CN208585403U - A kind of agricultural remote sensing unmanned plane being easy to carry - Google Patents
A kind of agricultural remote sensing unmanned plane being easy to carry Download PDFInfo
- Publication number
- CN208585403U CN208585403U CN201820494984.7U CN201820494984U CN208585403U CN 208585403 U CN208585403 U CN 208585403U CN 201820494984 U CN201820494984 U CN 201820494984U CN 208585403 U CN208585403 U CN 208585403U
- Authority
- CN
- China
- Prior art keywords
- adjusting bracket
- sliding block
- casing
- remote sensing
- unmanned plane
- Prior art date
- 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.)
- Expired - Fee Related
Links
Landscapes
- Catching Or Destruction (AREA)
Abstract
The utility model discloses a kind of agricultural remote sensing unmanned planes for being easy to carry, including casing assembly, flight component and adjust component, the adjusting component includes the first sliding block, the first adjusting rod, the first fixed link and the second sliding block, first sliding block is located at the top of the described first left adjusting bracket inner sidewall, and it is slidably connected with the described first left adjusting bracket, first adjusting rod is located at first sliding block lower surface, and is fixedly connected with first sliding block；Pass through the first sliding block of setting and the second sliding block, facilitate internal first adjusting rod of drive and the second adjusting rod mobile, extend remote sensing unmanned plane support frame length, different height medicine-chest is adapted to fix, use agricultural remote sensing unmanned plane more convenient, by the first fixed link of setting and the second fixed link, conveniently it is spirally connected and fixes the first adjusting rod and the first left adjusting bracket and the second adjusting rod and the second left adjusting bracket, make to control the simpler convenience of agricultural remote sensing unmanned plane support rod collapsing length.
Description
Technical field
The utility model belongs to air vehicle technique field, and in particular to a kind of agricultural remote sensing unmanned plane for being easy to carry.
Background technique
Unmanned plane is the not manned vehicle manipulated by radio robot or airborne computer stored program controlled.
Unmanned plane structure is simple, use cost is low, can not only complete the task of manned aircraft execution, be more suitable for someone's aircraft not
Preferably executing for task, such as the Geological Hazards Investigation of danger zone, air rescue commander and remote sensing of environment, unmanned plane is aerial
The miniature remote sensing technology of remote sensing platform.Traditional remote sensing unmanned plane use scope is extensive, rises extensively in plant protection field of spraying insecticide,
It is widely used in agricultural plant protection, the support rod of traditional remote sensing unmanned plane from band connection carry platform is mostly fixed form, no
The sprinkling medicine-chest for facilitating installation different height specification limits the specification for loading medicine-chest, had not only influenced the use of remote sensing unmanned plane, but also
Remote sensing unmanned plane is influenced in the development and popularization in agricultural spray field, and remote sensing unmanned plane propeller fixed frame is mostly single folding
Formula, folded remote sensing unmanned plane to overall volume change and it is little, influence the storage and carrying of remote sensing unmanned plane.
Utility model content
The purpose of this utility model is to provide a kind of agricultural remote sensing unmanned planes for being easy to carry, to solve above-mentioned background skill
The traditional remote sensing unmanned plane proposed in art from the support rod of band connection carry platform be mostly fixed form, it has not been convenient to different height are installed
The sprinkling medicine-chest of metric lattice limits the specification for loading medicine-chest, has not only influenced the use of remote sensing unmanned plane, but also influence remote sensing unmanned plane
Development and popularization in agricultural spray field, and remote sensing unmanned plane propeller fixed frame be mostly it is single collapsible, it is folded distant
Feel unmanned plane to overall volume change and it is little, influence remote sensing unmanned plane storage with carry the problem of.
