CN207985195U - A kind of folding unmanned plane of taking photo by plane - Google Patents
A kind of folding unmanned plane of taking photo by plane Download PDFInfo
- Publication number
- CN207985195U CN207985195U CN201820341105.7U CN201820341105U CN207985195U CN 207985195 U CN207985195 U CN 207985195U CN 201820341105 U CN201820341105 U CN 201820341105U CN 207985195 U CN207985195 U CN 207985195U
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- China
- Prior art keywords
- fuselage
- plane
- unmanned plane
- supporting rod
- propeller
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Abstract
The utility model discloses a kind of folding unmanned planes of taking photo by plane,Including unmanned plane main body,Fuselage,Side plate,Fixed plate,Camera,Convex block,First rotating shaft,Second shaft,Propeller fixed frame,Motor,Fixed seat,Supporting rod,Motion bar,Protective cover,Propeller,Fixed link,Buffer bar,Buffer spring,Pedestal,Buckle,Fixture block,Groove,Roll shaft and limit table top,The side of the unmanned plane main body is provided with fuselage,The bottom end of the fuselage is equipped with camera,The both sides of the fuselage are respectively connected with side plate,The both ends of the side plate are respectively connected with fixed plate,Both sides open up fluted inside the fixed plate,The lower end of the groove is provided with roll shaft,Supporting rod has been inserted in it in the upper end of the roll shaft,One end of the supporting rod is provided with motion bar,The side of the motion bar is equipped with propeller,The folding unmanned plane of taking photo by plane has easy to carry,The function of installation foldable and easy to disassemble,Improve the practicability used and convenience.
Description
Technical field
The utility model is related to air vehicle technique field, specially a kind of folding unmanned plane of taking photo by plane.
Background technology
UAV, abbreviation unmanned plane (UAV) are a kind of new concept weapon equipments being in rapidly developing,
It is low to have the advantages that maneuverability, rapid reaction, unmanned flight, operation require.Unmanned plane, can be with by carrying multiclass sensor
It realizes image real-time Transmission, high-risk areas detecting function, is the strong supplement of satellite remote sensing and traditional air remote sensing.Currently, nothing
Man-machine use scope has widened military affairs, scientific research, civilian three big field, specifically in electric power, communication, meteorology, agricultural, sea
Ocean, he explores, photographs, preventing and reducing natural disasters, Crop Estimation, drug law enforcement anti-smuggling, border patrol, the fields application such as public security anti-terrorism it is very wide.
Wherein, unmanned plane of taking photo by plane has extensive use in above-mentioned multiple fields.It takes photo by plane unmanned plane, includes mainly unmanned plane
And the aerial device being arranged on unmanned plane, wherein traditional unmanned plane of taking photo by plane mostly is integrated, embodiment is larger, does not have
Easy to carry, the function of installation foldable and easy to disassemble, therefore, a kind of folding unmanned plane of taking photo by plane of design is necessary
's.
Utility model content
The utility model provides a kind of folding unmanned plane of taking photo by plane, and can effectively solve mentioned above in the background art
Problem.
To achieve the above object, the utility model provides the following technical solutions:A kind of folding unmanned plane of taking photo by plane, including
Unmanned plane main body, fuselage, side plate, fixed plate, camera, convex block, first rotating shaft, the second shaft, propeller fixed frame, motor,
It is fixed seat, supporting rod, motion bar, protective cover, propeller, fixed link, buffer bar, buffer spring, pedestal, buckle, fixture block, recessed
Slot, roll shaft and limit table top, the side of the unmanned plane main body are provided with fuselage, and the bottom end of the fuselage is equipped with camera,
The both sides of the fuselage are respectively connected with side plate, and the both ends of the side plate are respectively connected with fixed plate, and both sides are equal inside the fixed plate
Open up fluted, the lower end of the groove is provided with roll shaft, passes through fixing piece adhesion, the roller between the roll shaft and fixed plate
Supporting rod has been inserted in the upper end of axis, is fixedly connected by first rotating shaft between the supporting rod and roll shaft, and the two of the supporting rod
Side is mounted on convex block, and one end of the supporting rod is provided with motion bar, passes through second turn between the motion bar and supporting rod
Axis is fixedly connected, and the side of the motion bar is connected with protective cover, and the inside of the protective cover is equipped with propeller, the spiral
It is fixedly connected by propeller fixed frame between paddle and protective cover, the bottom end of the protective cover is equipped with motor, the motor
One end is provided with fixed seat, and the side of the fixed seat is connected with buffer bar, and the interior welds of the buffer bar have buckle, described
It is provided with fixture block on the inside of buckle, is connected by fixed spring between the fixture block and buckle, the side setting of the buffer bar
There are buffer spring, the bottom end of the buffer bar to be provided with pedestal.
