CN219468038U - Small-size unmanned aerial vehicle that makes a video recording - Google Patents
Small-size unmanned aerial vehicle that makes a video recording Download PDFInfo
- Publication number
- CN219468038U CN219468038U CN202320073272.9U CN202320073272U CN219468038U CN 219468038 U CN219468038 U CN 219468038U CN 202320073272 U CN202320073272 U CN 202320073272U CN 219468038 U CN219468038 U CN 219468038U
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- carbon fiber
- top plate
- aerial vehicle
- unmanned aerial
- image transmission
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- 230000005540 biological transmission Effects 0.000 claims abstract description 50
- 229920000049 Carbon (fiber) Polymers 0.000 claims abstract description 49
- 239000004917 carbon fiber Substances 0.000 claims abstract description 49
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 claims abstract description 49
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 claims abstract description 45
- 230000007246 mechanism Effects 0.000 claims abstract description 34
- 230000001105 regulatory effect Effects 0.000 claims abstract description 16
- 238000009434 installation Methods 0.000 claims description 5
- 229910000838 Al alloy Inorganic materials 0.000 claims description 3
- 230000001276 controlling effect Effects 0.000 claims description 3
- 230000005611 electricity Effects 0.000 abstract description 19
- 238000013461 design Methods 0.000 abstract description 8
- 230000008901 benefit Effects 0.000 abstract description 6
- 238000012546 transfer Methods 0.000 abstract description 6
- 230000009286 beneficial effect Effects 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 230000017525 heat dissipation Effects 0.000 description 2
- 238000001746 injection moulding Methods 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 239000000243 solution Substances 0.000 description 2
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 229910052802 copper Inorganic materials 0.000 description 1
- 239000010949 copper Substances 0.000 description 1
- 238000013016 damping Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000001681 protective effect Effects 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
Classifications
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
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Abstract
The utility model discloses a small-sized camera unmanned aerial vehicle, which comprises a frame, a carbon fiber top plate, four rotating mechanisms, a camera device, a flight control electric adjusting plate, a frame, an image transmission device and a positioning frame, wherein the frame is provided with four rotating mechanism mounting cavities and accommodating cavities which are arranged in a square shape; the carbon fiber top plate is fixedly arranged on the frame; the four rotating mechanisms are arranged on the carbon fiber top plate and are respectively positioned in the corresponding rotating mechanism mounting cavities; the camera device is arranged on the carbon fiber top plate; the flight control electricity regulating plate is positioned in the accommodating cavity; the image transmission device is arranged corresponding to the flight control electric adjusting plate and is positioned in the accommodating cavity; the locating rack is clamped between the flight control electric adjusting plate and the image transmission device. The carbon fiber top plate is arranged, so that the rigidity of the carbon fiber top plate is good, and the vibration is reduced; the setting of locating rack is convenient for fly accuse electricity and transfers the counterpoint equipment of board and image transmission device, and image transmission device corresponds to fly accuse electricity and transfers the board setting in the holding chamber, compact structure does benefit to unmanned aerial vehicle's miniaturized design.
Description
Technical Field
The utility model relates to the unmanned aerial vehicle field technology, in particular to a small-sized camera unmanned aerial vehicle.
Background
Along with the popularization of unmanned aerial vehicle technique, the unmanned aerial vehicle flight performance requirement is higher and higher, and unmanned aerial vehicle still needs to consider long-time duration and mount shooting demand when miniaturized to and maintain convenient design demand.
The unmanned aerial vehicle in the traditional technology has a plurality of defects on its own structure, for example: 1. because the body is low in rigidity and weak in power, a large battery cannot be mounted, the endurance is difficult to lift, and the insufficient rigidity can cause some vibration, if a camera is externally mounted, a damping mechanism is required to be additionally arranged to filter the vibration, the structure is complex, and the vibration can influence the flight control operation, so that the electric energy conversion efficiency is further affected; 2. because the mounting holes of the flight control electric adjusting plate and the image transmission device are not corresponding, the flight control electric adjusting plate and the image transmission device are required to be respectively fixed on the top plate and the frame when being fixed, the assembly is inconvenient, and heat is easy to accumulate between the flight control electric adjusting plate and the image transmission device, so that the operation stability of the image transmission device is affected; 3. most of the existing unmanned aerial vehicle parts adopt screw and nut matching structures for fixing and assembling, so that more unmanned aerial vehicle parts are caused, and production assembly and later maintenance are not facilitated.
