CN206889548U - Flying control equipment damping device - Google Patents
Flying control equipment damping device Download PDFInfo
- Publication number
- CN206889548U CN206889548U CN201720603526.8U CN201720603526U CN206889548U CN 206889548 U CN206889548 U CN 206889548U CN 201720603526 U CN201720603526 U CN 201720603526U CN 206889548 U CN206889548 U CN 206889548U
- Authority
- CN
- China
- Prior art keywords
- mounting plate
- apparatus mounting
- upper frame
- control equipment
- shock absorbing
- 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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Abstract
Vibration frequency in flying control equipment flight course can accurately be filtered the utility model discloses a kind of, ensure the flying control equipment damping device of flying control equipment job stability.The flying control equipment damping device, including support, apparatus mounting plate, the cantilever tip are provided with upper frame, and the lower section of the upper frame has installing space, at least three resilient shock absorbing elements are provided between the apparatus mounting plate and upper frame；Described resilient shock absorbing elements one end is connected with upper frame, and the other end is connected with apparatus mounting plate, and the tie point on apparatus mounting plate is not on the same line；The apparatus mounting plate is suspended in below upper frame by resilient shock absorbing elements, and in installing space.Using the flying control equipment damping device, the damping comprehensive to apparatus mounting plate can be realized, plays the accurate filtering to apparatus mounting plate single equipment vibration frequency；It is applied to the accuracy for flying that winged control device work can be ensured on control device and ensures to fly the stability for controlling device work.
Description
Technical field
A kind of shock-absorption device is the utility model is related to, especially a kind of flying control equipment damping device.
Background technology
It is well-known：Existing navigation damping device, one piece of vibration damper plate is set usually below equipment installation pedestal,
Then resilient shock absorbing elements are set between vibration damper plate and basis.Equipment installation pedestal is arranged on vibration damper plate, passes through damping
The damping to equipment is realized in the effect of plate.Because damper element has just now under vibration damper plate, therefore can only realize on above-below direction
Damping, when multiple directions are respectively provided with vibration, good damping effect can not be played.Meanwhile if exist for flying control equipment
Vibrated in the course of work, it will the working condition of serious influence equipment, serious even causes the accident.Therefore it is existing
Damping device can not be used in the damping of flying control equipment.
Utility model content
Technical problem to be solved in the utility model be to provide it is a kind of can be to the vibration in flying control equipment flight course
Frequency is accurately filtered, and ensures the flying control equipment damping device of flying control equipment job stability.
Technical scheme is used by the utility model solves its technical problem：Flying control equipment damping device, including support,
Apparatus mounting plate, the cantilever tip are provided with upper frame, and the lower section of the upper frame has an installing space, the apparatus mounting plate with
At least three resilient shock absorbing elements are provided between upper frame；Described resilient shock absorbing elements one end is connected with upper frame, and the other end is with setting
Standby installing plate connects, and the tie point on apparatus mounting plate is not on the same line；
The apparatus mounting plate is suspended in below upper frame by resilient shock absorbing elements, and in installing space.
Further, the pedestal lower end is provided with mounting base.
Further, the upper frame is arranged to top plate.
Further, the resilient shock absorbing elements both ends are provided with connector, the resilient shock absorbing elements and connector
It is detachably connected；The resilient shock absorbing elements are connected with upper frame and apparatus mounting plate respectively by connector.
Further, the chute extended laterally is provided with the top plate；The connector being connected with apparatus mounting plate is located at
Below apparatus mounting plate, and connecting pole being provided with, described connecting pole one end is fixedly connected with connector, and the other end passes through chute,
And it is provided with locking nut；The locking nut coordinates with being connected axle thread.
Preferably, the resilient shock absorbing elements use silica gel strip.
Preferably, the support includes column, and the column uses expansion link.
The beneficial effects of the utility model are：Flying control equipment damping device described in the utility model, because equipment is installed
Plate is arranged on the lower section of upper frame by resilient shock absorbing elements；Resilient shock absorbing elements have three simultaneously, and vertical centerline does not exist
In same plane, therefore it can be realized to the damping on apparatus mounting plate vertical direction by resilient shock absorbing elements, due to that will set
Standby installing plate is suspended in the lower section of upper frame by resilient shock absorbing elements, therefore can realize in horizontal plane subtracting for all around direction
Shake.Therefore, flying control equipment damping device described in the utility model, the damping comprehensive to apparatus mounting plate can be realized, risen
To the accurate filtering to apparatus mounting plate single equipment vibration frequency；So as to which winged control device be filled installed in the flying control equipment damping
Put the accuracy that can ensure to fly control device work and ensure to fly the stability of control device work.
Brief description of the drawings
Fig. 1 is the stereogram of flying control equipment damping device in the utility model embodiment；
Fig. 2 is the structural representation of flying control equipment damping device in the utility model embodiment；
Fig. 3 is the top view of flying control equipment damping device in the utility model embodiment；
Indicated in figure：1- mounting bases, 2- supports, 21- installing spaces, 3- upper frames, 31- chutes, 4- apparatus mounting plates, 5-
Connector, 51- connecting poles, 6- resilient shock absorbing elements, 7- locking nuts.
Embodiment
The utility model is further illustrated with reference to the accompanying drawings and examples.
As shown in Figure 1 to Figure 3, flying control equipment damping device described in the utility model, including support 2, apparatus mounting plate
4, the top of support 2 is provided with upper frame 3, and the lower section of the upper frame 3 has installing space 21, the apparatus mounting plate 4 and top
At least three resilient shock absorbing elements 6 are provided between frame 3；Described one end of resilient shock absorbing elements 6 is connected with upper frame 3, the other end with
Apparatus mounting plate 4 connects, and the tie point on apparatus mounting plate 4 is not on the same line；
The apparatus mounting plate 4 is suspended in the lower section of upper frame 3 by resilient shock absorbing elements 6, and in installing space 21.
Specifically, at least three resilient shock absorbing elements 6 are provided between the apparatus mounting plate 4 and upper frame 3；The elasticity
The one end of damper element 6 is connected with upper frame 3, and the other end is connected with apparatus mounting plate 4, and the tie point on apparatus mounting plate 4 is not
On the same line；Because three points not on the same line determine a plane, therefore by being set on apparatus mounting plate 4
Three resilient shock absorbing elements 6 not on the same line are put, the damping to the in the vertical direction of apparatus mounting plate 4 can be realized.
Meanwhile the apparatus mounting plate 4 is suspended in the lower section of upper frame 3 by resilient shock absorbing elements 6, due to apparatus mounting plate 4
The lower section of upper frame 3 is arranged on by the way of suspention, therefore small sway can be passed through to the vibration in all directions on horizontal plane
Enter row buffering, then under the collective effect of the cushioning effect of resilient shock absorbing elements 6, realize to shaking in all directions on horizontal plane
Dynamic damping.In application process, support 2 need to be only arranged on to the position specified, flying control equipment is arranged on apparatus mounting plate 4
It is upper.
In summary, flying control equipment damping device described in the utility model, because apparatus mounting plate 4 passes through elastic shock attenuation
Element 6 is arranged on the lower section of upper frame 3；Resilient shock absorbing elements 6 have three simultaneously, and vertical centerline is not in the same plane,
Therefore can be realized to the damping on the vertical direction of apparatus mounting plate 4 by resilient shock absorbing elements 6, due to by apparatus mounting plate 4
The lower section of upper frame is suspended in by resilient shock absorbing elements 6, therefore the damping in direction all around in horizontal plane can be realized.Cause
This, flying control equipment damping device described in the utility model, can realize the damping comprehensive to apparatus mounting plate, play pair setting
The accurate filtering of standby installing plate single equipment vibration frequency；So as to which winged control device is arranged on into energy on the flying control equipment damping device
It is enough to ensure to fly the accuracy of control device work and ensure to fly the stability of control device work.
The support 2 can use various ways, such as integral support 2, welding sectional shelf-unit；For ease of the peace of support 2
Dress, further, the lower end of support 2 is provided with mounting base 1.By setting mounting base 1 installing in the lower end of support 2
Only mounting base 1 need to be installed to relevant position in journey.
For the ease of processing and manufacturing, and ensure the stability of structure, further, the upper frame 3 is arranged to top plate.
For the ease of the installation of resilient shock absorbing elements 6, while it is easy to the dismounting and change of resilient shock absorbing elements 6, further,
The both ends of resilient shock absorbing elements 6 are provided with connector 5, and the resilient shock absorbing elements 6 are detachably connected with connector 5；Institute
Resilient shock absorbing elements 6 are stated to be connected with upper frame 3 and apparatus mounting plate 4 respectively by connector 5.By setting connector 5 by elasticity
Damper element 6 is arranged between apparatus mounting plate 4 and upper frame 3, so that when installing resilient shock absorbing elements 6, only need to be by bullet
Property damper element 6 be attached with connector 5, the models of resilient shock absorbing elements 6 can be any, need to only ensure and connector 5
Realize connection.Therefore without be set according to the model of connection resilient shock absorbing elements 6 on apparatus mounting plate 4 and upper frame 3 pair
The attachment structure answered.
For the ease of position of the adjustment equipment installing plate 4 below upper frame 3, further, horizontal stroke is provided with the top plate
To the chute 31 of extension；The connector 5 being connected with apparatus mounting plate 4 is located at the lower section of apparatus mounting plate 4, and is provided with connecting pole
51, described one end of connecting pole 51 is fixedly connected with connector 5, and the other end passes through chute 31, and is provided with locking nut 7；It is described
Locking nut 7 coordinates with being connected axle thread.
