CN207985196U - A kind of unmanned plane of taking photo by plane convenient for adjusting camera - Google Patents
A kind of unmanned plane of taking photo by plane convenient for adjusting camera Download PDFInfo
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- CN207985196U CN207985196U CN201820344432.8U CN201820344432U CN207985196U CN 207985196 U CN207985196 U CN 207985196U CN 201820344432 U CN201820344432 U CN 201820344432U CN 207985196 U CN207985196 U CN 207985196U
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- fuselage
- mounting plate
- plane
- hole
- unmanned plane
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Abstract
The utility model discloses a kind of convenient for adjusting the unmanned plane of taking photo by plane of camera,Including wing,Undercarriage,Fixed link,Mounting plate,Fuselage,First through hole,Connecting rod,Camera,Annular groove,Slide bar,Cooling mechanism,Fixed frame,Motor,Electric pushrod,Resetting spring,Speed reducer and accumulator,Wing is mounted on the side top quadrangle of fuselage,The two bottom sides of fuselage are connect by resetting spring with undercarriage,The bottom center of fuselage offers first through hole,The top inner wall of fuselage offers annular groove,Annular groove is connect by slide bar with electric pushrod,The output shaft of electric pushrod is connected with mounting plate,The two bottom sides of mounting plate are equipped with fixed link,The corresponding side surface of fixed link is connect by connecting rod with camera,The top of mounting plate is connect by rotary shaft with speed reducer,The unmanned plane is reasonable for structure,It can 360 ° of rotary takings,And convenient for adjusting the displacement of vertical direction,It is easy to operate,Heat dissipation effect is notable simultaneously.
Description
Technical field
The utility model is related to air vehicle technique field, specially a kind of unmanned planes of taking photo by plane convenient for adjusting camera.
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, wherein boat
Unmanned plane is clapped mainly including unmanned plane and the aerial device being arranged on unmanned plane, and unmanned plane photography is with unmanned
Aircraft is as aerial platform, with airborne sensory equipment, such as high resolution CCD digital camera, light optical camera, infrared scan
Instrument, laser scanner, magnetic determining device etc. obtain information, are handled image information with computer, and according to certain required precision
It is fabricated to image.Total system design and optimal combination in terms of have the characteristics that protrusion, be integrated with high-altitude shoot, be remotely controlled,
The new application technology of telemetry, video image microwave transmission and computer image information processing, existing unmanned plane of taking photo by plane
Camera angle adjustment amplitude is small, can not carry out 360 ° omni-directional rotation, and the function without up and down adjustment, radiate simultaneously
Effect is poor, fragile parts.
Utility model content
The purpose of this utility model is to provide a kind of convenient for adjusting the unmanned plane of taking photo by plane of camera, to solve above-mentioned background
The problem of being proposed in technology.
In order to solve the above-mentioned technical problem, the utility model provides the following technical solutions：It is a kind of to be convenient for adjusting camera
It takes photo by plane unmanned plane, including wing, undercarriage, fixed link, mounting plate, fuselage, first through hole, connecting rod, camera, annular are sliding
Slot, slide bar, cooling mechanism, fixed frame, motor, electric pushrod, resetting spring, speed reducer and accumulator, the wing are mounted on
The two bottom sides of the side top quadrangle of fuselage, the fuselage are connect by resetting spring with undercarriage, the bottom of the fuselage
Center offers first through hole, and the top inner wall of the fuselage offers annular groove, and the annular groove passes through slide bar and electricity
Dynamic push rod connection, the output shaft of the electric pushrod are connected with mounting plate, and the two bottom sides of the mounting plate are equipped with fixed link,
The corresponding side surface of the fixed link is connect by connecting rod with camera, and the top of the mounting plate passes through rotary shaft and speed reducer
Connection, the top of the speed reducer and the output axis connection of motor, the motor are fixedly mounted on cooling mechanism by fixed frame
Bottom, the top both sides of the fuselage are equipped with accumulator, and the top insertion of the fuselage is equipped with cooling mechanism, described to dissipate
Heat engine structure is made of heat-conducting plate, heat radiation box, the second through-hole, heat dissipation scales and heating column, and the bottom of the heat radiation box opens up
There is the second through-hole, the side inner walls of the top uncovered of the heat radiation box, the heat radiation box are horizontally installed with heat-conducting plate, described
Several heating columns are equidistantly positioned at the top of heat-conducting plate, equidistant be socketed is equipped with heat dissipation scales on the heating column.
