell body；The first connecting portion includes a groove, the groove
Side wall be provided with the first receiving portion for accommodating coil, the inside grooves accommodate cell body, and the side wall of the cell body is provided with
Accommodate the second receiving portion of magnetic flow liquid.
Further, first receiving portion is the first annular groove, and second receiving portion is the second annular groove.
Further, the MR vibration damper also includes motion bar, and the inside of cell body is stretched into one end of the motion bar
And it is connected with bottom land.
Further, the motion bar is provided with screwed hole, and the material of the motion bar is aluminium.
Further, the second connecting portion of the pedestal is threaded rod, and the material of the pedestal is aluminium.
Further, the material of the cell body is vulcanization rubber.
Beneficial effects of the present invention are as follows：
(1) structural reliability is high, and vulcanization rubber is provided between pedestal and motion bar, and coil is arranged in base seat groove, structure
It is compact.Pedestal and motion bar are all that aluminum casting forms, therefore construction weight is small.
(2) elasticity and damping are adjustable, and coil and magnetic flow liquid are provided with damper, pass through and change inflow coil current
Size can change elasticity and the damping of damper.
Brief description of the drawings
The embodiment of the present invention is described in further detail below in conjunction with the accompanying drawings.
Fig. 1 is the overall appearance schematic diagram of MR vibration damper of the present invention；
Fig. 2 is MR vibration damper structural representation of the present invention.
In figure：1- pedestals；2- coils；3- cell bodies；4- motion bars；5- base thread bars；6- magnetic flow liquids；7- screwed holes.
Embodiment
In order to illustrate more clearly of the present invention, the present invention is done further with reference to preferred embodiments and drawings
It is bright.
As illustrated in fig. 1 and 2, MR vibration damper includes pedestal 1, coil 2, cell body 3, motion bar 4, threaded rod 5, magnetorheological
Liquid 6 and screwed hole 7；Pedestal 1 includes the first connecting portion being connected with camera and the second connecting portion affixed with helicopter；First
Connecting portion includes accommodating the first receiving portion of coil 2 and accommodates the second receiving portion of magnetic flow liquid 6, and the first receiving portion is looped around institute
State the periphery of the second receiving portion；Specifically, first connecting portion includes groove, the side wall of groove, which is provided with, accommodates the first of coil 2
Receiving portion, inside grooves then accommodate cell body 3, and the side wall of cell body 3 is provided with the second receiving portion for accommodating magnetic flow liquid 6；
First receiving portion is the first annular groove, and the second receiving portion is the second annular groove；One end of motion bar 4 is stretched into cell body 3 simultaneously
It is connected with the bottom land of cell body 3, the material of cell body 3 is vulcanization rubber, and motion bar 4 is provided with screwed hole 7, and camera passes through screwed hole
7 are connected with motion bar, and because motion bar 4 is connected with vulcanizing the cell body 3 of quality of rubber materials, thus between motion bar 4 and pedestal 1
Elasticity and damping are provided with, meanwhile, because being additionally provided with the first annular groove of installation coil 2 on pedestal 1, the side wall of cell body 3 is provided with
The second annular groove groove of magnetic flow liquid 6 is accommodated, the first annular groove is looped around the periphery of the second annular groove, when coil 2 is powered, it is possible to
Electromagnetic field is formed, the state of magnetic flow liquid 6 is changed, so as to produce damping, therefore shaking for pedestal is transferred to by helicopter
Dynamic loading can reduce, and so as to play a part of damping to camera, bottom of the pedestal 1 outside groove is provided with threaded rod 5, pedestal
1 is affixed by threaded rod 5 and helicopter.
Installation and debugging of the present invention are simple, and quality is small, are suitable for use in the damping of helicopter high-definition camera.When in use, open
Dynamic helicopter engine, allow the vibration of helicopter to be in normal operating conditions, open the image of high-definition camera observation shooting, to
Different size of electric current, the image of observation camera shooting, until image stabilization is clear are passed through in coil；Record is now in coil
The size of electric current, measure the now elasticity of damper of the present invention and damping using relevant device, you can it is determined that needing to install
Damper performance parameter, reached high-definition camera damping debugging purpose.
Obviously, the above embodiment of the present invention is only intended to clearly illustrate example of the present invention, and is not pair
The restriction of embodiments of the present invention, for those of ordinary skill in the field, may be used also on the basis of the above description
To make other changes in different forms, all embodiments can not be exhaustive here, it is every to belong to this hair
Row of the obvious changes or variations that bright technical scheme is extended out still in protection scope of the present invention.
Claims (6)
1. a kind of MR vibration damper for helicopter high-definition camera installation and debugging, it is characterised in that described magnetorheological to subtract
Shake device includes：Pedestal (1), coil (2) and magnetic flow liquid (6)；
The pedestal (1) includes the first connecting portion being connected with camera and the second connecting portion affixed with helicopter；
The first connecting portion includes the first receiving portion for accommodating coil (2) and the second receiving portion for accommodating magnetic flow liquid (6), institute
State the periphery that the first receiving portion is looped around second receiving portion；The MR vibration damper also includes cell body (3)；Described first
Connecting portion includes a groove, and the side wall of the groove is provided with the first receiving portion for accommodating coil (2), and the inside grooves accommodate
There is cell body (3), the side wall of the cell body (3) is provided with the second receiving portion for accommodating magnetic flow liquid (6).
2. MR vibration damper according to claim 1, it is characterised in that：First receiving portion is the first annular groove, institute
It is the second annular groove to state the second receiving portion.
3. MR vibration damper according to claim 1, it is characterised in that the MR vibration damper also includes motion bar
(4), one end of the motion bar (4) is stretched into the inside of cell body (3) and is connected with bottom land.
4. MR vibration damper according to claim 3, it is characterised in that the motion bar (4) is provided with screwed hole
(7), the material of the motion bar (4) is aluminium.
5. MR vibration damper according to claim 1, it is characterised in that the second connecting portion of the pedestal (1) is spiral shell
Rasp bar (5), the material of the pedestal (1) is aluminium.
6. MR vibration damper according to claim 1, it is characterised in that the material of the cell body (3) is vulcanization rubber.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610164680.XA CN105626758B (en) | 2016-03-22 | 2016-03-22 | A kind of MR vibration damper for helicopter high-definition camera installation and debugging |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610164680.XA CN105626758B (en) | 2016-03-22 | 2016-03-22 | A kind of MR vibration damper for helicopter high-definition camera installation and debugging |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN105626758A CN105626758A (en) | 2016-06-01 |
| CN105626758B true CN105626758B (en) | 2017-12-26 |
Family
ID=56041976
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610164680.XA Active CN105626758B (en) | 2016-03-22 | 2016-03-22 | A kind of MR vibration damper for helicopter high-definition camera installation and debugging |
Country Status (1)
| Country | Link |
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| CN (1) | CN105626758B (en) |
Families Citing this family (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109372922B (en) * | 2018-11-07 | 2020-02-07 | 中国矿业大学 | Magnetic fluid vibration reduction joint for camera support |
| CN114257731A (en) * | 2020-09-24 | 2022-03-29 | 北京小米移动软件有限公司 | Camera module, electronic equipment, camera module control method and device |
| WO2023272601A1 (en) * | 2021-06-30 | 2023-01-05 | 深圳市大疆创新科技有限公司 | Damping structure, movable platform, and load damping method |
| CN114321267B (en) * | 2021-12-29 | 2023-02-03 | 姜堰经济开发区科创中心 | Magnetic fluid damping joint for inspection robot camera support |
Family Cites Families (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE3030375A1 (en) * | 1980-08-11 | 1982-03-25 | Fa. Dieter Schlüter, 6052 Mühlheim | Remote controlled surveillance helicopter - has skid mounted camera cage elastically slung from unmanned fuselage |
| CN201461842U (en) * | 2009-06-10 | 2010-05-12 | 重庆材料仪表研究所 | Magnetorheological fluid elastic shock absorber |
| CN101813153A (en) * | 2010-02-09 | 2010-08-25 | 湖南工程学院 | Active and passive integrated vibration absorber based on electrorheological elastomer |
| CN202418403U (en) * | 2012-02-08 | 2012-09-05 | 谢宁 | Magneto-rheologic elastic body rotary type magneto-rheologic damper |
| CN202674147U (en) * | 2012-07-19 | 2013-01-16 | 吉林大学 | Multi-level extrusion type magnetorheological damper |
| CN103967985B (en) * | 2014-01-16 | 2016-02-10 | 三一重机有限公司 | Adjustable shock, absorber designing system and method |
| CN104895986B (en) * | 2015-01-28 | 2017-03-15 | 安徽微威胶件集团有限公司 | Shear mode magnetic rheology elastic body frequency conversion vibration isolator |
| CN205089884U (en) * | 2015-11-03 | 2016-03-16 | 温州瓯科科技有限公司 | Adjustable attenuator of adjustable rigidity viscoelasticity |
-
2016
- 2016-03-22 CN CN201610164680.XA patent/CN105626758B/en active Active
Also Published As
| Publication number | Publication date |
|---|---|
| CN105626758A (en) | 2016-06-01 |
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| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| CB03 | Change of inventor or designer information |
Inventor after: Guo Qihong Inventor after: Li Chao Inventor after: Wang Lianhui Inventor after: Sun Yang Inventor before: Guo Qihong Inventor before: Lin Kang Inventor before: Yang Yongqiang Inventor before: Zhang Pei Inventor before: Li Chao Inventor before: Zhou Quan Inventor before: Zu Jinge Inventor before: Wang Lianhui Inventor before: Sun Yang |
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| COR | Change of bibliographic data | ||
| GR01 | Patent grant | ||
| CP03 | Change of name, title or address |
Address after: 100191 room 1113, 11th floor, Xueyuan international building, No.1, Zhichun Road, Haidian District, Beijing Patentee after: Iridium gasman Aviation Technology Group Co., Ltd Address before: 100083 Beijing, Zhichun Road, No. 1 College International Building, room 11, room, room 1101 Patentee before: EAGLES MEN AERONAUTIC SCIENCE AND TECHNOLOGY GROUP Co.,Ltd. |
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