To achieve the above object, the utility model provides the following technical solutions: a kind of agricultural remote sensing being easy to carry nobody
Machine, including casing assembly, flight component and adjusting component, the casing assembly includes casing, the first left adjusting bracket, the second left tune
Frame, the first right adjusting bracket, the second right adjusting bracket and carry platform are saved, it is left that the first left adjusting bracket is located at the casing lower surface
Side, and be spirally connected fixation with the casing, the second left adjusting bracket is located at the described first left adjusting bracket lower surface, and described first is right
Adjusting bracket is located on the right side of the casing lower surface, and is fixedly connected with the casing, and the second right adjusting bracket is located at described the
One right adjusting bracket lower surface, the carry platform are located at the described second left adjusting bracket and the first right adjusting bracket lower surface, and with
The second left adjusting bracket is fixedly connected with the described first right adjusting bracket, and the flight component includes mounting base, fixing seat and spiral shell
Paddle is revolved, the mounting base is located in front of the casing left side wall, and is fixedly connected with the casing, and the fixed seating is in described
Mounting base left side wall, and being fixedly connected with the mounting base, the propeller are located on the left of the fixing seat upper surface, and with institute
Fixing seat rotation connection is stated, the adjusting component includes the first sliding block, the first adjusting rod, the first fixed link, the second sliding block, second
Adjusting rod, the second fixed link and limited block, first sliding block are located at the top of the described first left adjusting bracket inner sidewall, and with it is described
First left adjusting bracket is slidably connected, and first adjusting rod is located at first sliding block lower surface, and solid with first sliding block
Fixed connection, first fixed link is located at the described first left adjusting bracket left side wall bottom, and fixes with the described first left adjusting bracket
Connection, second sliding block is located at the described second left adjusting bracket inner sidewall bottom, and is slidably connected with the described second left adjusting bracket,
Second adjusting rod is located at second sliding block upper surface, and is fixedly connected with second sliding block, second fixed link
It at the top of the described second left adjusting bracket left side wall, and is fixedly connected with the described second left adjusting bracket, the limited block is located at institute
It states on the left of carry platform upper surface, and is fixedly connected with the carry platform.
Preferably, first adjusting rod and the first left adjusting bracket and second adjusting rod and the second left tune
Section frame is slidably connected by first sliding block and second sliding block.
Preferably, second adjusting rod and the second left adjusting bracket and first adjusting rod and the first left tune
Section frame is spirally connected fixation by second fixed link and first fixed link.
Preferably, the mounting base and the casing and the fixing seat and the mounting base pass through hinged.
Preferably, the mounting base, the fixing seat and the propeller are flight instruments, the quantity of the flight instruments
Be four, be set in front of the casing left side wall and left side wall rear and casing right side wall front and right side wall rear with
The casing is fixedly connected.
Compared with prior art, the utility model has the beneficial effects that by being set at the top of the first left adjusting bracket inner sidewall
It sets the first sliding block and the second sliding block is set in the second left adjusting bracket inner sidewall bottom, facilitate internal first adjusting rod and second of drive
Adjusting rod is mobile, extends remote sensing unmanned plane support frame length, adapts to different height medicine-chest and fixes, uses agricultural remote sensing unmanned plane
It is more convenient to get up, by the way that the first fixed link is arranged in the first left adjusting bracket left side wall bottom and in the second left adjusting bracket left side wall
The second fixed link is arranged in top, is conveniently spirally connected and fixes the first adjusting rod and the first left adjusting bracket and the second adjusting rod and the second left tune
Frame is saved, makes to control the simpler convenience of agricultural remote sensing unmanned plane support rod collapsing length, by setting on the left of carry platform upper surface
Set limited block, for limiting medicine-chest position, prevent medicine-chest from skidding off and drop, cause damages, by the setting hinged casing of mounting base and
The hinged mounting base of fixing seat, storage propeller fixed frame convenient for folding make agricultural remote sensing unmanned plane fold simpler convenience, side
Just the carrying and use of agricultural unmanned plane.
Detailed description of the invention
Fig. 1 is the structural schematic diagram of the utility model；Fig. 2 is the structure top view of the utility model；Fig. 3 is that this is practical
The second left adjusting bracket structural schematic diagram in novel.In figure: 10- casing assembly, 11- casing, the left adjusting bracket of 12- first, 13-
Second left adjusting bracket, the right adjusting bracket of 14- first, the right adjusting bracket of 15- second, 16- carry platform, 20- flight component, 21- installation
Seat, 22- fixing seat, 23- propeller, 30- adjust component, the first sliding block of 31-, the first adjusting rod of 32-, the first fixed link of 33-,
The second sliding block of 34-, the second adjusting rod of 35-, the second fixed link of 36-, 37- limited block.