Further, the wing is bolted with fuselage.
Further, the fixed link is connected through a screw thread with connecting rod.
Further, the diameter of the first through hole is bigger 1cm than the diameter of mounting plate.
Further, it is bolted between the resetting spring and undercarriage and fuselage.
Further, the diameter of second through-hole is bigger 1cm than the diameter of motor.
Compared with prior art, the advantageous effect that the utility model is reached is：This is convenient for the nothing of taking photo by plane for adjusting camera
Man-machine, the two bottom sides of fuselage are connect by resetting spring with undercarriage, can effectively slow down impact force when UAV Landing,
Avoid sharp pounding that damage of components, the bottom center of fuselage is caused to offer first through hole, the top inner wall of fuselage offers
Annular groove, annular groove are connect by slide bar with electric pushrod, and the output shaft of electric pushrod is connected with mounting plate, by electronic
Push rod can adjust displacement of the camera in vertical direction, and convenient for shooting of finding a view, the two bottom sides of mounting plate are equipped with fixed link,
The corresponding side surface of fixed link is connect by connecting rod with camera, and the top of mounting plate is connect by rotary shaft with speed reducer, is subtracted
The top of fast machine and the output axis connection of motor can make camera carry out 360 ° of rotation, convenient for shooting various angles, fuselage
Top insertion cooling mechanism is installed, cooling mechanism is by heat-conducting plate, heat radiation box, the second through-hole, heat dissipation scales and heating column
The bottom of composition, heat radiation box offers the second through-hole, the top uncovered of heat radiation box, the side inner walls level peace of heat radiation box
Equipped with heat-conducting plate, several heating columns are equidistantly positioned at the top of heat-conducting plate, equidistant be socketed is equipped with heat dissipation squama on heating column
Piece, the heat that motor running generates pass to heating column by heat-conducting plate, are distributed into air eventually by heat dissipation scales, the nothing
It is man-machine reasonable for structure, can 360 ° of rotary takings, it is easy to operate and convenient for adjusting the displacement of vertical direction, while heat dissipation effect is aobvious
It writes.
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 overall structure elevational schematic view of the utility model；
Fig. 2 is the fuselage interior structural schematic diagram of the utility model；
Fig. 3 is the cooling mechanism structural schematic diagram of the utility model；
In figure：1- wings；2- undercarriages；3- fixed links；4- mounting plates；5- fuselages；6- first through hole；7- connecting rods；8-
Camera；9- annular grooves；10- slide bars；11- cooling mechanisms；12- fixed frames；13- motors；14- electric pushrods；15- resets bullet
Spring；16- speed reducers；17- heat-conducting plates；18- heat radiation boxes；The second through-holes of 19-；20- heat dissipation scales；21- heating columns；22- electric power storages
Pond.
Specific implementation mode
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
The every other embodiment obtained, shall fall within the protection scope of the present invention.
- 3 are please referred to Fig.1, the utility model provides a kind of technical solution：It is a kind of to take photo by plane nobody convenient for adjusting camera
Machine, including wing 1, undercarriage 2, fixed link 3, mounting plate 4, fuselage 5, first through hole 6, connecting rod 7, camera 8, annular groove
9, slide bar 10, cooling mechanism 11, fixed frame 12, motor 13, electric pushrod 14, resetting spring 15, speed reducer 16 and accumulator 22,
Wing 1 is mounted on the side top quadrangle of fuselage 5, and the two bottom sides of fuselage 5 are connect by resetting spring 15 with undercarriage 2, machine
The bottom center of body 5 offers first through hole 6, and the top inner wall of fuselage 5 offers annular groove 9, and annular groove 9 passes through slide bar
10 connect with electric pushrod 14, and the output shaft of electric pushrod 14 is connected with mounting plate 4, and the two bottom sides of mounting plate 4 are equipped with admittedly
The corresponding side surface of fixed pole 3, fixed link 3 is connect by connecting rod 7 with camera 8, and the top of mounting plate 4 passes through rotary shaft and deceleration
Machine 16 connects, and the top of speed reducer 16 and the output axis connection of motor 13, motor 13 are fixedly mounted on heat dissipation by fixed frame 12
The top both sides of the bottom of mechanism 11, fuselage 5 are equipped with accumulator 22, and the top insertion of fuselage 5 is equipped with cooling mechanism 11, dissipates
Heat engine structure 11 is made of heat-conducting plate 17, heat radiation box 18, the second through-hole 19, heat dissipation scales 20 and heating column 21, heat radiation box 18
Bottom offer the second through-hole 19, the top uncovered of heat radiation box 18, the side inner walls of heat radiation box 18, which are horizontally installed with, to be led
The top of hot plate 17, heat-conducting plate 17 has been equidistantly positioned several heating columns 21, and equidistant be socketed is equipped with heat dissipation on heating column 21
Scale 20.