Therefore, a new solution is needed to solve the above problems.
Disclosure of Invention
In view of the above, the present utility model aims at overcoming the drawbacks of the prior art, and its main object is to provide a small-sized camera unmanned aerial vehicle, which has a carbon fiber top plate with good rigidity and reduced vibration; and through being provided with the locating rack between flight control electricity regulating plate and image transmission device to it is fixed with flight control electricity regulating plate and image transmission device's mounting hole, be convenient for flight control electricity regulating plate and image transmission device's counterpoint equipment, and image transmission device corresponds flight control electricity regulating plate and set up in the holding chamber, compact structure does benefit to unmanned aerial vehicle's miniaturized design.
In order to achieve the above purpose, the present utility model adopts the following technical scheme:
a miniature camera unmanned aerial vehicle comprising:
the rack is provided with four rotary mechanism mounting cavities which are arranged in a square shape, and a containing cavity is arranged in an area surrounded by the corresponding four rotary mechanism mounting cavities in the rack;
the carbon fiber top plate is fixedly arranged on the frame and used for covering the accommodating cavity, and has good rigidity and reduces vibration;
the four rotating mechanisms are arranged on the carbon fiber top plate and are respectively positioned in the corresponding rotating mechanism mounting cavities;
the image pickup device is arranged on the carbon fiber top plate;
the flight control electric regulating plate is positioned in the accommodating cavity and used for controlling the rotation of the rotating mechanism;
the image transmission device is arranged corresponding to the flight control electric adjusting plate, is positioned in the accommodating cavity and is used for being connected with the camera device;
the locating rack, the locating rack presss from both sides and locates between flight control electricity transfer board and the image transmission device for supply flight control electricity transfer board and image transmission device's mounting hole fixed, the counterpoint equipment of being convenient for flight control electricity transfer board and image transmission device, and image transmission device corresponds flight control electricity transfer board and set up in the holding chamber, compact structure does benefit to unmanned aerial vehicle's miniaturized design.
As a preferable scheme, the flight control electric adjusting plate is positioned above the image transmission device, the flight control electric adjusting plate and the positioning frame are fixedly arranged at the bottom of the carbon fiber top plate, and the image transmission device is fixedly arranged at the bottom of the positioning frame.
As a preferable scheme, the locating frame is made of aluminum alloy, so that heat dissipation of the flight control electric adjusting plate and the image transmission device is facilitated, and the image transmission device can operate more stably.
As a preferable scheme, the carbon fiber top plate is pre-embedded with a plurality of nuts, an integral injection molding process of the pre-embedded nuts is used, the number of parts is reduced, and the unmanned aerial vehicle is more convenient to assemble.
As a preferable scheme, the front end, the middle part and the rear end of the carbon fiber top plate are locked on the frame through two fixing screws, the containing cavity is formed by enclosing the six fixing screws, and the carbon fiber top plate and the frame can be separated or installed only by the six fixing screws, so that the assembly is convenient.
As a preferable scheme, the rotary mechanism mounting cavity is in a duct shape, and according to aerodynamics, besides the rotary mechanism can generate lifting force, the duct-shaped arrangement can also enable the frame to generate partial additional lifting force, so that the endurance time and the thrust of the unmanned aerial vehicle are improved.
As a preferable scheme, the rotating mechanism comprises a motor and a blade connected to the bottom of the motor, and the motor is arranged at the bottom of the carbon fiber top plate.
As a preferable mode, the image pickup device is arranged on the top of the carbon fiber top plate and is positioned at the front end of the carbon fiber top plate.
As a preferable scheme, the camera device is arranged at the top of the carbon fiber top plate through a mounting frame, a camera device mounting position is arranged on the mounting frame, and the camera device is arranged at the camera device mounting position.
As a preferred scheme, still be equipped with the mounting hole site that supplies external camera to install on the mounting bracket, the mounting hole site has reserved a mounting hole site that can fix external camera on the mounting bracket, can be used to the customization demand of taking photo by plane, for example installs high definition moving camera at the mounting hole site, satisfies the demand of taking photo by plane of high definition.
