CN107554761A - A kind of support being used in unmanned plane - Google Patents
A kind of support being used in unmanned plane Download PDFInfo
- Publication number
- CN107554761A CN107554761A CN201710952900.XA CN201710952900A CN107554761A CN 107554761 A CN107554761 A CN 107554761A CN 201710952900 A CN201710952900 A CN 201710952900A CN 107554761 A CN107554761 A CN 107554761A
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- support
- hollow
- relative
- side wall
- unmanned plane
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Abstract
The invention discloses a kind of support being used in unmanned plane, including housing, the inside of the housing, which is provided with lower end, has the lifting chamber of the first opening, the relative madial wall of the lifting chamber is arranged with the first limited block and the second limited block, and two relative one end side walls of first limited block are equipped with the second sliding groove, two relative one end side walls of second limited block are equipped with the 3rd sliding groove, the inner top of the lifting chamber is arranged with two the first hollow stems, cavity during the inside of two first hollow stems is equipped with first, the inner bottom part of two middle cavitys has been fixedly connected with the first spring, the both ends side wall of two first hollow stems, which runs through, is provided with the first sliding groove, two first hollow intracavitary slidably connect the first transverse slat.Reasonable in design, simple to operate, only not good damping effect of the invention, and there are a variety of damping modes.
Description
Technical field
The present invention relates to unmanned air vehicle technique field, more particularly to a kind of support being used in unmanned plane.
Background technology
Unmanned plane, it is the not manned aircraft manipulated using radio robot and the presetting apparatus provided for oneself, from skill
The definition of art angle can be divided into：Depopulated helicopter, unmanned fixed-wing aircraft, unmanned multi-rotor aerocraft, unmanned airship and nobody dissipate
Wing machine etc., in general uav bottom all can mounting bracket facilitate unmanned plane landing, but with the use range of unmanned plane
Be continuously increased, user has found, traditional unmanned machine support has damping effect difference and the drawbacks such as damping modes are single, tradition
Unmanned machine support increasingly can not meet the demand in epoch, unmanned machine support needs upgrading badly.
The content of the invention
The invention aims to solve the drawbacks such as damping effect is poor and damping modes are single, and the one kind proposed is used for
Support in unmanned plane, it does not only have good damping effect, and has a variety of damping modes.
To achieve these goals, present invention employs following technical scheme：
A kind of support being used in unmanned plane, including housing, the inside of the housing, which is provided with lower end, has the first opening
Chamber is lifted, the relative madial wall of the lifting chamber is arranged with the first limited block and the second limited block, and two described first
The relative one end side wall of limited block is equipped with the second sliding groove, and two relative one end side walls of second limited block are equipped with
Three sliding grooves, the inner top of the lifting chamber are arranged with two the first hollow stems, and the inside of two first hollow stems is equal
Provided with cavity in first, the inner bottom part of two middle cavitys has been fixedly connected with the first spring, two first hollow stems
Both ends side wall through being provided with the first sliding groove, two first hollow intracavitary slidably connect the first transverse slat, described the
The bottom of one spring is fixedly connected with the upper end of the first transverse slat, and the both ends side wall of first transverse slat extends through relative first
Sliding groove is simultaneously slidably connected with two the second sliding grooves respectively, and two first hollow intracavitary are equipped with first support bar, and two
Bottom of the upper end of the individual first support bar with the first transverse slat is fixedly connected, the bottom difference of two first support bars
Through the first relative hollow stem bottom sidewall and be fixedly connected with buffer stopper, and the both ends side wall of the buffer stopper respectively with
Two the 3rd sliding grooves are slidably connected, and the internal symmetry of the buffer stopper is provided with two connecting cavities, and the upper end of the housing is symmetrical
Provided with two gag lever posts, the bottom of two gag lever posts sequentially passes through housing, the first transverse slat, buffer stopper and extended respectively to
In relative connecting cavity, stopping means is equipped with two connecting cavities, two stopping means are relative with two respectively
Gag lever post connection, the bottom sidewall of the buffer stopper is arranged with two dashpots, is equipped with two dashpots slow
Flushing device, the bottom of two buffer units have been fixedly connected with support block, and the upper end of the housing is arranged with two admittedly
Determine block, the second transverse slat is fixedly connected between two fixed blocks.
