CN215399373U - Full-angle multi-load matched modular aerial photography unmanned aerial vehicle - Google Patents
Full-angle multi-load matched modular aerial photography unmanned aerial vehicle Download PDFInfo
- Publication number
- CN215399373U CN215399373U CN202121468818.8U CN202121468818U CN215399373U CN 215399373 U CN215399373 U CN 215399373U CN 202121468818 U CN202121468818 U CN 202121468818U CN 215399373 U CN215399373 U CN 215399373U
- Authority
- CN
- China
- Prior art keywords
- angle
- full
- fuselage
- aerial vehicle
- power
- 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.)
- Active
Links
- 210000001503 joint Anatomy 0.000 claims description 3
- 230000009286 beneficial effect Effects 0.000 abstract description 2
- 238000005457 optimization Methods 0.000 description 5
- 230000000694 effects Effects 0.000 description 1
Images
Landscapes
- Accessories Of Cameras (AREA)
Abstract
The utility model discloses an all-angle multi-load-matched modular aerial photography unmanned aerial vehicle which comprises an aerial vehicle body, an all-angle pan-tilt and a pan-tilt camera, wherein the aerial vehicle body is divided into a power body and a fixed body, the power body is divided into a left wing frame and a right wing frame which are symmetrical, each wing frame is connected with an independent power supply battery, the power body is movably connected with the fixed body, the all-angle pan-tilt is connected with the fixed body, an annular pitching shaft is arranged on the all-angle pan-tilt, and the fixed body is located at the annular center of the pitching shaft. The utility model has the beneficial effects that: this device passes through the whole combination of unmanned vehicles and cloud platform, lets the every single move direction of cloud platform can 360 rotations to at a flight machine position of hovering, shoot the picture of all angles, through modular package assembly, make the camera freely selectable, power can freely arrange in pairs, increases the convenience, is applicable to multiple trade and uses.
Description
Technical Field
The utility model relates to an unmanned aerial vehicle, in particular to a modular aerial photographing unmanned aerial vehicle with all-angle multi-load matching, and belongs to the technical field of industrial application type unmanned aerial vehicles.
Background
The existing aerial photography unmanned aerial vehicle is small in shot picture range, only pictures of the front, the back, the left, the right and the lower parts of the aerial vehicle can be shot, pictures on the aerial vehicle cannot be shot, in some professional purposes, the pictures on the aerial vehicle cannot be shot, and the effect of the aerial vehicle cannot be maximized.
SUMMERY OF THE UTILITY MODEL
The utility model aims to solve the problems and provide a modular aerial photography unmanned aerial vehicle with full-angle multi-load matching.
The utility model realizes the purpose through the following technical scheme, and the modularized aerial photography unmanned aerial vehicle with full angle and multiple loads matched comprises an aircraft body, a full angle pan-tilt and a pan-tilt camera, wherein the aircraft body is divided into a power body and a fixed body, the power body is divided into a left wing frame and a right wing frame which are symmetrical, each wing frame is connected with an independent power supply battery, the power body is movably connected with the fixed body, the full angle pan-tilt is connected with the fixed body, an annular pitching shaft is arranged on the full angle pan-tilt, the fixed body is positioned at the annular center of the pitching shaft, and the pan-tilt camera is arranged on the pitching shaft.
As a technical optimization scheme of the utility model, the rotation angle of the pitch axis is 360 degrees, and the holder camera is positioned on the rotation joint of the pitch axis and rotates along with the pitch axis.
As a technical optimization scheme of the utility model, the holder camera is of a detachable structure, and is in butt joint with the pitching shaft through a modular assembly interface.
As a technical optimization scheme of the utility model, the fixed machine body is internally provided with the flight controller, and the edge of the fixed machine body is provided with the machine body connecting module.
As a technical optimization scheme of the utility model, the power machine body is provided with a connecting joint matched with the machine body connecting module and is movably connected with the fixed machine body through the matching of the connecting joint and the machine body connecting module.
As a technical optimization scheme of the utility model, the bottom of the full-angle pan-tilt is provided with a plurality of racks, and the pan-tilt camera structure is protected by the racks.
