CN206409571U - Speed regulator vibration damping sheet and unmanned plane - Google Patents
Speed regulator vibration damping sheet and unmanned plane Download PDFInfo
- Publication number
- CN206409571U CN206409571U CN201621432249.0U CN201621432249U CN206409571U CN 206409571 U CN206409571 U CN 206409571U CN 201621432249 U CN201621432249 U CN 201621432249U CN 206409571 U CN206409571 U CN 206409571U
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- speed regulator
- connection sheet
- sheet portion
- vibration damping
- unmanned plane
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Abstract
The utility model discloses a kind of speed regulator vibration damping sheet and unmanned plane, its upper connection sheet portion and lower connection sheet portion for including the S-type shrapnel part in cross section and being arranged on the shrapnel part two ends；The upper connection sheet portion and the lower connection sheet portion are each provided with mounting hole.Above-mentioned speed regulator vibration damping sheet employs special shape design, and it has considered space utilization, during installation, and design relative with the junction of speed governing main body, general structure is more reliable.Speed regulator vibration damping sheet and unmanned plane that the utility model is provided, also with its simple in construction, simple installation, cost is lower, security and stability is higher, all many technical advantages such as weight is lighter.
Description
Technical field
The utility model is related to unmanned plane equipment technical field, more particularly to a kind of speed regulator vibration damping sheet and unmanned plane.
Background technology
In recent years, with the rise and the fast development of related model plane and unmanned plane art of unmanned plane, nobody
Machine is also applied in increasing occasion；In the process, increasing masses also start to contact unmanned plane, from this nothing
It is man-machine to have entered into common people's entertainment field from specialty, scientific research field.
Referred to as " unmanned plane ", english abbreviation is " UAV " to UAV, using radio robot and providing for oneself
The not manned aircraft that presetting apparatus is manipulated.Unmanned plane press application field, can be divided into it is military with it is civilian.It is many it is civilian nobody
In machine, it is exactly take photo by plane four axles, the unmanned planes such as six axles of taking photo by plane to occur more.
It is well known that it is above-mentioned take photo by plane civilian unmanned machine its it is main by unmanned plane body (for example：Frame and propeller), it is dynamic
Power apparatus is (for example：Motor, electron speed regulator, battery), control device (for example：Single-chip microcomputer, three axle Together, digital gyroscopes) etc.
Several big main device parts are constituted.Wherein, speed regulator is the important component of controlled motor, once speed regulator breaks down, entirely
Power set and UAS can all have the risk of paralysis.
However, it has been investigated that its governor arrangement part of existing many unmanned planes still lacks in the presence of some technologies at present
Fall into；Damping processing is not done between speed regulator and unmanned plane body, speed regulator is so easily caused in unmanned plane running
Moderately gusty air and trigger failure；In addition, indivedual unmanned plane products also devise some shock absorber devices to reach damping effect,
But this shock absorber device structure is extremely complex, the cost increase of unmanned plane is caused, while also becoming the weight of unmanned plane
Weight, have impact on the flight efficiency of unmanned plane, and heavier physical burden is brought to flight.
Utility model content
The purpose of this utility model is to provide a kind of speed regulator vibration damping sheet and unmanned plane, to solve the above problems.
In order to achieve the above object, the technical solution of the utility model is realized in：
The utility model provides a kind of speed regulator vibration damping sheet, including the S-type shrapnel part in cross section and is arranged on institute
State the upper connection sheet portion and lower connection sheet portion at shrapnel part two ends；The upper connection sheet portion and the lower connection sheet portion are each provided with peace
Fill hole.
It is preferred that, can embodiment as one kind；The bearing of trend in the upper connection sheet portion and the lower connection sheet portion
Bearing of trend is mutually perpendicular to.
It is preferred that, can embodiment as one kind；The upper connection sheet portion be arranged on the top of the shrapnel part and along
Vertical direction is extended；The lower connection sheet portion is arranged on the bottom of the shrapnel part and is extended along horizontal direction.
It is preferred that, can embodiment as one kind；Multiple mounting holes are provided with the upper connection sheet portion, and it is described
Multiple mounting hole sequence interval arrangements in upper connection sheet portion.
It is preferred that, can embodiment as one kind；A mounting hole is provided with the lower connection sheet portion.
It is preferred that, can embodiment as one kind；The shrapnel part and the upper connection sheet portion, the lower connection sheet portion are equal
For stainless steel substrates.