Preferably, the inside of the fuselage is equipped with charged lithium cells.
Preferably, the bottom end side of the fuselage is provided with radiating fin.
Preferably, second shaft is internally provided with limiting slot.
Preferably, the side of the pedestal is connected with rubber mount.
Preferably, the fuselage is a kind of component of carbon fibre materials.
Compared with prior art, the beneficial effects of the utility model:The utility model is scientific and reasonable for structure, side safe to use
Just, the side of the folding unmanned plane of taking photo by plane, unmanned plane main body is provided with fuselage, and fuselage uses cylindrical member, reduces
Fuselage weight, flight are more stablized, and the bottom end of fuselage is equipped with camera, can be shot to ground scene, the two of fuselage
Side is respectively connected with side plate, and the both ends of side plate are respectively connected with fixed plate, and both sides open up fluted, the lower end of groove inside fixed plate
It is provided with roll shaft, supporting rod, supporting rod and roll shaft have been inserted in by fixing piece adhesion, the upper end of roll shaft between roll shaft and fixed plate
Between be fixedly connected by first rotating shaft, the both sides of supporting rod are mounted on convex block, can be pushed to fix by supporting rod by roll shaft
The inside of plate, and the inside of groove is snapped onto by the convex block of supporting rod both sides, to realize the folding of propeller, carry in this way
It is more convenient, it occupies little space, applied widely, one end of supporting rod is provided with motion bar, leads between motion bar and supporting rod
It crosses the second shaft to be fixedly connected, under the action of the second shaft, propeller can be collapsed in the upper end of fixed plate, the one of motion bar
Side is connected with protective cover, and the inside of protective cover is equipped with propeller, solid by propeller fixed frame between propeller and protective cover
Fixed connection, the bottom end of protective cover are equipped with motor, provide power to propeller, one end of motor is provided with fixed seat, fixed seat
Side be connected with buffer bar, when unmanned plane lands, reduce the downward impulse force of unmanned plane, reduce damage, buffer bar
Interior welds have buckle, and fixture block is provided on the inside of buckle, and removing and installing for buffer bar, fixture block and buckle are realized by fixture block
Between connected by fixed spring, the side of buffer bar is provided with buffer spring, increases damping effect.
Description of the drawings
Attached drawing is used to provide a further understanding of the present invention, and a part for constitution instruction, with this practicality
Novel embodiment for explaining the utility model, does not constitute limitations of the present invention together.
In the accompanying drawings:
Fig. 1 is the structural schematic diagram of the utility model;
Fig. 2 is the vertical view of the utility model;
Fig. 3 is the fixed plate structure schematic diagram of the utility model;
Fig. 4 is the buffer bar structural schematic diagram of the utility model;
Fig. 5 is the buffer bar vertical view of the utility model;
Figure label:1, unmanned plane main body;2, fuselage;3, side plate;4, fixed plate;5, camera;6, convex block;7, first turn
Axis;8, the second shaft;9, propeller fixed frame;10, motor;11, fixed seat;12, supporting rod;13, motion bar;14, protective cover;
15, propeller;16, fixed link;17, buffer bar;18, buffer spring;19, pedestal;20, it buckles;21, fixture block;22, groove;23、
Roll shaft;24, table top is limited.
Specific implementation mode
The preferred embodiment of the utility model is illustrated below in conjunction with attached drawing, it should be understood that described herein excellent
It selects embodiment to be only used for describing and explaining the present invention, is not used to limit the utility model.
