CN208149596U - A kind of unmanned plane shock bracket - Google Patents
A kind of unmanned plane shock bracket Download PDFInfo
- Publication number
- CN208149596U CN208149596U CN201820670967.4U CN201820670967U CN208149596U CN 208149596 U CN208149596 U CN 208149596U CN 201820670967 U CN201820670967 U CN 201820670967U CN 208149596 U CN208149596 U CN 208149596U
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- CN
- China
- Prior art keywords
- unmanned plane
- spring
- fixed
- sleeve
- support column
- Prior art date
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- Expired - Fee Related
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- Vibration Prevention Devices (AREA)
Abstract
The utility model discloses a kind of unmanned plane shock brackets, including support column and support plate, connecting rod is fixedly installed below the support column, the lateral wall of the connecting rod is provided with the first spring, one end of first spring is fixedly connected with the support column, the other end of first spring is fixedly connected with fixing seat, and reinforcing bar is provided on the support column, and the reinforcing bar and the support column are detachably connected；Lower gasket, Upper gasket and second spring are internally provided in attachment base; lower gasket and Upper gasket fix second spring; when unmanned plane rises and falls; by second spring the vibration amplitude of unmanned plane itself is reduced; a possibility that improving the loose-parts inside original unmanned plane, is provided with support plate and sponge sleeve on support rod, and the shaking force of generation is transferred in support plate; the amplitude of bracket vibration is reduced by sponge sleeve, dual shock absorption is to unmanned plane duplicate protection.
Description
Technical field
The utility model belongs to air vehicle technique field, and in particular to a kind of unmanned plane shock bracket.
Background technique
Unmanned plane is to utilize the not manned aircraft of radio robot and the presetting apparatus provided for oneself manipulation, Huo Zheyou
Car-mounted computer fully or intermittently automatically operates, and mapping unmanned plane is essential when staff surveys and draws operation sets
It is standby, because easy to operate easy-to-use, receive the extensive favorable comment of staff.
When unmanned plane rises and falls, in addition the weight of itself, original unmanned machine support is easy to produce vibration, may cause nothing
The loose-parts of man-machine inside even result in unmanned plane damage, bring economic loss to user of service.
Utility model content
The purpose of this utility model is to provide a kind of unmanned plane shock brackets, to solve to propose in above-mentioned background technique
When unmanned plane rises and falls, in addition the weight of itself, original unmanned machine support is easy to produce vibration, may cause in unmanned plane
The problem of loose-parts in portion even result in unmanned plane damage, bring economic loss to user of service.
To achieve the above object, the utility model provides the following technical solutions：A kind of unmanned plane shock bracket, including branch
Dagger and support plate are fixedly installed connecting rod below the support column, and the lateral wall of the connecting rod is provided with the first bullet
One end of spring, first spring is fixedly connected with the support column, and the other end of first spring is fixedly connected with fixation
, it is provided with reinforcing bar on the support column, the reinforcing bar and the support column are detachably connected, the top of the support column
It is fixedly installed attachment base, support rod is provided in the fixing seat, the support rod is fixedly connected with the connecting rod, described
The inside of attachment base offers the first cavity, and the attachment base is internally provided with lower gasket, and the lower gasket and attachment base are solid
Fixed connection, the lower gasket upper surface are fixedly installed sleeve, and the other end of the sleeve is provided with Upper gasket, the Upper gasket
It is fixedly connected with the sleeve, the support plate is removably connected on the support rod, the support plate bottom is provided with solid
Fixed pole, the fixed link are fixedly connected with the support plate, and the fixed link lateral wall is arranged with sponge sleeve, the sponges cover
Cylinder is fixedly connected with the fixed link, and the inner sidewall of the sponge sleeve is provided with thickening layer, the thickening layer and the sponge
Sleeve is adhesively fixed.
Preferably, fixed block is fixedly installed in the reinforcing bar, the reinforcing bar passes through the fixed block and the branch
Dagger is fixedly connected.
Preferably, the inside of the sleeve offers the second cavity, and the sleeve inner is provided with second spring, and described
One end of two springs is fixedly connected with the sleeve, and the other end of the second spring is fixedly connected with the Upper gasket.
Preferably, the inner sidewall of the thickening layer is provided with silica gel sheath, and the silica gel sheath and the thickening layer are adhesively fixed.
Preferably, connection ring is fixedly installed in the support plate, the support plate passes through the connection ring and the branch
Strut is detachably connected.
Preferably, the lateral wall of the sponge sleeve is fixedly installed fixed ring, and the quantity of the fixed ring is two,
Two fixed rings are symmetric the lateral wall in the sponge sleeve.
Compared with prior art, the utility model has the beneficial effects that：Lower gasket, Upper gasket are internally provided in attachment base
And second spring, lower gasket and Upper gasket fix second spring, when unmanned plane rises and falls, make unmanned plane by second spring
A possibility that vibration amplitude of itself reduces, and improves the loose-parts inside original unmanned plane, is provided with branch on support rod
Fagging and sponge sleeve, the shaking force of generation is transferred in support plate, and the amplitude of bracket vibration is reduced by sponge sleeve,
Dual shock absorption reduces the economic loss of user of service to unmanned plane duplicate protection.
