CN208559744U - A kind of environmental monitoring unmanned plane undercarriage - Google Patents
A kind of environmental monitoring unmanned plane undercarriage Download PDFInfo
- Publication number
- CN208559744U CN208559744U CN201820529843.4U CN201820529843U CN208559744U CN 208559744 U CN208559744 U CN 208559744U CN 201820529843 U CN201820529843 U CN 201820529843U CN 208559744 U CN208559744 U CN 208559744U
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- China
- Prior art keywords
- support frame
- fixedly connected
- unmanned plane
- fuselage
- slide bar
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Abstract
The utility model discloses a kind of environmental monitoring unmanned plane undercarriages, including fuselage, the fuselage bottom two sides are fixedly connected with the first support frame, the first support frame bottom movable sleeve is connected to the second support frame, second support frame bottom is fixedly connected with the plate that rises and falls, second support frame is internally provided with rubber block, the rubber block bottom is fixedly connected with the plate that rises and falls, first support frame is located at the hollow setting in one end inside the second support frame, the first support frame internal slide is plugged with the first slide bar, first slide bar is located at one end inside the first support frame and is fixedly connected with limited block, first slide bar is located at the first support frame outer surface movable sleeve and is connected to the first spring, first support frame two sides are provided with sliding slot.By being equipped with the first spring and second spring, effectively make to rise and fall is buffered between plate and ground the utility model, increases unmanned plane service life, reduces unmanned plane manufacturing cost.
Description
Technical field
The utility model relates to environmental monitoring air vehicle technique field, in particular to a kind of environmental monitoring unmanned plane is with rising and falling
Frame.
Background technique
Environmental monitoring unmanned plane is provided with undercarriage at present, and the band that rises and falls of unmanned plane is responsible for when unmanned plane lands
Safe condition is landed suddenly in landing by unmanned plane, is easy to cause landing gear to damage, influences unmanned plane service life, mention
High unmanned plane production cost.
Therefore, invent a kind of environmental monitoring unmanned plane solved the above problems with undercarriage it is necessary.
Utility model content
The purpose of this utility model is to provide a kind of environmental monitoring unmanned plane undercarriage, by be equipped with the first spring with
Second spring, effectively making to rise and fall is buffered between plate and ground, increase unmanned plane service life, reduce unmanned plane manufacture at
This, to solve the problems mentioned in the above background technology.
To achieve the above object, the utility model provides the following technical solutions: a kind of environmental monitoring unmanned plane undercarriage,
Including fuselage, the fuselage bottom two sides are fixedly connected with the first support frame, and the first support frame bottom movable sleeve is connected to
Two support frames, second support frame bottom are fixedly connected with the plate that rises and falls, and second support frame is internally provided with rubber block, institute
It states rubber block bottom to be fixedly connected with the plate that rises and falls, first support frame is located at the hollow setting in one end inside the second support frame, institute
It states the first support frame internal slide and is plugged with the first slide bar, first slide bar is located at one end inside the first support frame and is fixedly connected
There is limited block, first slide bar is located at the first support frame outer surface movable sleeve and is connected to the first spring, first support frame
Two sides are provided with sliding slot, and the second slide bar is fixedly connected between the sliding slot both ends, and the second slide bar surface activity is socketed with
Second spring, second slide bar are located at the second support frame interior surface sliding sleeve and are connected to sliding block, and described sliding block one end is fixed to be connected
It connects in the second support frame inner wall.
Preferably, the plate that rises and falls is fixedly connected with fixed block, the fixation between two second support frames
Block two sides are rotatably connected to third support frame, and second support frame one end is provided with universal wheel.
Preferably, fixed block position two sides are fixedly connected with half-round bar, and third support frame is run through in described half-round bar one end
Inner wall is fixedly connected with fixed block.
Preferably, third spring, the third spring inner wall are provided between described half-round bar one end and third support frame
It is slidably socketed on half-round bar surface.
Preferably, first support frame and the top and bottom of fuselage junction are fixedly connected to fixed link, described
Fixed link one end is fixedly connected with the first support frame surface, forms triangle between the fixed link, the first support frame and fuselage
Shape.