Preferably, the stopping means includes the 3rd limited block for being fixed on the bottom of gag lever post, the 3rd limited block
In connecting cavity, the relative madial wall of the connecting cavity is rotatably connected to rotating bar, and two rotating bars are away from connection
One end of chamber inner sidewall is rotatably connected on the side wall of the 3rd limited block, and the 3rd limited block and the one of connecting cavity inner bottom part
End is fixedly connected by second spring.
Preferably, the buffer unit includes being fixed on the second hollow stem of support block upper end, second hollow stem
Cavity during inside is provided with second, the second hollow intracavitary slidably connect second support bar, the upper end of the second support bar
Through the second hollow stem upper end side wall and be fixedly connected with the inner top of dashpot.
Preferably, the inside of the second support bar is provided with telescopic cavity, and the inner bottom part of cavity is provided with vertically in described second
3rd support bar, the upper end of the 3rd support bar is run through the bottom sidewall of the 3rd support bar and extended in telescopic cavity, and institute
State and the 3rd spring is provided between the second hollow stem and dashpot inner top, the second hollow intracavitary bottom and second support bar
The 4th spring is provided between bottom.
Preferably, two relative madial walls of the dashpot are equipped with the 4th sliding groove, two the 4th sliding grooves
Sliding shoe is inside slidably connected, the both ends side wall of second hollow stem, which runs through, is provided with what is be interconnected with cavity in second
5th sliding groove, is equipped with the first connecting plate between the both ends side wall of second hollow stem and relative sliding shoe, and described
The both ends side wall of two support bars is equipped with the second connecting plate, and multiple the are provided between first connecting plate and the second connecting plate
Five springs.
Preferably, the upper end of two gag lever posts is equipped with projection, and multiple six are provided between the projection and housing
Spring.
Preferably, the upper end of second transverse slat is fixedly connected with placement block, and the upper end for placing block is provided with standing groove.
In the present invention, when by impulsive force, support block can play a part of impact, the second hollow stem to the second hollow stem
During rising, the first connecting plate is driven to rise, so that being connected between the first connecting plate and the second connecting plate
5th spring can play good buffering effect, while during the rising of the second hollow stem, the 3rd spring can be hollow to whole second
Bar play alleviate impulsive force effect, injured so as to reduce impulsive force to caused by unmanned plane, whole buffer stopper rising when
Wait, rotating bar and second spring can reduce impulsive force, and when buffer stopper rises, two first support bars are played with the effect of impact
Fruit, in the presence of two first support bars so that the first transverse slat is during rising, because the effect of the first spring, drop
It is low and weaken impulsive force, unmanned plane can be placed and connected in standing groove with convenient use person.The present invention is reasonable in design, behaviour
Make simple, only not good damping effect, and there are a variety of damping modes.
Brief description of the drawings
Fig. 1 is a kind of structural representation of support being used in unmanned plane proposed by the present invention；
Fig. 2 is schematic enlarged-scale view at a kind of A of support in unmanned plane proposed by the present invention；
Fig. 3 is schematic enlarged-scale view at a kind of B of support in unmanned plane proposed by the present invention.
In figure：1 buffer stopper, 2 support blocks, 3 second limited blocks, 4 first limited blocks, 5 housings, 6 fixed blocks, 7 second transverse slats,
8 place blocks, 9 projections, 10 gag lever posts, 11 first hollow stems, 12 first transverse slats, 13 the 3rd limited blocks, 14 rotating bars, 15 second
Strut, 16 second connecting plates, 17 first connecting plates, 18 second hollow stems, 19 the 3rd support bars.
Embodiment
Below in conjunction with the accompanying drawing in the embodiment of the present invention, the technical scheme in the embodiment of the present invention is carried out clear, complete
Site preparation describes, it is clear that described embodiment is only part of the embodiment of the present invention, rather than whole embodiments.
Reference picture 1-3, a kind of support being used in unmanned plane, including housing 5, the inside of housing 5, which is provided with lower end, has the
The lifting chamber of one opening, the relative madial wall of lifting chamber are arranged with the first limited block 4 and the second limited block 3, and two the
The relative one end side wall of one limited block 4 is equipped with the second sliding groove, and two relative one end side walls of the second limited block 3 are equipped with
Three sliding grooves, the inner top for lifting chamber are arranged with two the first hollow stems 11, and the inside of two the first hollow stems 11 is equipped with
Cavity in first, the inner bottom part of two middle cavitys have been fixedly connected with the first spring, the both ends side wall of two the first hollow stems 11
Through being provided with the first sliding groove, two the first hollow intracavitary slidably connect the first transverse slat 12, the bottom of the first spring and the
The upper end of one transverse slat 12 is fixedly connected, and the both ends side wall of the first transverse slat 12 extends through the first relative sliding groove and respectively with two
Individual second sliding groove is slidably connected, and two the first hollow intracavitary are equipped with first support bar, and the upper end of two first support bars is equal
It is fixedly connected with the bottom of the first transverse slat 12, the bottom of two first support bars extends through the bottom of the first relative hollow stem 11
Portion's side wall is simultaneously fixedly connected with buffer stopper 1, and the both ends side wall of buffer stopper 1 is slidably connected with two the 3rd sliding grooves respectively, delays
The internal symmetry for rushing block 1 is provided with two connecting cavities, and the upper end of housing 5 is arranged with two gag lever posts 10, two gag lever posts 10
Bottom sequentially passes through housing 5, the first transverse slat 12, buffer stopper 1 and extended respectively in relative connecting cavity, in two connecting cavities
It is equipped with stopping means, the gag lever post 10 relative with two is connected two stopping means respectively, and the bottom sidewall of buffer stopper 1 is symmetrical
Provided with two dashpots, buffer unit is equipped with two dashpots, the bottom of two buffer units has been fixedly connected with support
Block 2, the upper end of housing 5 are arranged with two fixed blocks 6, the second transverse slat 7 are fixedly connected between two fixed blocks 6, when by
During impulsive force, support block 2 can play a part of impact to the second hollow stem 18, and the second hollow stem 18 is during rising, band
Dynamic first connecting plate 17 rises, so that the 5th spring being connected between the first connecting plate 17 and the second connecting plate 16 can
Good buffering effect is played, while during the rising of the second hollow stem 18, the 3rd spring can play slow to whole second hollow stem 18
The effect of impulsive force is solved, is injured so as to reduce impulsive force to caused by unmanned plane.
In the present invention, stopping means includes the 3rd limited block 13 for being fixed on the bottom of gag lever post 10, the 3rd limited block 13
In connecting cavity, the relative madial wall of connecting cavity is rotatably connected to rotating bar 14, and two rotating bars 14 are away from connecting cavity
One end of side wall is rotatably connected on the side wall of the 3rd limited block 13, and one end of the 3rd limited block 13 and connecting cavity inner bottom part leads to
Cross second spring to be fixedly connected, buffer unit includes being fixed on the second hollow stem 18 of the upper end of support block 2, the second hollow stem 18
Cavity during inside is provided with second, the second hollow intracavitary slidably connect second support bar 15, and the upper end of second support bar 15 is run through
The upper end side wall of second hollow stem 18 is simultaneously fixedly connected with the inner top of dashpot, and the inside of second support bar 15, which is provided with, stretches
Chamber, the inner bottom part of cavity is provided with the 3rd support bar 19 vertically in second, and the 3rd support bar 19 is run through in the upper end of the 3rd support bar 19
Bottom sidewall and extend in telescopic cavity, and the 3rd spring is provided between the second hollow stem 18 and dashpot inner top, second
The 4th spring is provided between hollow intracavitary bottom and the bottom of second support bar 15, two relative madial walls of dashpot are equipped with
4th sliding groove, slidably connects sliding shoe in two the 4th sliding grooves, and the both ends side wall of the second hollow stem 18 is through setting
There is the 5th sliding groove being interconnected with cavity in second, between the both ends side wall of the second hollow stem 18 and relative sliding shoe
Provided with the first connecting plate 17, the both ends side wall of second support bar 15 is equipped with the second connecting plate 16, and the first connecting plate 17 and
Multiple 5th springs are provided between two connecting plates 16, the upper end of two gag lever posts 10 is equipped with projection 9, between projection 9 and housing 5
Provided with multiple 6th springs, by increasing capacitance it is possible to increase the effect of buffering, the upper end of the second transverse slat 7, which is fixedly connected with, places block 8, places block 8
Upper end be provided with standing groove, convenient use person places and connection unmanned plane.