Correspondingly, the utility model additionally provides a kind of unmanned plane, including unmanned plane body and speed regulator main body, Yi Jisi
Individual above-mentioned speed regulator vibration damping sheet；Four speed regulator vibration damping sheets are arranged between speed regulator main body and unmanned plane body；
The upper connection sheet portion of each speed regulator vibration damping sheet is connected with the speed regulator main body, and the speed regulator damping
The lower connection sheet portion of piece is connected with the base of the unmanned plane body.
It is preferred that, can embodiment as one kind；Four speed regulator vibration damping sheets are specifically located at speed regulator master respectively
Four edges of body bottom.
It is preferred that, can embodiment as one kind；The unmanned plane also includes elastomeric pad, and the elastomeric pad is set
Put the bottom in upper connection sheet portion and lower connection sheet portion.
It is preferred that, can embodiment as one kind；The elastomeric pad is specially rubber sheet gasket or engineering plastics pad.
Compared with prior art, the advantage of the utility model embodiment is：
A kind of speed regulator vibration damping sheet and unmanned plane that the utility model is provided, wherein above-mentioned speed regulator vibration damping sheet is with as follows
Structure type：Above-mentioned speed regulator vibration damping sheet its be an independent design of part；The speed regulator vibration damping sheet, it is mainly by transversal
Three element portions of the S-type shrapnel part in face and upper connection sheet portion and lower connection sheet portion are constituted.
Wherein, shrapnel part has special shape design, i.e. its cross section of the shrapnel part is S-type, so its shell fragment
Portion can implement elastic deformation in a certain direction, and then play elastic buffer effect；Connection sheet portion and lower connection on this simultaneously
Piece portion is then separately positioned on the shrapnel part two ends；The upper connection sheet portion and the lower connection sheet portion are each provided with mounting hole.
The upper connection sheet portion of speed regulator vibration damping sheet is connected by mounting hole with speed regulator main body, and at the same time the speed regulator subtracts
The lower connection sheet portion of shake piece is connected by mounting hole with the base of unmanned plane body, and then may be such that speed regulator vibration damping sheet firmly
It is fixed between speed regulator main body and unmanned plane body, while playing both effects of connection, even more serves elastic buffer work
With above-mentioned speed regulator vibration damping sheet is conducive to the stability and reliability of unmanned plane governor structure.
To sum up, the utility model is provided speed regulator vibration damping sheet and unmanned plane, its simple in construction, simple installation, cost is low,
Security and stability is high, lightweight.The speed regulator vibration damping sheet that the utility model is provided employs special shape design, and it considers
Space utilization, during installation, design relative with the junction of speed governing main body, general structure is more reliable.
Brief description of the drawings
, below will be right in order to illustrate more clearly of the utility model embodiment or technical scheme of the prior art
The accompanying drawing used required in embodiment or description of the prior art is briefly described, it should be apparent that, describe below
In accompanying drawing be some embodiments of the present utility model, for those of ordinary skill in the art, do not paying creativeness
On the premise of work, other accompanying drawings can also be obtained according to these accompanying drawings.
A kind of structural representation for the speed regulator vibration damping sheet that Fig. 1 provides for the utility model embodiment；
Another structural representation for the speed regulator vibration damping sheet that Fig. 2 provides for the utility model embodiment；
The yet another construction schematic diagram for the speed regulator vibration damping sheet that Fig. 3 provides for the utility model embodiment；
Knot is assembled between speed regulator vibration damping sheet and speed regulator main body Facad structure that Fig. 4 provides for the utility model embodiment
Structure schematic diagram；
Knot is assembled between speed regulator vibration damping sheet and speed regulator main body backside structure that Fig. 5 provides for the utility model embodiment
Structure schematic diagram；
Description of reference numerals：
Speed regulator main body A；
Speed regulator vibration damping sheet 1；
Shrapnel part 11；
Upper connection sheet portion 12；
Lower connection sheet portion 13；
Mounting hole 14.
Embodiment
The technical solution of the utility model is clearly and completely described below in conjunction with accompanying drawing, it is clear that described
Embodiment is a part of embodiment of the utility model, rather than whole embodiments.Based on the embodiment in the utility model, sheet
The every other embodiment that field those of ordinary skill is obtained under the premise of creative work is not made, belongs to this practicality
Novel protected scope.