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 agricultural remote sensing unmanned plane being easy to carry,
Including casing assembly 10, flight component 20 and component 30 is adjusted, casing assembly 10 includes casing 11, the first left adjusting bracket 12, the
Two left adjusting brackets 13, the first right adjusting bracket 14, the second right adjusting bracket 15 and carry platform 16；The first left adjusting bracket 12 is located at institute
It states on the left of 11 lower surface of casing, and is spirally connected fixation with the casing 11, the second left adjusting bracket 13 is located at the described first left tune
It is connected forwards, backwards below section frame 12 and mutually by adjusting component 30 along length；The first right adjusting bracket 14 is located at the casing 11
It on the right side of lower surface, and is fixedly connected with the casing 11, the second right adjusting bracket 15 is located under the described first right adjusting bracket 14
Just and mutually connected forwards, backwards by adjusting component 30 along length；Flight component 20 includes mounting base 21, fixing seat 22 and propeller
23, mounting base 21 is located in front of 11 left side wall of casing, and is fixedly connected with casing 11, and fixing seat 22 is located at 21 left side of mounting base
Wall, and be fixedly connected with mounting base 21, propeller 23 is located on the left of 22 upper surface of fixing seat, and is rotatablely connected with fixing seat 22；
Adjusting component 30 includes the first sliding block 31, the first adjusting rod 32, the first fixed link 33, the second sliding block 34, the second adjusting rod 35, the
Two fixed links 36 and limited block 37, the first sliding block 31 are located at the top of the first left 12 inner sidewall of adjusting bracket, and with the first left adjusting bracket
12 are slidably connected, and the first adjusting rod 32 is located at 31 lower surface of the first sliding block, and is fixedly connected with the first sliding block 31, the first fixed link
33 are located at the first left 12 left side wall bottom of adjusting bracket, and are fixedly connected with the first left adjusting bracket 12, and the second sliding block 34 is located at second
Left 13 inner sidewall bottom of adjusting bracket, and be slidably connected with the second left adjusting bracket 13, the second adjusting rod 35 is located at 34 table of the second sliding block
Face, and being fixedly connected with the second sliding block 34, the second fixed link 36 are located at the top of the second left 13 left side wall of adjusting bracket, and with second left side
Adjusting bracket 13 is fixedly connected, and limited block 37 is located on the left of 16 upper surface of carry platform, and is fixedly connected with carry platform 16.
It in the present embodiment, is fixedly connected between the first adjusting rod 32 and the second adjusting rod 35, the first sliding block 31 and the is set
Two sliding blocks 34 facilitate internal first adjusting rod 32 of drive and the second adjusting rod 35 mobile, extend remote sensing unmanned plane support frame length,
First fixed link 33 and 36 surface of the second fixed link are equipped with screw thread, and the first fixed link 33 and the second fixed link 36 is arranged, facilitates spiral shell
It connects and fixes the first adjusting rod 32 and the first left adjusting bracket 12 and the second adjusting rod 35 and the second left adjusting bracket 13,37 shape of limited block
Be it is rectangular, setting limited block 37 prevent medicine-chest from skidding off for limiting medicine-chest position and drop.
In the present embodiment, the first sliding block 31 and the second sliding block 34 are set, facilitate internal first adjusting rod 32 of drive and the
Two adjusting rods 35 are mobile, extend remote sensing unmanned plane support frame length, adapt to different height medicine-chest and fix, make agricultural remote sensing unmanned plane
It is more convenient to use, and the first fixed link 33 and the second fixed link 36 is arranged, and is conveniently spirally connected and fixes the first adjusting rod 32 and the
One left adjusting bracket 12 and the second adjusting rod 35 and the second left adjusting bracket 13 make to control the flexible length of agricultural remote sensing unmanned plane support rod
Simpler convenience is spent, setting limited block 37 prevents medicine-chest from skidding off and drop for limiting medicine-chest position.
Further, the first adjusting rod 32 and the first left adjusting bracket 12 and the second adjusting rod 35 and the second left adjusting bracket 13 are logical
It crosses the first sliding block 31 and the second sliding block 34 is slidably connected.
In the present embodiment, it is slidably connected the first adjusting rod 32 and the first left adjusting by the first sliding block 31 and the second sliding block 34
Frame 12 and the second adjusting rod 35 and the second left adjusting bracket 13 facilitate and extend remote sensing unmanned plane support frame length, adapt to different height
Medicine-chest is fixed, and uses agricultural remote sensing unmanned plane more convenient.
Further, the second adjusting rod 35 and the second left adjusting bracket 13 and the first adjusting rod 32 and the first left adjusting bracket 12 are logical
It crosses the second fixed link 36 and the first fixed link 33 is spirally connected fixation.
In the present embodiment, it is spirally connected by the second fixed link 36 and the first fixed link 33 and fixes the second adjusting rod 35 and second
Left adjusting bracket 13 and the first adjusting rod 32 and the first left adjusting bracket 12, make to control agricultural remote sensing unmanned plane support rod collapsing length more
Add simple and convenient.
Further, mounting base 21 and casing 11 and 22 mounting base 21 of fixing seat pass through hinged.