In the present invention, when by impulsive force, support block 2, which is understood, play a part of impact to the second hollow stem 18, in second
Empty bar 18 drives the first connecting plate 17 to rise during rising, connects so that being connected to the first connecting plate 17 and second
The 5th spring between fishplate bar 16 can play good buffering effect, while during the rising of the second hollow stem 18, the 3rd spring energy
The effect for alleviating impulsive force is played to whole second hollow stem 18, is injured so as to reduce impulsive force to caused by unmanned plane, entirely
For buffer stopper 1 when rising, rotating bar 14 and second spring can reduce impulsive force, when buffer stopper 1 rises, to two the
One support bar plays the effect of impact, in the presence of two first support bars so that the first transverse slat 12 during rising,
Because the effect of the first spring, impulsive force is reduced and weakened, unmanned plane can be placed and connect with convenient use person in standing groove.
The foregoing is only a preferred embodiment of the present invention, but protection scope of the present invention be not limited thereto,
Any one skilled in the art the invention discloses technical scope in, technique according to the invention scheme and its
Inventive concept is subject to equivalent substitution or change, should all be included within the scope of the present invention.
Claims (7)
1. a kind of support being used in unmanned plane, including housing (5), it is characterised in that the inside of the housing (5) is provided with lower end
Lifting chamber with the first opening, the relative madial wall of the lifting chamber are arranged with the first limited block (4) and second spacing
Block (3), and two relative one end side walls of first limited block (4) are equipped with the second sliding groove, two described second spacing
The relative one end side wall of block (3) is equipped with the 3rd sliding groove, and the inner top of the lifting chamber is arranged with two the first hollow stems
(11) cavity during, the inside of two first hollow stems (11) is equipped with first, the inner bottom part of two middle cavitys are solid
Surely the first spring is connected with, the both ends side wall of two first hollow stems (11), which runs through, is provided with the first sliding groove, two institutes
State the first hollow intracavitary and slidably connect the first transverse slat (12), the bottom and the upper end of the first transverse slat (12) of first spring are consolidated
Fixed connection, the both ends side wall of first transverse slat (12) extend through the first relative sliding groove and slided respectively with two second
Groove is slidably connected, and two first hollow intracavitary are equipped with first support bar, the upper ends of two first support bars with
The bottom of first transverse slat (12) is fixedly connected, and the bottom of two first support bars extends through the first relative hollow stem
(11) bottom sidewall is simultaneously fixedly connected with buffer stopper (1), and the both ends side wall of the buffer stopper (1) respectively with two the 3rd cunnings
Dynamic groove is slidably connected, and the internal symmetry of the buffer stopper (1) is provided with two connecting cavities, and the upper end of the housing (5) is arranged with
Two gag lever posts (10), the bottom of two gag lever posts (10) sequentially pass through housing (5), the first transverse slat (12), buffer stopper
(1) and extend respectively in relative connecting cavity, stopping means, two stopping means are equipped with two connecting cavities
The gag lever post relative with two (10) is connected respectively, and the bottom sidewall of the buffer stopper (1) is arranged with two dashpots, two
Buffer unit is equipped with the dashpot, the bottom of two buffer units has been fixedly connected with support block (2), the shell
The upper end of body (5) is arranged with two fixed blocks (6), and the second transverse slat (7) is fixedly connected between two fixed blocks (6).