Preferably, the fuselage two sides are provided with wing, and institute's fuselage bottom is located between two first support frames
It is even to be provided with camera, 90 degree are differed between camera described in every two.
The technical effect and advantage of the utility model:
1, by being equipped with the first spring, being conducive to, which makes fuselage, generates buffer function between the plate that rises and falls, by being equipped with sliding block,
Be conducive to sliding block in the second slide bar surface sliding compression second spring, make to generate level 2 buffering between fuselage and undercarriage, pass through
First spring and second spring active force, effectively when unmanned plane lands, making to rise and fall between plate and ground is buffered, effectively
Prevent the first support frame and damaged between the plate that rises and falls, it is effective to increase unmanned plane service life, reduce unmanned plane manufacture
Cost；
2, by being equipped with universal wheel, the frictional force between unmanned plane and ground is advantageously reduced, plate damage of rising and falling is prevented, leads to
Cross and be equipped with half-round bar, be conducive to slide third support frame on half-round bar surface, it is effective reduce universal wheel and ground it
Between pressure, thus effectively prevent universal wheel and rise and fall plate damage, by be equipped with multiple cameras, effectively by it is multi-faceted over the ground
Face carries out shooting and monitoring, effective to increase the accuracy monitored also range.
Detailed description of the invention
Fig. 1 is the overall structure diagram of the utility model.
Fig. 2 is the overall structure left view of the utility model.
Fig. 3 is the portion A structural schematic diagram in the utility model Fig. 1.
Fig. 4 is the portion B structural schematic diagram in the utility model Fig. 3.
Fig. 5 is D structural schematic diagram in the utility model Fig. 2.
Fig. 6 is the portion C structural schematic diagram in the utility model and 3.
Fig. 7 is the portion E structural schematic diagram in the utility model Fig. 2.
In figure: 1 fuselage, 2 first support frames, 3 second support frames, 4 are risen and fallen plate, 5 rubber blocks, 6 first slide bars, 7 first bullets
Spring, 8 sliding slots, 9 second slide bars, 10 second springs, 11 limited blocks, 12 sliding blocks, 13 fixed blocks, 14 third support frames, 15 universal wheels,
16 half-round bars, 17 third springs, 18 fixed links, 19 cameras, 20 wings.
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.
The utility model provides a kind of environmental monitoring unmanned plane undercarriage as shown in figs. 1-7, including fuselage 1, institute
It states 1 two sides of the bottom of fuselage and is fixedly connected with the first support frame 2, the 2 bottom movable sleeve of the first support frame is connected to the second support frame
3,3 bottom of the second support frame is fixedly connected with the plate 4 that rises and falls, and second support frame 3 is internally provided with rubber block 5, passes through
Rubber block 5 effectively prevents the first support frame 2 from damaging, and 5 bottom of rubber block is fixedly connected with the plate 4 that rises and falls, and described first
Support frame 2 is located at the 3 hollow setting in inside one end of the second support frame, and 2 internal slide of the first support frame is plugged with the first slide bar
6, first slide bar 6 is located at 2 inside one end of the first support frame and is fixedly connected with limited block 11, prevents the first slide bar 6 and first
Support frame 2 falls off, and first slide bar 6 is located at 2 outer surface movable sleeve of the first support frame and is connected to the first spring 7, passes through first
Spring force 7 makes fuselage 1 and generates buffer function between the plate 4 that rises and falls, and 2 two sides of the first support frame are provided with sliding slot 8, described
The second slide bar 9 is fixedly connected between 8 both ends of sliding slot, 9 surface activity of the second slide bar is socketed with second spring 10, passes through
The second spring power 10 on two slide bars, 9 surface acts on, and makes fuselage 1 and generates level 2 buffering between the plate 4 that rises and falls, passes through the first spring 7
With 10 active force of second spring, effectively when unmanned plane lands, making to rise and fall between plate 4 and ground is buffered, and described second
Slide bar 9 is located at 3 interior surface sliding sleeve of the second support frame and is connected to sliding block 12, and described 12 one end of sliding block is fixedly connected on second
3 inner wall of support.