In the present embodiment, pass through hinged mounting base 21 and casing 11 and fixing seat 22 and mounting base 21, storage convenient for folding
Propeller fixed frame makes agricultural remote sensing unmanned plane fold simpler convenience, facilitates the carrying and use of agricultural unmanned plane.
Further, mounting base 21, fixing seat 22 and propeller 23 are flight instruments, and the quantity of flight instruments is four,
In front of 11 left side wall of casing and in front of left side wall rear and 11 right side wall of casing and right side wall rear is fixed with casing 11
Connection.
In the present embodiment, pass through in front of 11 left side wall of casing and in front of left side wall rear and 11 right side wall of casing and right side
A flight instruments are respectively arranged in wall rear, convenient to provide sufficient power for agricultural remote sensing unmanned plane, ensure the normal of plant protection sprinkling
It carries out.
The working principle and process for using of the utility model: after the utility model installs, by agricultural remote sensing unmanned plane
Fully charged, according to medicine-chest specification, spiral shell the first fixed link 33 of pine and the second fixed link 36 are extended inside the first left adjusting bracket 12
It is suitable for development length that the second adjusting rod 35 inside first adjusting rod 32 and the second left adjusting bracket 13, which is arranged, then solid by first
Fixed pole 33 and the second fixed link 36 are spirally connected and fix the first adjusting rod 32 and the first left adjusting bracket 12 and the second adjusting rod 35 and second
Left adjusting bracket 13 fixes medicine-chest, connects flusher, starts agricultural remote sensing unmanned plane switch, is operated, controlled by operator
Sprinkling closes agricultural remote sensing unmanned plane switch, folds mounting base 21 and fixing seat 22, store super helix paddle fixed frame when not used,
Agricultural unmanned plane is stored, is continued to use to next time.
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 (5)
1. a kind of agricultural remote sensing unmanned plane for being easy to carry, it is characterised in that: including casing assembly (10), flight component (20) and
Adjust component (30), the casing assembly (10) include casing (11), the first left adjusting bracket (12), the second left adjusting bracket (13),
First right adjusting bracket (14), the second right adjusting bracket (15) and carry platform (16)；The first left adjusting bracket (12) is located at the machine
It on the left of shell (11) lower surface, and is spirally connected fixation with the casing (11), it is left that the second left adjusting bracket (13) is located at described first
It is connected forwards, backwards below adjusting bracket (12) and mutually by adjusting component (30) along length；The first right adjusting bracket (14) is located at institute
It states on the right side of casing (11) lower surface, and is fixedly connected with the casing (11), the second right adjusting bracket (15) is located at described the
It is connected forwards, backwards below one right adjusting bracket (14) and mutually by adjusting component (30) along length；The carry platform (16) is located at described
Below second left adjusting bracket (13) and the first right adjusting bracket (14) and with the described second left adjusting bracket (13) and described first
Right adjusting bracket (14) is fixedly connected；
The flight component (20) includes mounting base (21), fixing seat (22) and propeller (23), and the mounting base (21) is located at
It in front of casing (11) left side wall, and is fixedly connected with the casing (11), the fixing seat (22) is located at the mounting base
(21) left side wall, and be fixedly connected with the mounting base (21), the propeller (23) is located at the fixing seat (22) upper surface
Left side, and be rotatablely connected with the fixing seat (22)；
The adjusting component (30) includes the first sliding block (31), the first adjusting rod (32), the first fixed link (33), the second sliding block
(34), the second adjusting rod (35), the second fixed link (36) and limited block (37), it is left that first sliding block (31) is located at described first
It at the top of adjusting bracket (12) inner sidewall, and is slidably connected with the described first left adjusting bracket (12), first adjusting rod (32) is located at
First sliding block (31) lower surface, and be fixedly connected with first sliding block (31), first fixed link (33) is located at institute
The first left adjusting bracket (12) left side wall bottom is stated, and is fixedly connected with the described first left adjusting bracket (12), second sliding block
(34) it is located at the described second left adjusting bracket (13) inner sidewall bottom, and is slidably connected with the described second left adjusting bracket (13), it is described
Second adjusting rod (35) is located at the second sliding block (34) upper surface, and is fixedly connected with second sliding block (34), and described
Two fixed links (36) are located at the top of the described second left adjusting bracket (13) left side wall, and fix and connect with the described second left adjusting bracket (13)
It connects, the limited block (37) is located on the left of carry platform (16) upper surface, and is fixedly connected with the carry platform (16).