When needing adjustment equipment 4 position of installing plate, will locking nut 7 only need to be set on the connector 5 being connected with top plate
Unscrew, be then slidably connected first 5 to relevant position, then locked by locking nut 7.
The resilient shock absorbing elements 6 can use spring or rubber etc., in order to ensure damping effect, ensure accurate filtering
The vibration frequency of single equipment；Preferably, the resilient shock absorbing elements 6 use silica gel strip.
For the ease of adjusting the height of upper frame 3, further, the support 2 includes column, and the column is using flexible
Bar.
Claims (7)
1. flying control equipment damping device, it is characterised in that：Including support (2), apparatus mounting plate (4), support (2) top is set
Upper frame (3) is equipped with, the lower section of the upper frame (3) has installing space (21), between the apparatus mounting plate (4) and upper frame (3)
It is provided with least three resilient shock absorbing elements (6)；Described resilient shock absorbing elements (6) one end is connected with upper frame (3), and the other end is with setting
Standby installing plate (4) connects, and the tie point on apparatus mounting plate (4) is not on the same line；
The apparatus mounting plate (4) is suspended in below upper frame (3) by resilient shock absorbing elements (6), and is located at installing space (21)
It is interior.
2. flying control equipment damping device as claimed in claim 1, it is characterised in that：Support (2) lower end is provided with installation
Bottom plate (1).
3. flying control equipment damping device as claimed in claim 1, it is characterised in that：The upper frame (3) is arranged to top plate.
4. flying control equipment damping device as claimed in claim 3, it is characterised in that：Resilient shock absorbing elements (6) both ends are equal
Connector (5) is provided with, the resilient shock absorbing elements (6) are detachably connected with connector (5)；The resilient shock absorbing elements (6)
It is connected respectively with upper frame (3) and apparatus mounting plate (4) by connector (5).
5. flying control equipment damping device as claimed in claim 4, it is characterised in that：It is provided with what is extended laterally on the top plate
Chute (31)；The connector (5) being connected with apparatus mounting plate (4) is located at below apparatus mounting plate (4), and is provided with connecting pole
(51), described connecting pole (51) one end is fixedly connected with connector (5), and the other end passes through chute (31), and is provided with locking screw
Female (7)；The locking nut (7) coordinates with being connected axle thread.
6. flying control equipment damping device as claimed in claim 1, it is characterised in that：The resilient shock absorbing elements (6) use silicon
Adhesive tape.
7. flying control equipment damping device as claimed in claim 1, it is characterised in that：The support (2) includes column, described vertical
Post uses expansion link.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720603526.8U CN206889548U (en) | 2017-05-26 | 2017-05-26 | Flying control equipment damping device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720603526.8U CN206889548U (en) | 2017-05-26 | 2017-05-26 | Flying control equipment damping device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206889548U true CN206889548U (en) | 2018-01-16 |
Family
ID=61320435
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720603526.8U Active CN206889548U (en) | 2017-05-26 | 2017-05-26 | Flying control equipment damping device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206889548U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2019227781A1 (en) * | 2018-05-30 | 2019-12-05 | 深圳市大疆创新科技有限公司 | Shock-absorbing mechanism and movable device |
-
2017
- 2017-05-26 CN CN201720603526.8U patent/CN206889548U/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2019227781A1 (en) * | 2018-05-30 | 2019-12-05 | 深圳市大疆创新科技有限公司 | Shock-absorbing mechanism and movable device |
| CN110896647A (en) * | 2018-05-30 | 2020-03-20 | 深圳市大疆创新科技有限公司 | Damping mechanism and movable device |
| CN110896647B (en) * | 2018-05-30 | 2021-04-23 | 深圳市大疆创新科技有限公司 | Damping mechanism and movable device |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20211110 Address after: 430000 No. 100, Weihu Road, Shamao street, Hannan District, Wuhan City, Hubei Province Patentee after: Hubei Jili Taili Flying Car Co.,Ltd. Patentee after: ZHEJIANG GEELY HOLDING GROUP Co.,Ltd. Address before: 610041 No. 1103, floor 11, building 1, No. 1800, middle section of Yizhou Avenue, high tech Zone, Chengdu, Sichuan Patentee before: SICHUAN AOSSCI TECHNOLOGY Co.,Ltd. |
|
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20230613 Address after: 610000 China (Sichuan) pilot Free Trade Zone, Chengdu Patentee after: SICHUAN AOSSCI TECHNOLOGY Co.,Ltd. Address before: 430000 No. 100, Weihu Road, Shamao street, Hannan District, Wuhan City, Hubei Province Patentee before: Hubei Jili Taili Flying Car Co.,Ltd. Patentee before: ZHEJIANG GEELY HOLDING GROUP Co.,Ltd. |