, it is necessary to explanation in description of the present utility model, term " " center ", " on ", " under ", it is "left", "right", " perpendicular
Directly ", the orientation or position relationship of the instruction such as " level ", " interior ", " outer " are, based on orientation shown in the drawings or position relationship, to be only
Described for the ease of description the utility model and simplifying, rather than to indicate or imply that signified device or element must have specific
Orientation, with specific azimuth configuration and operation, therefore it is not intended that to limitation of the present utility model.In addition, term " the
One ", " second ", " the 3rd " are only used for describing purpose, and it is not intended that indicating or implying relative importance.
, it is necessary to which explanation, unless otherwise clearly defined and limited, term " are pacified in description of the present utility model
Dress ", " connected ", " connection " should be interpreted broadly, for example, it may be fixedly connected or be detachably connected, or integratedly
Connection；Can be mechanical connection or electrical connection；Can be joined directly together, can also be indirectly connected to by intermediary,
It can be the connection of two element internals.For the ordinary skill in the art, above-mentioned art can be understood with concrete condition
Concrete meaning of the language in the utility model.
The utility model is described in further detail below by specific embodiment and with reference to accompanying drawing.
A kind of speed regulator vibration damping sheet 1 provided referring to Fig. 1, Fig. 2, Fig. 3, the utility model embodiment, including cross section are in S
The shrapnel part 11 of type and the upper connection sheet portion 12 and lower connection sheet portion 13 for being arranged on the two ends of shrapnel part 11；The upper connection
Mounting hole 14 is each provided with piece portion 12 and the lower connection sheet portion 13.
In embodiment of the present utility model, because speed regulator main body is made up of soft copy in scheme, soft copy due to
The factors such as welding, it is impossible to bear to shake, collide equivalent risk, and because the system is used for aircraft, there is harshness to want again weight
Ask.So we on the basis of original speed regulator using increasing, assembling is simple in four shell fragments, structure and meets weight demands, again
System can be made stable, failure risk is reduced.
The main construction for analyzing above-mentioned speed regulator vibration damping sheet is understood：Above-mentioned speed regulator vibration damping sheet its be an independent part
Structure；The speed regulator vibration damping sheet, it is mainly by the S-type shrapnel part 11 in cross section and upper connection sheet portion 12 and lower connection sheet portion
13 3 critical piece parts are constituted.
Wherein, there is above-mentioned shrapnel part 11 special shape to design, i.e., this its cross section of shrapnel part 11 is S-type (can shape
Elephant is interpreted as serpentine shaped), so its shrapnel part 11 can implement elastic deformation in a certain direction, and then play bullet
Property cushioning effect；Connection sheet portion 12 and lower connection sheet portion 13 are then separately positioned on the two ends of shrapnel part 11 on this simultaneously；It is described
Upper connection sheet portion 12 and the lower connection sheet portion 13 are each provided with mounting hole 14.
The upper connection sheet portion 12 of speed regulator vibration damping sheet is connected by mounting hole 14 with speed regulator main body A, at the same time the tune
The lower connection sheet portion 13 of fast device vibration damping sheet is connected by mounting hole with the base of unmanned plane body (not shown), and then may be such that tune
Fast device vibration damping sheet is firmly fixed between speed regulator main body A and unmanned plane body, while playing both effects of connection, is even more
Elastic buffer effect is served, above-mentioned speed regulator vibration damping sheet is conducive to the stability and reliability of unmanned plane governor structure.
To sum up, the utility model is provided speed regulator vibration damping sheet and unmanned plane, its simple in construction, simple installation, cost is low,
Security and stability is high, lightweight.The speed regulator vibration damping sheet that the utility model is provided employs special shape design, and it considers
Space utilization, during installation, design relative with the junction of speed governing main body, general structure is more reliable.
The speed regulator vibration damping sheet and the concrete structure and specific skill of unmanned plane provided below the utility model embodiment
Art effect, which is done, to be described in detail：
It is preferred that, can embodiment as one kind；The bearing of trend in the upper connection sheet portion and the lower connection sheet portion
Bearing of trend is mutually perpendicular to.
It is preferred that, can embodiment as one kind；The upper connection sheet portion 12 be arranged on the top of the shrapnel part 11 and
It is extended along vertical direction；The lower connection sheet portion 13 is arranged on the bottom of the shrapnel part 11 and prolonged along horizontal direction
Setting is stretched, i.e., upper connection sheet portion 12 is set with lower connection sheet portion 13 in right-angled intersection direction.