Detailed description of the invention
Fig. 1 is the structural schematic diagram of the utility model；
Fig. 2 is the sponge tube-in-tube structure schematic diagram in the utility model；
Fig. 3 is the second spring structural schematic diagram in the utility model；
In figure：10, support column；11, connecting rod；12, the first spring；13, fixing seat；14, reinforcing bar；141, fixed block；
15, attachment base；16, support rod；17, lower gasket；18, sleeve；181, Upper gasket；19, second spring；20, support plate；21, even
Connect ring；22, fixed link；23, sponge sleeve；231, fixed ring；24, thickening layer；25, silica gel sheath.
Specific embodiment
The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model
Clearly and completely describe, it is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole
Embodiment.Based on the embodiments of the present invention, those of ordinary skill in the art are without making creative work
Every other embodiment obtained, fall within the protection scope of the utility model.
Fig. 1-3 is please referred to, the utility model provides a kind of technical solution：A kind of unmanned plane shock bracket, including support
Column 10 and support plate 20, the lower section of support column 10 are fixedly installed connecting rod 11, and the lateral wall of connecting rod 11 is provided with the first bullet
One end of spring 12, the first spring 12 is fixedly connected with support column 10, and the other end of the first spring 12 is fixedly connected with fixing seat 13,
Reinforcing bar 14 is provided on support column 10, reinforcing bar 14 and support column 10 are detachably connected, the top fixed setting of support column 10
There is attachment base 15, support rod 16 is provided in fixing seat 13, support rod 16 is fixedly connected with connecting rod 11, the inside of attachment base 15
The first cavity is offered, attachment base 15 is internally provided with lower gasket 17, and lower gasket 17 is fixedly connected with attachment base 15, lower gasket
17 upper surfaces are fixedly installed sleeve 18, and the other end of sleeve 18 is provided with Upper gasket 181, and Upper gasket 181 and sleeve 18 are fixed
It connects, support plate 20 is removably connected on support rod 16,20 bottom of support plate is provided with fixed link 22, fixed link 22 and support
Plate 20 is fixedly connected, and 22 lateral wall of fixed link is arranged with sponge sleeve 23, and sponge sleeve 23 is fixedly connected with fixed link 22, sponge
The inner sidewall of sleeve 23 is provided with thickening layer 24, and thickening layer 24 and sponge sleeve 23 are adhesively fixed.
In the present embodiment, lower gasket 17, Upper gasket 181 and second spring 19, underlay are internally provided in attachment base 15
Piece 17 and Upper gasket 181 are fixed second spring 19, when unmanned plane rises and falls, make unmanned plane itself by second spring 19
A possibility that vibration amplitude reduces, and improves the loose-parts inside original unmanned plane, is provided with support plate on support rod 16
20 and sponge sleeve 23, the shaking force of generation is transferred in support plate 20, bracket vibration is reduced by sponge sleeve 23
Amplitude, dual shock absorption reduce the economic loss of user of service to unmanned plane duplicate protection, and the lateral wall of thickening layer 24 is provided with silicon
Gum cover 25, silica gel sheath 25 make sponge sleeve 23 more firm in fixed link 22, increase rubbing for sponge sleeve 23 and fixed link 22
Wipe power.
Further, fixed block 141 is fixedly installed in reinforcing bar 14, reinforcing bar 14 passes through fixed block 141 and support column
10 are fixedly connected.
In the present embodiment, it is easy to use personnel by reinforcing bar 14 by fixed block 141, is fixed on support column 10, to branch
Erect reinforcement effect.
Further, the inside of sleeve 18 offers the second cavity, and sleeve 18 is internally provided with second spring 19, the second bullet
One end of spring 19 is fixedly connected with sleeve 18, and the other end of second spring 19 is fixedly connected with Upper gasket 181.
In the present embodiment, when unmanned plane rises and falls, by second spring 19 vibration amplitude of unmanned plane itself is reduced,
Improve the possibility of the loose-parts inside original unmanned plane.
Further, the lateral wall of thickening layer 24 is provided with silica gel sheath 25, and silica gel sheath 25 and thickening layer 24 are adhesively fixed.
In the present embodiment, silica gel sheath 25 makes sponge sleeve 23 more firm in fixed link 22, increases by 23 He of sponge sleeve
The frictional force of fixed link 22.
Further, connection ring 21 is fixedly installed in support plate 20, support plate 20 passes through connection ring 21 and support rod 16
It is detachably connected.
In the present embodiment, support plate 20 is sticked into and is fixed to 16 lateral wall of support rod by connection ring 21 by user of service,
It is easily installed.
Further, the inner sidewall of sponge sleeve 23 is fixedly installed fixed ring 231, and the quantity of fixed ring 231 is two
A, two fixed rings 231 are symmetric the lateral wall in sponge sleeve 23.
In the present embodiment, fixed ring 231 again increases the frictional force of sponge sleeve 23 Yu ground, so that bracket steadily connects
Tread surface.
The working principle and process for using of the utility model：After the utility model installs, when unmanned plane rises and falls, under
Gasket 17 and Upper gasket 181 are fixed by second spring 19, by second spring 19 vibration amplitude of unmanned plane itself are reduced,
The shaking force of generation is transferred in support plate 20, passes through sea by a possibility that improving the loose-parts inside original unmanned plane
Continuous sleeve 23 reduces the amplitude of bracket vibration, and dual shock absorption reduces the economic loss of user of service to unmanned plane duplicate protection,
Silica gel sheath 25 makes sponge sleeve 23 more firm in fixed link 22, increases the frictional force of sponge sleeve 23 and fixed link 22, makes
With personnel by connection ring 21, support plate 20 is sticked into and is fixed to 16 lateral wall of support rod, is easily installed, fixed ring 231 is again
The secondary frictional force for increasing sponge sleeve 23 Yu ground, so that bracket steadily contacts ground.
While there has been shown and described that the embodiments of the present invention, for the ordinary skill in the art,
It is understood that these embodiments can be carried out with a variety of variations in the case where not departing from the principles of the present invention and spirit, repaired
Change, replacement and variant, the scope of the utility model is defined by the appended claims and the equivalents thereof.
Claims (6)
1. a kind of unmanned plane shock bracket, it is characterised in that：Including support column (10) and support plate (20), the support column
(10) it is fixedly installed below connecting rod (11), the lateral wall of the connecting rod (11) is provided with the first spring (12), described
One end of first spring (12) is fixedly connected with the support column (10), and the other end of first spring (12) is fixedly connected with
Fixing seat (13) is provided with reinforcing bar (14) on the support column (10), and the reinforcing bar (14) and the support column (10) can
Dismantling connection is fixedly installed attachment base (15) at the top of the support column (10), is provided with support on the fixing seat (13)
Bar (16), the support rod (16) are fixedly connected with the connecting rod (11), and the inside of the attachment base (15) offers first
Cavity, the attachment base (15) are internally provided with lower gasket (17), and the lower gasket (17) is fixedly connected with attachment base (15),
Lower gasket (17) upper surface is fixedly installed sleeve (18), and the other end of the sleeve (18) is provided with Upper gasket (181),
The Upper gasket (181) is fixedly connected with the sleeve (18), is removably connected with the support plate on the support rod (16)
(20), support plate (20) bottom is provided with fixed link (22), the fixed link (22) and the fixed company of the support plate (20)
It connects, fixed link (22) lateral wall is arranged with sponge sleeve (23), and the sponge sleeve (23) and the fixed link (22) are solid
Fixed connection, the inner sidewall of the sponge sleeve (23) are provided with thickening layer (24), the thickening layer (24) and the sponge sleeve
(23) it is adhesively fixed.
2. a kind of unmanned plane shock bracket according to claim 1, it is characterised in that：It is fixed on the reinforcing bar (14)
It is provided with fixed block (141), the reinforcing bar (14) is fixedly connected by the fixed block (141) with the support column (10).
3. a kind of unmanned plane shock bracket according to claim 1, it is characterised in that：It opens the inside of the sleeve (18)
Equipped with the second cavity, the sleeve (18) is internally provided with second spring (19), one end of the second spring (19) and described
Sleeve (18) is fixedly connected, and the other end of the second spring (19) is fixedly connected with the Upper gasket (181).
4. a kind of unmanned plane shock bracket according to claim 1, it is characterised in that：The inside of the thickening layer (24)
Wall is provided with silica gel sheath (25), and the silica gel sheath (25) and the thickening layer (24) are adhesively fixed.
5. a kind of unmanned plane shock bracket according to claim 1, it is characterised in that：It is fixed on the support plate (20)
It is provided with connection ring (21), the support plate (20) is detachably connected by the connection ring (21) and the support rod (16).
6. a kind of unmanned plane shock bracket according to claim 1, it is characterised in that：Outside the sponge sleeve (23)
Side wall is fixedly installed fixed ring (231), and the quantity of the fixed ring (231) is two, and two fixed rings (231) are in
It is symmetrically distributed in the lateral wall of the sponge sleeve (23).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820670967.4U CN208149596U (en) | 2018-05-07 | 2018-05-07 | A kind of unmanned plane shock bracket |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820670967.4U CN208149596U (en) | 2018-05-07 | 2018-05-07 | A kind of unmanned plane shock bracket |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208149596U true CN208149596U (en) | 2018-11-27 |
Family
ID=64389430
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820670967.4U Expired - Fee Related CN208149596U (en) | 2018-05-07 | 2018-05-07 | A kind of unmanned plane shock bracket |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208149596U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110155360A (en) * | 2019-05-19 | 2019-08-23 | 郭屹 | One kind is based on aircraft aerial survey positioning bracket |
-
2018
- 2018-05-07 CN CN201820670967.4U patent/CN208149596U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110155360A (en) * | 2019-05-19 | 2019-08-23 | 郭屹 | One kind is based on aircraft aerial survey positioning bracket |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| 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: 20181127 Termination date: 20190507 |