2. a kind of agricultural remote sensing unmanned plane for being easy to carry according to claim 1, it is characterised in that: described first is adjusted
Bar (32) and the first left adjusting bracket (12) and second adjusting rod (35) and the second left adjusting bracket (13) pass through institute
It states the first sliding block (31) and second sliding block (34) is slidably connected.
3. a kind of agricultural remote sensing unmanned plane for being easy to carry according to claim 1, it is characterised in that: described second is adjusted
Bar (35) and the second left adjusting bracket (13) and first adjusting rod (32) and the first left adjusting bracket (12) pass through institute
It states the second fixed link (36) and first fixed link (33) is spirally connected fixation.
4. a kind of agricultural remote sensing unmanned plane for being easy to carry according to claim 1, it is characterised in that: the mounting base
(21) pass through hingedly with the casing (11) with the fixing seat (22) and the mounting base (21).
5. a kind of agricultural remote sensing unmanned plane for being easy to carry according to claim 1, it is characterised in that: the mounting base
(21), the fixing seat (22) and the propeller (23) are flight instruments, and the quantity of the flight instruments is four, are set to institute
State in front of casing (11) left side wall and left side wall rear and the casing (11) right side wall front and right side wall rear with it is described
Casing (11) is fixedly connected.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820494984.7U CN208585403U (en) | 2018-04-09 | 2018-04-09 | A kind of agricultural remote sensing unmanned plane being easy to carry |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820494984.7U CN208585403U (en) | 2018-04-09 | 2018-04-09 | A kind of agricultural remote sensing unmanned plane being easy to carry |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208585403U true CN208585403U (en) | 2019-03-08 |
Family
ID=65532184
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820494984.7U Expired - Fee Related CN208585403U (en) | 2018-04-09 | 2018-04-09 | A kind of agricultural remote sensing unmanned plane being easy to carry |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208585403U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111846224A (en) * | 2020-07-23 | 2020-10-30 | 湖南星图空间信息技术有限公司 | Remote sensing unmanned aerial vehicle based on remote sensing technology is easily carried article |
-
2018
- 2018-04-09 CN CN201820494984.7U patent/CN208585403U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111846224A (en) * | 2020-07-23 | 2020-10-30 | 湖南星图空间信息技术有限公司 | Remote sensing unmanned aerial vehicle based on remote sensing technology is easily carried article |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN206155784U (en) | Unmanned aerial vehicle | |
| EP3632793B1 (en) | Unmanned aerial vehicle and landing gear thereof | |
| CN109896004A (en) | A kind of unmanned plane of scalable horn | |
| CN208585403U (en) | A kind of agricultural remote sensing unmanned plane being easy to carry | |
| CN208102337U (en) | A kind of telescopic unmanned plane flight support frame structure | |
| CN102180267A (en) | Umbrella-shaped foldable multi-rotor aircraft | |
| CN108216603A (en) | A kind of foldable four axis unmanned plane of long wheelbase | |
| CN208278328U (en) | A kind of agricultural plant protection unmanned plane | |
| CN108791917A (en) | A kind of unmanned plane of taking photo by plane of multi-faceted shooting | |
| CN106088612A (en) | A kind of portable concrete pay-off for building | |
| CN113567183A (en) | Soil sampling device | |
| CN207225637U (en) | A kind of multi-rotor unmanned aerial vehicle horn is remotely controlled draw off gear | |
| CN107199938B (en) | A kind of caravan carriage expanding type chassis of automatic lifting | |
| CN202054142U (en) | Umbrella-shaped foldable aircraft with multiple rotors | |
| CN109866914B (en) | Fixed wing unmanned aerial vehicle running takeoff auxiliary device | |
| CN209306376U (en) | A kind of clothes hanger in intelligent garment hanging system | |
| CN110550198A (en) | Rock wall fixed point type unmanned aerial vehicle | |
| CN208412170U (en) | A kind of unmanned aerial vehicle station unmanned plane recycling shutdown platform | |
| CN207744628U (en) | A kind of spraying control device of plant protection aircraft | |
| CN209229424U (en) | A kind of desk lamp | |
| CN209581857U (en) | A kind of collapsible damping device that rises and falls | |
| CN209683992U (en) | A kind of unmanned plane with folded antenna | |
| CN208530260U (en) | A kind of automobile outdoor sun shade | |
| CN207311808U (en) | A kind of four axis plant protection unmanned planes | |
| CN207783570U (en) | A kind of weeder based on unmanned plane |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20190308 Termination date: 20210409 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |