CN206797754U - A kind of damping device of unmanned machine equipment installation - Google Patents
A kind of damping device of unmanned machine equipment installation Download PDFInfo
- Publication number
- CN206797754U CN206797754U CN201720642402.0U CN201720642402U CN206797754U CN 206797754 U CN206797754 U CN 206797754U CN 201720642402 U CN201720642402 U CN 201720642402U CN 206797754 U CN206797754 U CN 206797754U
- Authority
- CN
- China
- Prior art keywords
- lower shoe
- upper plate
- fixing band
- machine equipment
- equipment installation
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- 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
It the utility model is related to unmanned plane equipment technical field, more particularly to a kind of damping device of unmanned machine equipment installation, including main case, wing and damping base, the wing is symmetricly set on the main case side, the damping base includes upper plate and lower shoe, is fixedly connected between the upper plate and the lower shoe by spring part；The shape and structure of the upper plate upper surface and the shape and structure of the main case lower surface match, and the bottom surface of the upper plate is plane；The lower shoe upper surface is symmetrical arranged fixing band, and the fixing band free end is connected by velcro；The fixing band is fixed on the outside of the edge on perspective plane of the upper plate on the lower shoe along the lower shoe length direction spaced set, the fixing band lower end；The lower shoe bottom surface sets yielding rubber pad.The utility model good damping effect, and can adapt to a variety of unmanned plane models and use, it is versatile.
Description
Technical field
It the utility model is related to unmanned plane equipment technical field, and in particular to a kind of damping dress of unmanned machine equipment installation
Put.
Background technology
Installation form is mostly rigid installation under currently used unmanned vehicle engine, i.e., snubber block is rigid,
The damping effect of rigid snubber block is poor during vibrations, and more vibrations are transferred to each position of fuselage, and this will influence to fly
The service life of machine various pieces part and the stability of flight；Flight control system is precision electronic element simultaneously, and more vibrations require
Height, shaking conference causes the damage of flight control system.
Utility model content
The technical problem of solution
For the disadvantages mentioned above present in prior art, the utility model provides a kind of damping of unmanned machine equipment installation
Device, can be efficiently against damping effect difference present in prior art the problem of, while solve being applicable for damping device
Sex chromosome mosaicism.
Technical scheme
To realize object above, the utility model is achieved by the following technical programs：
A kind of damping device of unmanned machine equipment installation, including main case, wing and damping base, the wing are symmetrically set
Put in the main case side, the damping base includes upper plate and lower shoe, between the upper plate and the lower shoe
It is fixedly connected by spring part；The shape and structure of the upper plate upper surface and the shape and structure phase of the main case lower surface
Match somebody with somebody, the bottom surface of the upper plate is plane；The lower shoe upper surface is symmetrical arranged fixing band, and the fixing band free end passes through
Velcro connects；The fixing band is fixed on institute along the lower shoe length direction spaced set, the fixing band lower end
On the outside of the edge for stating perspective plane of the upper plate on the lower shoe；The lower shoe bottom surface sets yielding rubber pad.
Further, the bottom plate suqare is more than the upper plate area.
Further, the upper end of the spring part is fixed on the bottom surface of the upper plate, and the lower end of the spring part is consolidated
It is scheduled on the upper surface of the lower shoe.
Further, the central axis of the spring part is in the upper plate bottom surface and the lower shoe upper table
Face.
Further, the spring part is uniformly arranged between the upper plate and the lower shoe.
Further, perspective plane of the upper plate on the lower shoe is centrally located at the lower shoe upper surface
At center.
Beneficial effect
Using technical scheme provided by the utility model, compared with known publicly-owned technology, have the advantages that：
1st, good damping effect, electronic component and battery in unmanned plane can effectively be protected.
2nd, it is easy for installation, firmly install, and damping level is adjustable.
3rd, it is easy to dismount, it is wide available for the unmanned plane of Multiple Type, use range.
Brief description of the drawings
, below will be to embodiment in order to illustrate more clearly of the utility model embodiment or technical scheme of the prior art
Or the required accompanying drawing used is briefly described in description of the prior art.It should be evident that drawings in the following description are only
It is some embodiments of the utility model, for those of ordinary skill in the art, is not paying the premise of creative work
Under, other accompanying drawings can also be obtained according to these accompanying drawings.
Fig. 1 is main structure diagram of the present utility model；
Fig. 2 is overlooking the structure diagram of the present utility model；
Label in figure represents respectively：Main case 1；Wing 2；Yielding rubber pad 3；Upper plate 4；Lower shoe 5；Spring part 6；
Fixing band 7；Velcro 8.
Embodiment
It is new below in conjunction with this practicality to make the purpose, technical scheme and advantage of the utility model embodiment clearer
Accompanying drawing in type embodiment, the technical scheme in the embodiment of the utility model is clearly and completely described.Obviously, retouched
The embodiment stated is the utility model part of the embodiment, rather than whole embodiments.Based on the implementation in the utility model
Example, the every other embodiment that those of ordinary skill in the art are obtained under the premise of creative work is not made, is belonged to
The scope of the utility model protection.
With reference to embodiment, the utility model will be further described.
Embodiment
A kind of damping device of unmanned machine equipment installation of the present embodiment, including main case 1, wing 2 and damping base, machine
The wing 2 is symmetricly set on the side of main case 1, and damping base includes upper plate 4 and lower shoe 5, leads between upper plate 4 and lower shoe 5
Spring part 6 is crossed to be fixedly connected；The shape and structure of the upper surface of upper plate 4 and the shape and structure of the lower surface of main case 1 match, upper bottom
The bottom surface of plate 4 is plane；The upper surface of lower shoe 5 is symmetrical arranged fixing band 7, and the free end of fixing band 7 is connected by velcro 8；
Fixing band 7 is fixed on projection of the upper plate 4 on lower shoe 5 along the length direction spaced set of lower shoe 5, the lower end of fixing band 7
On the outside of the edge in face；The bottom surface of lower shoe 5 sets yielding rubber pad 3；The area of lower shoe 5 is more than the area of upper plate 4；Spring part 6
Upper end is fixed on the bottom surface of upper plate 4, and the lower end of spring part 6 is fixed on the upper surface of lower shoe 5；The center line of spring part 6 hangs down
Directly in the bottom surface of upper plate 4 and the upper surface of lower shoe 5；Spring part 6 is uniformly arranged between upper plate 4 and lower shoe 5；Upper plate 4
Perspective plane on lower shoe 5 is centrally located at the upper surface center of lower shoe 5.
Operation principle：In use, the upper surface of upper plate 4 is bonded into the bottom surface of main case 1, fixing band 7 is wrapped in master upwards
Fixed by velcro 8 on casing 1, when fixed, can be adjusted according to the compression degree of the adjustment of weight spring part 6 of unmanned plane
Save its damping level born；When unmanned plane is fallen, lower shoe 5 first lands, and yielding rubber pad 3 plays preliminary cushioning effect, after
And the compression of spring part 6 buffers the purpose that impulsive force of contacting to earth reaches damping, good damping effect.
Movable be fixed on the unmanned plane of Multiple Type of the present embodiment uses, and use range is extensive, and flexibility is strong.
Above example is only to illustrate the technical solution of the utility model, rather than its limitations；Although with reference to foregoing reality
Example is applied the utility model is described in detail, it will be understood by those within the art that：It still can be to preceding
State the technical scheme described in each embodiment to modify, or equivalent substitution is carried out to which part technical characteristic；And these
Modification or replace, can't make appropriate technical solution essence depart from various embodiments of the utility model technical scheme spirit and
Scope.
Claims (6)
1. a kind of damping device of unmanned machine equipment installation, including main case (1), wing (2) and damping base, the wing
(2) it is symmetricly set on the main case (1) side, it is characterised in that：The damping base includes upper plate (4) and lower shoe
(5), it is fixedly connected between the upper plate (4) and the lower shoe (5) by spring part (6)；Upper plate (4) upper surface
Shape and structure and the shape and structure of the main case (1) lower surface match, the bottom surface of the upper plate (4) is plane；Institute
State lower shoe (5) upper surface and be symmetrical arranged fixing band (7), fixing band (7) free end is connected by velcro (8)；Institute
State fixing band (7) and be fixed on the upper bottom along the lower shoe (5) length direction spaced set, fixing band (7) lower end
On the outside of the edge on perspective plane of the plate (4) on the lower shoe (5)；Lower shoe (5) bottom surface sets yielding rubber pad (3).
2. the damping device of unmanned machine equipment installation according to claim 1, lower shoe (5) area are more than on described
Bottom plate (4) area.
3. the damping device of unmanned machine equipment installation according to claim 1, the upper end of the spring part (6) is fixed on institute
The bottom surface of upper plate (4) is stated, the lower end of the spring part (6) is fixed on the upper surface of the lower shoe (5).
4. the damping device of unmanned machine equipment installation according to claim 1, the central axis of the spring part (6) in
Upper plate (4) bottom surface and the lower shoe (5) upper surface.
5. the damping device of unmanned machine equipment installation according to claim 1, the spring part (6) is uniformly arranged on described
Between upper plate (4) and the lower shoe (5).
6. the damping device of unmanned machine equipment installation according to claim 1, the upper plate (4) is in the lower shoe
(5) perspective plane on is centrally located at the lower shoe (5) upper surface center.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720642402.0U CN206797754U (en) | 2017-06-05 | 2017-06-05 | A kind of damping device of unmanned machine equipment installation |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720642402.0U CN206797754U (en) | 2017-06-05 | 2017-06-05 | A kind of damping device of unmanned machine equipment installation |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206797754U true CN206797754U (en) | 2017-12-26 |
Family
ID=60744912
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720642402.0U Expired - Fee Related CN206797754U (en) | 2017-06-05 | 2017-06-05 | A kind of damping device of unmanned machine equipment installation |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206797754U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108382602A (en) * | 2018-01-30 | 2018-08-10 | 孙吉毅 | A kind of novel unmanned plane anti-collision protection device |
-
2017
- 2017-06-05 CN CN201720642402.0U patent/CN206797754U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108382602A (en) * | 2018-01-30 | 2018-08-10 | 孙吉毅 | A kind of novel unmanned plane anti-collision protection device |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20171226 |