Compared with the prior art, the utility model has obvious advantages and beneficial effects, and in particular, the technical scheme can be as follows:
the carbon fiber top plate is arranged, so that the rigidity of the carbon fiber top plate is good, and the vibration is reduced; and through being provided with the locating rack between flight control electricity regulating plate and image transmission device to it is fixed with flight control electricity regulating plate and image transmission device's mounting hole, be convenient for flight control electricity regulating plate and image transmission device's counterpoint equipment, and image transmission device corresponds flight control electricity regulating plate and set up in the holding chamber, compact structure does benefit to unmanned aerial vehicle's miniaturized design.
In order to more clearly illustrate the structural features and efficacy of the present utility model, the present utility model will be described in detail below with reference to the accompanying drawings and examples.
Drawings
FIG. 1 is a schematic perspective view of a preferred embodiment of the present utility model;
FIG. 2 is a perspective view of another view of the preferred embodiment of the present utility model;
FIG. 3 is an exploded view of a preferred embodiment of the present utility model;
FIG. 4 is a top view of a preferred embodiment of the present utility model.
The attached drawings are used for identifying and describing:
1. a frame; 2. a carbon fiber top plate; 3. a rotation mechanism; 4. a flight control electric regulating plate; 5. an image pickup device; 6. an image transmission device; 7. a positioning frame; 8. installing hole sites; 9. a rotating mechanism mounting cavity; 10. a receiving chamber; 11. a mounting column; 12. a backhaul antenna; 13. a protective ring; 14. a nut; 15. a set screw; 16. a motor; 17. a paddle; 18. a mounting frame; 19. a camera mounting position; 20. a mounting part; 21. a mounting hole; 22. and positioning holes.
Detailed Description
First, it should be noted that, in the description of the present utility model, the azimuth or positional relationship indicated by the terms "upper", "lower", "left", "right", etc. are based on the azimuth or positional relationship shown in the drawings, and are merely for convenience of describing the present utility model and simplifying the description, and do not indicate or imply that the apparatus or element to be referred to must have a specific azimuth, be configured and operated in a specific azimuth, and thus should not be construed as limiting the present utility model.
Referring to fig. 1 to 4, a specific structure of a preferred embodiment of the present utility model is shown, which includes a frame 1, a carbon fiber top plate 2, four rotating mechanisms 3, a flight control electric tuning board 4, an image pickup device 5, an image transmission device 6 and a positioning frame 7.
The machine frame 1 is provided with four rotary mechanism mounting cavities 9 which are arranged in a square shape, and an accommodating cavity 10 is arranged in an area which is surrounded by the corresponding four rotary mechanism mounting cavities 9 in the machine frame 1;
specifically, the front end, the middle part and the rear end in the area surrounded by the four rotating mechanism mounting cavities 9 are provided with two mounting posts 11, the four rotating mechanism mounting cavities 9 are arranged at intervals, the rotating mechanism mounting cavities 9 are communicated up and down, and the opening of the accommodating cavity 10 is arranged upwards; the rear end of the frame 1 is provided with a return antenna installation position for installing a return antenna, the return antenna installation position is provided with a return antenna 12, and the return antenna 12 is connected with the image transmission device 6;
preferably, a protection ring 13 is arranged on the periphery of the frame 1, and the protection ring 13 is arranged to reduce damage to the frame 1 caused by collision; the installation cavity 9 of the rotating mechanism is in a duct shape, and according to aerodynamics, besides the rotating mechanism 3 can generate lifting force, the duct-shaped installation can also enable the frame 1 to generate partial additional lifting force, so that the endurance time and the thrust of the unmanned aerial vehicle are improved.
The carbon fiber top plate 2 is fixedly arranged on the frame 1 and used for covering the accommodating cavity 10, and the carbon fiber top plate 2 has good rigidity and reduces vibration;
specifically, the carbon fiber top plate 2 is pre-embedded with a plurality of nuts 14, and an integral injection molding process of the pre-embedded nuts 14 is used, so that the number of parts is reduced, and the unmanned aerial vehicle is more convenient to assemble;
preferably, the front end, the middle part and the rear end of the carbon fiber top plate 2 are locked to the corresponding mounting posts 11 through two fixing screws 15, the accommodating cavity 10 is formed by enclosing between the six fixing screws 15, and the carbon fiber top plate 2 and the frame 1 can be separated or mounted only by the six fixing screws 15, so that the assembly is convenient.
The four rotating mechanisms 3 are arranged on the carbon fiber top plate 2 and are respectively positioned in the corresponding rotating mechanism mounting cavities 9; specifically, the rotating mechanism 3 comprises a motor 16 and a paddle 17 connected to the bottom of the motor 16, and the motor 16 is arranged at the bottom of the carbon fiber top plate 2; in this embodiment, the top of the motor 16 is fastened to the bottom of the carbon fiber top plate 2 by screws.
The image pickup device 5 is arranged on the carbon fiber top plate 2; specifically, the image pickup device 5 is disposed at the top of the carbon fiber top plate 2 and is located at the front end of the carbon fiber top plate 2, the image pickup device 5 is disposed at the top of the carbon fiber top plate 2 through a mounting frame 18, an image pickup device mounting position 19 is disposed on the mounting frame 18, and the image pickup device 5 is disposed at the image pickup device mounting position 19;
preferably, the mounting frame 18 is further provided with a mounting hole 8 for mounting an external camera, the mounting hole 8 is arranged at the rear side of the mounting position 19 of the camera device, and a mounting hole 8 capable of fixing the external camera is reserved on the mounting frame 18 and can be used for customizing aerial photographing requirements, for example, a high-definition moving camera is arranged at the mounting hole 8 to meet the high-definition aerial photographing requirements; the mounting frame 18 has a mounting portion 20, the camera device mounting position 19 is located the front side of mounting portion 20, the mounting hole site 8 is located the top of mounting portion 20, mounting portion 20 sets up in the bottom of carbon fiber roof 2, and a plurality of nuts 14 can supply mounting portion 20 lock solid for mounting portion 20 passes through the screw from bottom to top lock in the bottom of carbon fiber roof 2, nut 14 is copper nut.
The fly-control electric adjusting plate 4 is positioned in the accommodating cavity 10 and used for controlling the rotation mechanism 3 to operate, and the image transmission device 6 is arranged corresponding to the fly-control electric adjusting plate 4 and positioned in the accommodating cavity 10 and used for being connected with the image pickup device 5; specifically, the flight control electric adjusting plate 4 is located above the image transmission device 6, the flight control electric adjusting plate 4 and the positioning frame 7 are fixedly arranged at the bottom of the carbon fiber top plate 2 together, and the image transmission device 6 is fixedly arranged at the bottom of the positioning frame 7;
preferably, a positioning frame 7 is sandwiched between the flight control electric adjusting plate 4 and the image transmission device 6, the positioning frame 7 is used for fixing the flight control electric adjusting plate 4 and the mounting hole 21 of the image transmission device 6, so that the flight control electric adjusting plate 4 and the image transmission device 6 are convenient to assemble in a contraposition manner, and the image transmission device 6 is arranged in the accommodating cavity 10 corresponding to the flight control electric adjusting plate 4, so that the unmanned aerial vehicle is compact in structure and beneficial to miniaturization design of the unmanned aerial vehicle; the positioning frame 7 is made of aluminum alloy, so that heat dissipation of the flight control electric adjusting plate 4 and the image transmission device 6 is facilitated, and the image transmission device 6 can run more stably;
in this embodiment, the mounting holes 21 of the flight control electric tuning plate 4 and the image transmission device 6 are four arranged at four corners, the mounting holes 8 of the four flight control electric tuning plates 4 are located outside the area surrounded by the mounting holes 21 of the four image transmission devices 6, the positioning frame 7 is in a grid shape, four corners of the positioning frame 7 are respectively corresponding to the mounting holes 21 of the four flight control electric tuning plates 4 and the mounting holes 21 of the four image transmission devices 6, and positioning holes 22 are formed in the four corners of the positioning frame 7.
The design focus of the utility model is that:
the carbon fiber top plate is arranged, so that the rigidity of the carbon fiber top plate is good, and the vibration is reduced; and through being provided with the locating rack between flight control electricity regulating plate and image transmission device to it is fixed with flight control electricity regulating plate and image transmission device's mounting hole, be convenient for flight control electricity regulating plate and image transmission device's counterpoint equipment, and image transmission device corresponds flight control electricity regulating plate and set up in the holding chamber, compact structure does benefit to unmanned aerial vehicle's miniaturized design.
The foregoing description is only a preferred embodiment of the present utility model, and is not intended to limit the technical scope of the present utility model, so any minor modifications, equivalent changes and modifications made to the above embodiments according to the technical principles of the present utility model are still within the scope of the technical solutions of the present utility model.
Claims (10)
1. A miniature camera unmanned aerial vehicle, comprising:
the rack is provided with four rotary mechanism mounting cavities which are arranged in a square shape, and a containing cavity is arranged in an area surrounded by the corresponding four rotary mechanism mounting cavities in the rack;
the carbon fiber top plate is fixedly arranged on the rack and used for covering the accommodating cavity;
the four rotating mechanisms are arranged on the carbon fiber top plate and are respectively positioned in the corresponding rotating mechanism mounting cavities;
the image pickup device is arranged on the carbon fiber top plate;
the flight control electric regulating plate is positioned in the accommodating cavity and used for controlling the rotation of the rotating mechanism;
the image transmission device is arranged corresponding to the flight control electric adjusting plate, is positioned in the accommodating cavity and is used for being connected with the camera device;
the locating frame is clamped between the flight control electric adjusting plate and the image transmission device and is used for fixing the flight control electric adjusting plate and the image transmission device through mounting holes.
2. A miniature camera unmanned aerial vehicle as claimed in claim 1, wherein: the fly-control electric adjusting plate is positioned above the image transmission device, the fly-control electric adjusting plate and the positioning frame are fixedly arranged at the bottom of the carbon fiber top plate, and the image transmission device is fixedly arranged at the bottom of the positioning frame.
3. A miniature camera unmanned aerial vehicle according to claim 1 or 2, wherein: the locating rack is made of aluminum alloy.
4. A miniature camera unmanned aerial vehicle as claimed in claim 1, wherein: the carbon fiber roof is pre-embedded with a plurality of nuts.
5. A miniature camera unmanned aerial vehicle as claimed in claim 1 or 4, wherein: the front end, the middle part and the rear end of the carbon fiber top plate are locked on the rack through two fixing screws, and the containing cavity is formed by surrounding the six fixing screws.
6. A miniature camera unmanned aerial vehicle as claimed in claim 1, wherein: the rotary mechanism installation cavity is in a duct shape.
7. A miniature camera unmanned aerial vehicle as claimed in claim 1 or 6, wherein: the rotating mechanism comprises a motor and paddles connected to the bottom of the motor, and the motor is arranged at the bottom of the carbon fiber top plate.
8. A miniature camera unmanned aerial vehicle as claimed in claim 1, wherein: the camera device is arranged at the top of the carbon fiber top plate and is positioned at the front end of the carbon fiber top plate.
9. The miniature camera unmanned aerial vehicle of claim 8, wherein: the camera device is arranged at the top of the carbon fiber top plate through the mounting frame, a camera device mounting position is arranged on the mounting frame, and the camera device is arranged at the camera device mounting position.
10. The miniature camera unmanned aerial vehicle of claim 9, wherein: the mounting frame is also provided with a mounting hole site for mounting an external camera, and the mounting hole site is arranged at the rear side of the mounting position of the camera device.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202320073272.9U CN219468038U (en) | 2023-01-10 | 2023-01-10 | Small-size unmanned aerial vehicle that makes a video recording |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202320073272.9U CN219468038U (en) | 2023-01-10 | 2023-01-10 | Small-size unmanned aerial vehicle that makes a video recording |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN219468038U true CN219468038U (en) | 2023-08-04 |
Family
ID=87437864
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202320073272.9U Active CN219468038U (en) | 2023-01-10 | 2023-01-10 | Small-size unmanned aerial vehicle that makes a video recording |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN219468038U (en) |
-
2023
- 2023-01-10 CN CN202320073272.9U patent/CN219468038U/en active Active
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