It is preferred that, can embodiment as one kind；Multiple mounting holes 14 are provided with the upper connection sheet portion 12, and
Multiple mounting hole sequence interval arrangements in the upper connection sheet portion.
It is preferred that, can embodiment as one kind；A mounting hole 14 is provided with the lower connection sheet portion 13.
It should be noted that upper connection sheet portion 12 is arranged on the top of shrapnel part 11 and is extended along vertical direction,
Multiple mounting holes thereon are to arrange to lay along the vertically extending direction in upper connection sheet portion 12 simultaneously；Lower connection sheet portion 13 is set
It is extended in the bottom of shrapnel part 11 and along horizontal direction；As shown in Figure 4 and Figure 5, so, upper connection sheet portion can lead to
Cross multiple mounting holes multiple positions of speed regulator main body are fixed, and then realize the firm work to speed regulator agent structure
With；Meanwhile, lower connection sheet portion 13 is laterally to be laid on unmanned plane body, can be to nobody by four lower connection sheet portions 13
Four positions of machine body are fastened and fixed, and can so be completed to unmanned plane body and speed regulator by said structure form
Main body carries out elastic shock attenuation connection and fixed operation.
It is preferred that, can embodiment as one kind；The shrapnel part 11 and the upper connection sheet portion 12, the lower connection sheet
Portion 13 is stainless steel substrates or other metal structure pieces.
It should be noted that the shrapnel part 11 and the upper connection sheet portion 12, the lower connection sheet portion 13 can be selected
Using multiple structural forms, but it is preferably selected and welded using integrally formed stainless steel substrates or other metal structure pieces
Shaping also may be used.The speed regulator vibration damping sheet of said structure, its architecture quality is lighter, while its structural stability and reliability are more
It is superior.
Correspondingly, referring to Fig. 4 and Fig. 5, the utility model additionally provides a kind of unmanned plane, including unmanned plane body (does not show
Go out) and speed regulator main body A, and four above-mentioned speed regulator vibration damping sheets 1；Four speed regulator vibration damping sheets 1 are arranged at tune
Between fast device main body and unmanned plane body A；
The upper connection sheet portion of each speed regulator vibration damping sheet 1 is connected with the speed regulator main body, and the speed regulator subtracts
The lower connection sheet portion of shake piece 1 is connected with the base of the unmanned plane body.
It is preferred that, can embodiment as one kind；Four speed regulator vibration damping sheets 1 are specifically located at speed regulator master respectively
Four edges of body A bottoms.
It is preferred that, can embodiment as one kind；The unmanned plane also includes elastomeric pad (not shown), and the bullet
Property pad is arranged on the bottom in connection sheet portion and lower connection sheet portion.
It should be noted that above-mentioned elastomeric pad is just provided in the upper connection sheet and the speed regulator of speed regulator vibration damping sheet
Between main body, and between the lower connection sheet of the speed regulator vibration damping sheet and the base of the unmanned plane body, above-mentioned cushion
Piece is advantageously in the stability and reliability of structure.
It is preferred that, can embodiment as one kind；The elastomeric pad is specially rubber sheet gasket or engineering plastics pad.
It should be noted that above-mentioned elastomeric pad can select the pad using diversified forms, but it is in order at weight and tries one's best
Lightweight, anti-wear performance is tried one's best the technical requirements such as superior, and it preferably uses rubber sheet gasket or engineering plastics pad；Above-mentioned engineering plastic
Backing strap piece has higher structural strength, anti-wear performance and tear resistance.Meanwhile, its structural stability and structural reliability
It is stronger, can be lifted between speed regulator vibration damping sheet and unmanned plane fastening effect (because in general, hardware and hardware configuration it
Between direct rigid connection, its steadiness is poor；If adding using above-mentioned elastomeric pad, it can lift connection between the two
Steadiness).
The speed regulator vibration damping sheet and unmanned plane that the utility model embodiment is provided have the technical advantage of following aspect：
First, the speed regulator vibration damping sheet that the utility model embodiment is provided, its speed regulator vibration damping sheet employs special shape and set
Meter (i.e. main body is snakelike shrapnel part structure), it has considered space utilization, during installation, relative with the junction of speed governing main body
Design, general structure is more reliable.
2nd, the unmanned plane that the utility model embodiment is provided, its by four speed regulator vibration damping sheets and unmanned plane body with
Speed regulator main body is connected, and on the one hand it serves the effect of being fastenedly connected；On the other hand it, which is also acted, realizes cushioning effect.This reality
The unmanned plane provided with new embodiment, it considers from security and operational reliability angle, devises said structure form.
3rd, the speed regulator vibration damping sheet and unmanned plane that the utility model embodiment is provided, simple in construction, simple installation, cost
Low, security and stability is high, lightweight.Increase i.e. on original speed regulator subjective basis in four speed regulator vibration damping sheets, structure and fill
With simple and meet weight demands, it can make system stable again, reduce failure risk.
Many significant technical advantages based on more than, the speed regulator vibration damping sheet and unmanned plane that the utility model is provided will bands
Carry out good market prospects and economic benefit.
Finally it should be noted that：Various embodiments above is only limited to illustrate the technical solution of the utility model, rather than to it
System；Although the utility model is described in detail with reference to foregoing embodiments, one of ordinary skill in the art should
Understand：It can still modify to the technical scheme described in foregoing embodiments, or to which part or whole
Technical characteristic carries out equivalent substitution；And these modifications or replacement, the essence of appropriate technical solution is departed from this practicality newly
The scope of each embodiment technical scheme of type.
Claims (10)
1. a kind of speed regulator vibration damping sheet, it is characterised in that including the S-type shrapnel part in cross section and be arranged on the shrapnel part
The upper connection sheet portion and lower connection sheet portion at two ends；The upper connection sheet portion and the lower connection sheet portion are each provided with mounting hole.
2. speed regulator vibration damping sheet as claimed in claim 1, it is characterised in that
The bearing of trend in the upper connection sheet portion and the bearing of trend in the lower connection sheet portion are mutually perpendicular to.
3. speed regulator vibration damping sheet as claimed in claim 2, it is characterised in that
The upper connection sheet portion is arranged on the top of the shrapnel part and is extended along vertical direction；The lower connection sheet portion
It is arranged on the bottom of the shrapnel part and is extended along horizontal direction.
4. speed regulator vibration damping sheet as claimed in claim 1, it is characterised in that
The multiple mounting holes being provided with the upper connection sheet portion on multiple mounting holes, and the upper connection sheet portion are suitable
Sequence is spaced.
5. speed regulator vibration damping sheet as claimed in claim 1, it is characterised in that
A mounting hole is provided with the lower connection sheet portion.
6. speed regulator vibration damping sheet as claimed in claim 1, it is characterised in that
The shrapnel part and the upper connection sheet portion, the lower connection sheet portion are stainless steel substrates.
7. a kind of unmanned plane, it is characterised in that including unmanned plane body and speed regulator main body, and four such as claim 1-6
Speed regulator vibration damping sheet described in any one；Four speed regulator vibration damping sheets be arranged at speed regulator main body and unmanned plane body it
Between；
The upper connection sheet portion of each speed regulator vibration damping sheet is connected with the speed regulator main body, and the speed regulator vibration damping sheet
Lower connection sheet portion is connected with the base of the unmanned plane body.
8. unmanned plane as claimed in claim 7, it is characterised in that
Four speed regulator vibration damping sheets are specifically located at four edges of speed regulator bottom part body respectively.
9. unmanned plane as claimed in claim 8, it is characterised in that
The unmanned plane also includes elastomeric pad, and the elastomeric pad is arranged on connection sheet portion and lower connection sheet portion
Bottom.
10. unmanned plane as claimed in claim 9, it is characterised in that
The elastomeric pad is specially rubber sheet gasket or engineering plastics pad.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621432249.0U CN206409571U (en) | 2016-12-23 | 2016-12-23 | Speed regulator vibration damping sheet and unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621432249.0U CN206409571U (en) | 2016-12-23 | 2016-12-23 | Speed regulator vibration damping sheet and unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206409571U true CN206409571U (en) | 2017-08-15 |
Family
ID=59552065
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621432249.0U Active CN206409571U (en) | 2016-12-23 | 2016-12-23 | Speed regulator vibration damping sheet and unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206409571U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109673118A (en) * | 2018-12-29 | 2019-04-23 | 深圳航星光网空间技术有限公司 | A kind of damping |
-
2016
- 2016-12-23 CN CN201621432249.0U patent/CN206409571U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109673118A (en) * | 2018-12-29 | 2019-04-23 | 深圳航星光网空间技术有限公司 | A kind of damping |
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