Embodiment:As shown in Figs. 1-5, a kind of technical solution of the utility model offer, a kind of folding unmanned plane of taking photo by plane,
Including unmanned plane main body 1, fuselage 2, side plate 3, fixed plate 4, camera 5, convex block 6, first rotating shaft 7, the second shaft 8, propeller
Fixed frame 9, motor 10, fixed seat 11, supporting rod 12, motion bar 13, protective cover 14, propeller 15, fixed link 16, buffer bar
17, buffer spring 18, pedestal 19, buckle 20, fixture block 21, groove 22, roll shaft 23 and limit table top 24, the one of unmanned plane main body 1
Side is provided with fuselage 2, and the bottom end of fuselage 2 is equipped with camera 5, and the both sides of fuselage 2 are respectively connected with side plate 3, and the both ends of side plate 3 are equal
Be connected with fixed plate 4,4 inside both sides of fixed plate open up fluted 22, and the lower end of groove 22 is provided with roll shaft 23, roll shaft 23 with
It has been inserted in supporting rod 12, has been passed through between supporting rod 12 and roll shaft 23 by fixing piece adhesion, the upper end of roll shaft 23 between fixed plate 4
First rotating shaft 7 is fixedly connected, and the both sides of supporting rod 12 are mounted on convex block 6, and one end of supporting rod 12 is provided with motion bar 13, living
It is fixedly connected by the second shaft 8 between lever 13 and supporting rod 12, the side of motion bar 13 is connected with protective cover 14, protective cover
14 inside is equipped with propeller 15, is fixedly connected by propeller fixed frame 9 between propeller 15 and protective cover 14, protective cover
14 bottom end is equipped with motor 10, and one end of motor 10 is provided with fixed seat 11, and the side of fixed seat 11 is connected with buffer bar 17,
The interior welds of buffer bar 17 have buckle 20, and the inside for buckling 20 is provided with fixture block 21, by solid between fixture block 21 and buckle 20
Determine spring connection, the side of buffer bar 17 is provided with buffer spring 18, and the bottom end of buffer bar 17 is provided with pedestal 19.
In order to which motor 10 can work normally, in the present embodiment, it is preferred that the inside of fuselage 2 is equipped with charged lithium cells.
It radiates for the ease of fuselage 2, in the present embodiment, it is preferred that the bottom end side of fuselage 2 is provided with radiating fin.
In order to make propeller 15 be maintained at horizontal position, in the present embodiment, it is preferred that the second shaft 8 is internally provided with
Limiting slot.
To the loss of pedestal when in order to reduce landing, in the present embodiment, it is preferred that it is soft that the side of pedestal 19 is connected with rubber
Pad.
In order to increase the fastness of fuselage 2, in the present embodiment, it is preferred that fuselage 2 is a kind of component of carbon fibre materials.
The operation principle and process for using of the utility model:The side of unmanned plane main body 1 is provided with fuselage 2, and fuselage 2 is adopted
With cylindrical member, reduce fuselage weight, flight is more stablized, and the bottom end of fuselage 2 is equipped with camera 5, can be to ground feelings
Scape is shot, and the both sides of fuselage 2 are respectively connected with side plate 3, and the both ends of side plate 3 are respectively connected with fixed plate 4,4 inside two of fixed plate
Side opens up fluted 22, and the lower end of groove 22 is provided with roll shaft 23, by fixing piece adhesion between roll shaft 23 and fixed plate 4,
Supporting rod 12 has been inserted in the upper end of roll shaft 23, is fixedly connected by first rotating shaft 7 between supporting rod 12 and roll shaft 23, supporting rod 12
Both sides be mounted on convex block 6, supporting rod 12 can push to the inside of fixed plate 4 by roll shaft 23 to, and pass through 12 liang of supporting rod
The convex block 6 of side snaps onto the inside of groove 22, to realize the folding of propeller, carries more convenient, occupies little space in this way,
Applied widely, one end of supporting rod 12 is provided with motion bar 13, solid by the second shaft 8 between motion bar 13 and supporting rod 12
Fixed connection can collapse propeller 15 in the upper end of fixed plate 4, the side of motion bar 13 connects under the action of the second shaft 8
There are protective cover 14, the inside of protective cover 14 that propeller 15 is installed, is fixed by propeller between propeller 15 and protective cover 14
Frame 9 is fixedly connected, and the bottom end of protective cover 14 is equipped with motor 10, provides power to propeller 15, one end of motor 10 is provided with
The side of fixed seat 11, fixed seat 11 is connected with buffer bar 17, and when unmanned plane lands, reduction unmanned plane is downward to be rushed
Power reduces damage, and the interior welds of buffer bar 17 have buckle 20, and the inside for buckling 20 is provided with fixture block 21, real by fixture block 21
Removing and installing for existing buffer bar 17, is connected between fixture block 21 and buckle 20 by fixed spring, the side setting of buffer bar 17
There is buffer spring 18, increases damping effect.
Finally it should be noted that:The foregoing is merely the preferred embodiments of the utility model, are not limited to this reality
With novel, although the utility model is described in detail with reference to the foregoing embodiments, those skilled in the art is come
Say, still can with technical scheme described in the above embodiments is modified, or to which part technical characteristic into
Row equivalent replacement.Within the spirit and principle of the utility model, any modification, equivalent replacement, improvement and so on, should all
It is included within the scope of protection of this utility model.