Further, in the above-mentioned technical solutions, the plate 4 that rises and falls is fixed between two second support frames 3
It is connected with fixed block 13,13 two sides of fixed block are rotatably connected to third support frame 14, and third support frame 14 is lower than the plate that rises and falls
4, described second support frame, 3 one end is provided with universal wheel 15, contacts ground prior to the plate 4 that rises and falls by universal wheel 15, effective logical
Cross the frictional force between the reduction unmanned plane of universal wheel 15 and ground；
Further, in the above-mentioned technical solutions, 13 two sides of the fixed block are fixedly connected with half-round bar 16, described
16 one end of half-round bar is fixedly connected through 14 inner wall of third support frame with fixed block 13；
Further, in the above-mentioned technical solutions, is provided between described 16 one end of half-round bar and third support frame 14
Three springs 17,17 inner wall of third spring are slidably socketed on 16 surface of half-round bar, by 14 stress of third support frame, make third
Support frame 14 is slided on 16 surface of half-round bar, effective to reduce universal wheel 15 and ground by 17 active force of third spring
Between pressure；
Further, in the above-mentioned technical solutions, first support frame 2 and the top and bottom of 1 junction of fuselage are equal
It is fixedly connected with fixed link 18, described 18 one end of fixed link is fixedly connected with 2 surface of the first support frame, the fixed link 18,
Triangle is formed between one support frame 2 and fuselage 1, prevents from damaging deformation between the first support frame 2 and fuselage 1；
Further, in the above-mentioned technical solutions, 1 two sides of fuselage are provided with wing 20, and 1 bottom of institute's fuselage is located at
It is evenly arranged with camera 19 between two first support frames 2, differs 90 degree between camera 19 described in every two.
This practical working principle:
Referring to Figure of description 1-5, by under 1 whereabouts inertia force of fuselage, making the first support frame 2 compress the second support frame 3,
It is shunk inside the first support frame 2 by the first slide bar 6, by the first spring 7, makes fuselage 1 and generated between the plate 4 that rises and falls
Buffer function, by the first support frame 2 in 3 internal contraction of the second support frame, by sliding block 12 on 2 surface of the first support frame
It is slided inside sliding slot 8, is acted on by the second spring power 10 on 9 surface of the second slide bar, make fuselage 1 and produced between the plate 4 that rises and falls
Raw level 2 buffering, by the first spring 7 and 10 active force of second spring, effectively when unmanned plane lands, make to rise and fall plate 4 with
It is buffered between ground, effectively prevents the first support frame 2 and damaged between the plate 4 that rises and falls, effectively increase unmanned plane
Service life reduces unmanned plane manufacturing cost；
Referring to Figure of description 6-7, when landing by unmanned plane, ground is contacted prior to the plate 4 that rises and falls by universal wheel 15,
The effective frictional force reduced between unmanned plane and ground by universal wheel 15 prevents the damage of plate 4 of rising and falling, passes through third support frame
14 stress slide third support frame 14 on 16 surface of half-round bar, by 17 active force of third spring, effectively reduce ten thousand
To pressure between wheel 15 and ground, to effectively prevent universal wheel 15 and the damage of plate 4 of rising and falling, it is arranged by 1 bottom of fuselage multiple
Camera 19 effectively carries out shooting and monitoring to ground by multi-faceted, effective to increase the accuracy monitored also range.Most
It afterwards it is noted that the above descriptions are merely preferred embodiments of the present invention, is not intended to limit the utility model, to the greatest extent
Pipe is with reference to the foregoing embodiments described in detail the utility model, for those skilled in the art, still
It is possible to modify the technical solutions described in the foregoing embodiments, or part of technical characteristic is equally replaced
It changes, within the spirit and principle of the utility model, any modification, equivalent replacement, improvement and so on should be included in this
Within the protection scope of utility model.