Further, wing 1 is bolted with fuselage 5.
Further, fixed link 3 is connected through a screw thread with connecting rod 7.
Further, the diameter of first through hole 6 is bigger 1cm than the diameter of mounting plate 4.
Further, it is bolted between resetting spring 15 and undercarriage 2 and fuselage 5.
Further, the diameter of the second through-hole 19 is bigger 1cm than the diameter of motor 13.
Operation principle：The two bottom sides of fuselage 5 are connect by resetting spring 15 with undercarriage 2, nobody can be effectively slowed down
Impact force when machine lands, avoids sharp pounding that damage of components, the bottom center of fuselage 5 is caused to offer first through hole 6, machine
The top inner wall of body 5 offers annular groove 9, and annular groove 9 is connect by slide bar 10 with electric pushrod 14, electric pushrod 14
Output shaft is connected with mounting plate 4, and displacement of the camera 8 in vertical direction can be adjusted by electric pushrod 14, is clapped convenient for finding a view
It takes the photograph, the two bottom sides of mounting plate 4 are equipped with fixed link 3, and the corresponding side surface of fixed link 3 is connect by connecting rod 7 with camera 8,
The top of mounting plate 4 is connect by rotary shaft with speed reducer 16, the top of speed reducer 16 and the output axis connection of motor 13, can be with
Camera 8 is set to carry out 360 ° of rotation, convenient for shooting various angles, the top insertion of fuselage 5 is equipped with cooling mechanism 11, radiates
Mechanism 11 is made of heat-conducting plate 17, heat radiation box 18, the second through-hole 19, heat dissipation scales 20 and heating column 21, heat radiation box 18
Bottom offers the second through-hole 19, the top uncovered of heat radiation box 18, and the side inner walls of heat radiation box 18 are horizontally installed with heat conduction
The top of plate 17, heat-conducting plate 17 has been equidistantly positioned several heating columns 21, and equidistant be socketed is equipped with heat dissipation squama on heating column 21
Piece 20, motor 13 running generate heat heating column 21 is passed to by heat-conducting plate 17, eventually by heat dissipation scales 20 distribute to
In air, the unmanned plane is reasonable for structure, can 360 ° of rotary takings, and convenient for adjust vertical direction displacement, it is easy to operate, simultaneously
Heat dissipation effect is notable.
Finally it should be noted that：The above descriptions are merely preferred embodiments of the present invention, is not limited to this
Utility model, although the utility model is described in detail with reference to the foregoing embodiments, for those skilled in the art
For, it still can be with technical scheme described in the above embodiments is modified, or to which part technical characteristic
Carry out equivalent replacement.Within the spirit and principle of the utility model, any modification, equivalent replacement, improvement and so on,
It should be included within the scope of protection of this utility model.
Claims (6)
1. a kind of unmanned plane of taking photo by plane convenient for adjusting camera, including wing (1), undercarriage (2), fixed link (3), mounting plate
(4), fuselage (5), first through hole (6), connecting rod (7), camera (8), annular groove (9), slide bar (10), cooling mechanism
(11), fixed frame (12), motor (13), electric pushrod (14), resetting spring (15), speed reducer (16) and accumulator (22),
It is characterized in that：The wing (1) is mounted on the side top quadrangle of fuselage (5), and the two bottom sides of the fuselage (5) pass through reset
Spring (15) is connect with undercarriage (2), and the bottom center of the fuselage (5) offers first through hole (6), the fuselage (5)
Top inner wall offers annular groove (9), and the annular groove (9) is connect by slide bar (10) with electric pushrod (14), described
The output shaft of electric pushrod (14) is connected with mounting plate (4), and the two bottom sides of the mounting plate (4) are equipped with fixed link (3), institute
The corresponding side surface for stating fixed link (3) is connect by connecting rod (7) with camera (8), passes through rotation at the top of the mounting plate (4)
Axis is connect with speed reducer (16), the output axis connection at the top and motor (13) of the speed reducer (16), and the motor (13) is logical
The bottom that fixed frame (12) is fixedly mounted on cooling mechanism (11) is crossed, the top both sides of the fuselage (5) are equipped with accumulator
(22), the top insertion of the fuselage (5) is equipped with cooling mechanism (11), the cooling mechanism (11) by heat-conducting plate (17), dissipate
Hot tank body (18), the second through-hole (19), heat dissipation scales (20) and heating column (21) composition, the bottom of the heat radiation box (18) is opened
Equipped with the second through-hole (19), the top uncovered of the heat radiation box (18), the side inner walls level peace of the heat radiation box (18)
Equipped with heat-conducting plate (17), several heating columns (21), the heating column (21) have been equidistantly positioned at the top of the heat-conducting plate (17)
Upper equidistant socket is equipped with heat dissipation scales (20).
2. a kind of unmanned plane of taking photo by plane convenient for adjusting camera according to claim 1, it is characterised in that：The wing
(1) it is bolted with fuselage (5).
3. a kind of unmanned plane of taking photo by plane convenient for adjusting camera according to claim 1, it is characterised in that：The fixed link
(3) it is connected through a screw thread with connecting rod (7).
4. a kind of unmanned plane of taking photo by plane convenient for adjusting camera according to claim 1, it is characterised in that：Described first is logical
The diameter in hole (6) is bigger 1cm than the diameter of mounting plate (4).
5. a kind of unmanned plane of taking photo by plane convenient for adjusting camera according to claim 1, it is characterised in that：The reset bullet
It is bolted between spring (15) and undercarriage (2) and fuselage (5).
6. a kind of unmanned plane of taking photo by plane convenient for adjusting camera according to claim 1, it is characterised in that：Second through-hole
(19) diameter is bigger 1cm than the diameter of motor (13).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820344432.8U CN207985196U (en) | 2018-03-14 | 2018-03-14 | A kind of unmanned plane of taking photo by plane convenient for adjusting camera |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820344432.8U CN207985196U (en) | 2018-03-14 | 2018-03-14 | A kind of unmanned plane of taking photo by plane convenient for adjusting camera |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207985196U true CN207985196U (en) | 2018-10-19 |
Family
ID=63827903
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820344432.8U Expired - Fee Related CN207985196U (en) | 2018-03-14 | 2018-03-14 | A kind of unmanned plane of taking photo by plane convenient for adjusting camera |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207985196U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111017221A (en) * | 2019-12-12 | 2020-04-17 | 张自明 | Aviation agricultural sprinkling irrigation unmanned aerial vehicle |
| CN113329601A (en) * | 2021-07-07 | 2021-08-31 | 辽宁工程技术大学 | Unmanned aerial vehicle remote sensing device for surveying and mapping engineering measurement |
| CN113955104A (en) * | 2020-07-20 | 2022-01-21 | 江苏雨能水利工程有限公司 | Measure unmanned aerial vehicle linkage of hydrology |
-
2018
- 2018-03-14 CN CN201820344432.8U patent/CN207985196U/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111017221A (en) * | 2019-12-12 | 2020-04-17 | 张自明 | Aviation agricultural sprinkling irrigation unmanned aerial vehicle |
| CN113955104A (en) * | 2020-07-20 | 2022-01-21 | 江苏雨能水利工程有限公司 | Measure unmanned aerial vehicle linkage of hydrology |
| CN113329601A (en) * | 2021-07-07 | 2021-08-31 | 辽宁工程技术大学 | Unmanned aerial vehicle remote sensing device for surveying and mapping engineering measurement |
| CN113329601B (en) * | 2021-07-07 | 2023-12-01 | 郑道仓 | Unmanned aerial vehicle remote sensing device for surveying and mapping engineering measurement |
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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 |
Granted publication date: 20181019 Termination date: 20190314 |
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| CF01 | Termination of patent right due to non-payment of annual fee |