Claims (6)
1. a kind of folding unmanned plane of taking photo by plane, including unmanned plane main body (1), fuselage (2), side plate (3), fixed plate (4), camera shooting
Head (5), convex block (6), first rotating shaft (7), the second shaft (8), propeller fixed frame (9), motor (10), fixed seat (11), branch
Strut (12), motion bar (13), protective cover (14), propeller (15), fixed link (16), buffer bar (17), buffer spring (18),
Pedestal (19), buckle (20), fixture block (21), groove (22), roll shaft (23) and limit table top (24), it is characterised in that:The nothing
The side of man-machine main body (1) is provided with fuselage (2), and the bottom end of the fuselage (2) is equipped with camera (5), the fuselage (2)
Both sides are respectively connected with side plate (3), and the both ends of the side plate (3) are respectively connected with fixed plate (4), the internal both sides of the fixed plate (4)
It opens up fluted (22), the lower end of the groove (22) is provided with roll shaft (23), between the roll shaft (23) and fixed plate (4)
By fixing piece adhesion, supporting rod (12) has been inserted in the upper end of the roll shaft (23), the supporting rod (12) and roll shaft (23) it
Between be fixedly connected by first rotating shaft (7), the both sides of the supporting rod (12) are mounted on convex block (6), the supporting rod (12)
One end be provided with motion bar (13), be fixedly connected by the second shaft (8) between the motion bar (13) and supporting rod (12),
The side of the motion bar (13) is connected with protective cover (14), and the inside of the protective cover (14) is equipped with propeller (15), institute
It states and is fixedly connected by propeller fixed frame (9) between propeller (15) and protective cover (14), the bottom end of the protective cover (14)
Motor (10) is installed, one end of the motor (10) is provided with fixed seat (11), and the side of the fixed seat (11) is connected with
The interior welds of buffer bar (17), the buffer bar (17) have buckle (20), and fixture block is provided on the inside of the buckle (20)
(21), it is connect by fixed spring between the fixture block (21) and buckle (20), the side of the buffer bar (17) is provided with slow
Spring (18) is rushed, the bottom end of the buffer bar (17) is provided with pedestal (19).
2. the folding unmanned plane of taking photo by plane of one kind according to claim 1, which is characterized in that the inside of the fuselage (2)
Charged lithium cells are installed.
3. the folding unmanned plane of taking photo by plane of one kind according to claim 1, which is characterized in that the bottom end of the fuselage (2)
Side is provided with radiating fin.
4. the folding unmanned plane of taking photo by plane of one kind according to claim 1, which is characterized in that second shaft (8)
It is internally provided with limiting slot.
5. the folding unmanned plane of taking photo by plane of one kind according to claim 1, which is characterized in that the side of the pedestal (19)
It is connected with rubber mount.
6. the folding unmanned plane of taking photo by plane of one kind according to claim 1, which is characterized in that the fuselage (2) is one kind
The component of carbon fibre materials.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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CN201820341105.7U CN207985195U (en) | 2018-03-13 | 2018-03-13 | A kind of folding unmanned plane of taking photo by plane |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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CN201820341105.7U CN207985195U (en) | 2018-03-13 | 2018-03-13 | A kind of folding unmanned plane of taking photo by plane |
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CN207985195U true CN207985195U (en) | 2018-10-19 |
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CN201820341105.7U Expired - Fee Related CN207985195U (en) | 2018-03-13 | 2018-03-13 | A kind of folding unmanned plane of taking photo by plane |
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Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN113148159A (en) * | 2021-04-27 | 2021-07-23 | 桂林天经地纬遥感信息技术有限公司 | Unmanned aerial vehicle takes photo by plane |
CN113212758A (en) * | 2021-03-16 | 2021-08-06 | 广东海洋大学 | Novel unmanned aerial vehicle that security performance is high |
-
2018
- 2018-03-13 CN CN201820341105.7U patent/CN207985195U/en not_active Expired - Fee Related
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN113212758A (en) * | 2021-03-16 | 2021-08-06 | 广东海洋大学 | Novel unmanned aerial vehicle that security performance is high |
CN113148159A (en) * | 2021-04-27 | 2021-07-23 | 桂林天经地纬遥感信息技术有限公司 | Unmanned aerial vehicle takes photo by plane |
CN113148159B (en) * | 2021-04-27 | 2023-02-07 | 桂林天经地纬遥感信息技术有限公司 | Unmanned aerial vehicle takes photo by plane |
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Legal Events
Date | Code | Title | Description |
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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: 20181019 Termination date: 20190313 |