2. a kind of support being used in unmanned plane according to claim 1, it is characterised in that the stopping means includes solid
The 3rd limited block (13) of the bottom of gag lever post (10) is scheduled on, the 3rd limited block (13) is located in connecting cavity, the connection
The relative madial wall of chamber is rotatably connected to rotating bar (14), the one end of two rotating bars (14) away from connection chamber inner sidewall
The side wall of the 3rd limited block (13) is rotatably connected on, and the 3rd limited block (13) and one end of connecting cavity inner bottom part pass through
Second spring is fixedly connected.
3. a kind of support being used in unmanned plane according to claim 1, it is characterised in that the buffer unit includes solid
It is scheduled on second hollow stem (18) of support block (2) upper end, cavity during the inside of second hollow stem (18) is provided with second is described
Second hollow intracavitary slidably connects second support bar (15), and the second hollow stem is run through in the upper end of the second support bar (15)
(18) upper end side wall is simultaneously fixedly connected with the inner top of dashpot.
A kind of 4. support being used in unmanned plane according to claim 3, it is characterised in that the second support bar (15)
Inside be provided with telescopic cavity, the inner bottom part of cavity is provided with the 3rd support bar (19), the 3rd support bar vertically in described second
(19) upper end through the 3rd support bar (19) bottom sidewall and extend in telescopic cavity, and second hollow stem (18) with
The 3rd spring is provided between dashpot inner top, is set between the second hollow intracavitary bottom and the bottom of second support bar (15)
There is the 4th spring.
5. a kind of support being used in unmanned plane according to claim 3, it is characterised in that two dashpots are relative
Madial wall be equipped with the 4th sliding groove, slidably connect sliding shoe in two the 4th sliding grooves, described second is hollow
The both ends side wall of bar (18) runs through the 5th sliding groove for being provided with and being interconnected with cavity in second, second hollow stem (18)
Both ends side wall and relative sliding shoe between be equipped with the first connecting plate (17), the both ends side wall of the second support bar (15)
The second connecting plate (16) is equipped with, and multiple 5th bullets are provided between first connecting plate (17) and the second connecting plate (16)
Spring.
A kind of 6. support being used in unmanned plane according to claim 1, it is characterised in that two gag lever posts (10)
Upper end be equipped with projection (9), multiple 6th springs are provided between the projection (9) and housing (5).
7. a kind of support being used in unmanned plane according to claim 1, it is characterised in that second transverse slat (7)
Upper end, which is fixedly connected with, places block (8), and the upper end for placing block (8) is provided with standing groove.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710952900.XA CN107554761A (en) | 2017-10-13 | 2017-10-13 | A kind of support being used in unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710952900.XA CN107554761A (en) | 2017-10-13 | 2017-10-13 | A kind of support being used in unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107554761A true CN107554761A (en) | 2018-01-09 |
Family
ID=60985632
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710952900.XA Withdrawn CN107554761A (en) | 2017-10-13 | 2017-10-13 | A kind of support being used in unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107554761A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109263995A (en) * | 2018-11-21 | 2019-01-25 | 常宁市耘茂农业产业发展有限责任公司 | A kind of multifunctional agriculture desinsection unmanned plane |
-
2017
- 2017-10-13 CN CN201710952900.XA patent/CN107554761A/en not_active Withdrawn
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109263995A (en) * | 2018-11-21 | 2019-01-25 | 常宁市耘茂农业产业发展有限责任公司 | A kind of multifunctional agriculture desinsection unmanned plane |
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| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20180109 |
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| WW01 | Invention patent application withdrawn after publication |