Claims (6)
1. a kind of environmental monitoring unmanned plane undercarriage, including fuselage (1), it is characterised in that: fuselage (1) two sides of the bottom are solid
Surely it being connected with the first support frame (2), the first support frame (2) bottom movable sleeve is connected to the second support frame (3), and described second
Support (3) bottom is fixedly connected with the plate that rises and falls (4), and second support frame (3) is internally provided with rubber block (5), the rubber
Block (5) bottom is fixedly connected with the plate that rises and falls (4), and first support frame (2) is located at the second support frame (3), and internal one end is hollow sets
It sets, the first support frame (2) internal slide is plugged with the first slide bar (6), and first slide bar (6) is located at the first support frame
(2) internal one end is fixedly connected with limited block (11), and first slide bar (6) is located at the activity of the first support frame (2) outer surface
It is socketed with the first spring (7), the first support frame (2) two sides are provided with sliding slot (8), fixed between sliding slot (8) both ends
It is connected with the second slide bar (9), the second slide bar (9) surface activity is socketed with second spring (10), the second slide bar (9) position
In the second support frame (3), interior surface sliding sleeve is connected to sliding block (12), and described sliding block (12) one end is fixedly connected on the second support
Frame (3) inner wall.
2. a kind of environmental monitoring unmanned plane undercarriage according to claim 1, it is characterised in that: the plate that rises and falls (4)
It is fixedly connected with fixed block (13) between two second support frames (3), fixed block (13) the two sides rotation connection
Have third support frame (14), described second support frame (3) one end is provided with universal wheel (15).
3. a kind of environmental monitoring unmanned plane undercarriage according to claim 2, it is characterised in that: the fixed block (13)
Position two sides are fixedly connected with half-round bar (16), and third support frame (14) inner wall and fixed block are run through in described half-round bar (16) one end
(13) it is fixedly connected.
4. a kind of environmental monitoring unmanned plane undercarriage according to claim 3, it is characterised in that: the half-round bar (16)
It is provided between one end and third support frame (14) third spring (17), third spring (17) inner wall is slidably socketed in semicircle
Bar (16) surface.
5. a kind of environmental monitoring unmanned plane undercarriage according to claim 1, it is characterised in that: first support frame
(2) it is fixedly connected to fixed link (18) with the top and bottom of fuselage (1) junction, described fixed link (18) one end and first
Support frame (2) surface is fixedly connected, and forms triangle between the fixed link (18), the first support frame (2) and fuselage (1).
6. a kind of environmental monitoring unmanned plane undercarriage according to claim 1, it is characterised in that: the fuselage (1) two
Side is provided with wing (20), and institute's fuselage (1) bottom is evenly arranged with camera between two first support frames (2)
(19), 90 degree are differed between camera described in every two (19).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820529843.4U CN208559744U (en) | 2018-04-16 | 2018-04-16 | A kind of environmental monitoring unmanned plane undercarriage |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820529843.4U CN208559744U (en) | 2018-04-16 | 2018-04-16 | A kind of environmental monitoring unmanned plane undercarriage |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208559744U true CN208559744U (en) | 2019-03-01 |
Family
ID=65480512
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820529843.4U Expired - Fee Related CN208559744U (en) | 2018-04-16 | 2018-04-16 | A kind of environmental monitoring unmanned plane undercarriage |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208559744U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113479322A (en) * | 2021-08-24 | 2021-10-08 | 浙江迪澳普地理信息技术有限公司 | Environment monitoring unmanned aerial vehicle |
| CN113815855A (en) * | 2021-09-29 | 2021-12-21 | 安徽徽光智能科技有限责任公司 | Examine and beat integrative unmanned aerial vehicle |
| CN114408167A (en) * | 2021-12-06 | 2022-04-29 | 南京中智腾飞航空科技研究院有限公司 | Based on infrared heat wave nondestructive test device of unmanned aerial vehicle |
-
2018
- 2018-04-16 CN CN201820529843.4U patent/CN208559744U/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113479322A (en) * | 2021-08-24 | 2021-10-08 | 浙江迪澳普地理信息技术有限公司 | Environment monitoring unmanned aerial vehicle |
| CN113479322B (en) * | 2021-08-24 | 2024-04-09 | 浙江迪澳普地理信息技术有限公司 | Environment monitoring unmanned aerial vehicle |
| CN113815855A (en) * | 2021-09-29 | 2021-12-21 | 安徽徽光智能科技有限责任公司 | Examine and beat integrative unmanned aerial vehicle |
| CN114408167A (en) * | 2021-12-06 | 2022-04-29 | 南京中智腾飞航空科技研究院有限公司 | Based on infrared heat wave nondestructive test device of unmanned aerial vehicle |
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| 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: 20190301 |