The utility model has the beneficial effects that: this device passes through the whole combination of unmanned vehicles and cloud platform, lets the every single move direction of cloud platform can 360 rotations to at a flight machine position of hovering, shoot the picture of all angles, through modular package assembly, make the camera freely selectable, power can freely arrange in pairs, increases the convenience, is applicable to multiple trade and uses.
Drawings
FIG. 1 is a schematic view of the overall structure of the present invention;
fig. 2 is a top view of the pitch axis of the present invention.
In the figure: 1. the device comprises a power machine body, 2 a fixed machine body, 3 a rack, 4 a full-angle tripod head, 5 a pitching shaft, 6 a tripod head camera, 7 and a machine body connecting module.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
Example 1
Referring to fig. 1-2, an all-angle multi-load-matching modular aerial photography unmanned aerial vehicle comprises an aircraft body, an all-angle pan-tilt 4 and a pan-tilt camera 6, wherein the aircraft body is divided into a power aircraft body 1 and a fixed aircraft body 2, the power aircraft body 1 is divided into a left wing frame and a right wing frame which are symmetrical, each wing frame is connected with an independent power supply battery, the power aircraft body 1 is movably connected with the fixed aircraft body 2, the all-angle pan-tilt 4 is connected with the fixed aircraft body 2, an annular pitch shaft 5 is arranged on the all-angle pan-tilt 4, the fixed aircraft body 2 is located at the annular center of the pitch shaft 5, and the pan-tilt camera 6 is arranged on the pitch shaft 5; the rotation angle of the pitching shaft 5 is 360 degrees, and the holder camera 6 is positioned on the rotation joint of the pitching shaft 5 and rotates along with the pitching shaft 5; the pan-tilt camera 6 is of a detachable structure and is in butt joint with the pitching shaft 5 through a modular assembly interface; the fixed machine body 2 is internally provided with a flight controller, and the edge of the fixed machine body is provided with a machine body connecting module 7; the power machine body 1 is provided with a connecting joint matched with the machine body connecting module 7, and is movably connected with the fixed machine body 2 in a matched mode through the connecting joint and the machine body connecting module 7, and the bottom of the full-angle holder 4 is provided with a plurality of racks 3.
When the multifunctional power aircraft is used, firstly, the left and right power airframes 1 are respectively connected with a battery, namely the left and right sides of the aircraft independently meet the power and power supply batteries, when in transportation, the power airframes 1 on the left and right sides of the aircraft are independently disassembled to increase the portability, and motors with different powers can be grouped and matched with the same battery, so that when different load requirements are met, different power airframes 1 are selected in a modularized mode, the three-axis full-angle pan-tilt 4 is used for controlling the shooting angle of the pan-tilt camera 6, the pitching shaft 5 adopts an annular power form, the fixed airframe 2 is arranged in the middle of the ring, and the flight controller is installed at the position; the power fuselage 1 is butted on the fixed fuselage 2 through the fuselage connection module 7, the aircraft can fly, the pitching shaft 5 adopts a large ring shape and surrounds the fuselage, so 360-degree shooting can be realized, and the full-angle shooting of the aircraft can be realized through the rotation of the aircraft.
It will be evident to those skilled in the art that the utility model is not limited to the details of the foregoing illustrative embodiments, and that the present invention may be embodied in other specific forms without departing from the spirit or essential attributes thereof. The present embodiments are therefore to be considered in all respects as illustrative and not restrictive, the scope of the utility model being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein. Any reference sign in a claim should not be construed as limiting the claim concerned.
Furthermore, it should be understood that although the present description refers to embodiments, not every embodiment may contain only a single embodiment, and such description is for clarity only, and those skilled in the art should integrate the description, and the embodiments may be combined as appropriate to form other embodiments understood by those skilled in the art.
Claims (6)
1. The utility model provides a many load of full angle collocation modularization unmanned vehicles that takes photo by plane, includes aircraft fuselage, full angle cloud platform (4) and cloud platform camera (6), its characterized in that: the aircraft fuselage divide into power fuselage (1) and fixed fuselage (2), power fuselage (1) is the wing frame of two left and right symmetries, and each wing frame is connected with independent power supply battery respectively, power fuselage (1) with swing joint between fixed fuselage (2), full angle cloud platform (4) are connected with fixed fuselage (2), be provided with annular pitch axis (5) on full angle cloud platform (4), fixed fuselage (2) are located the annular center department of pitch axis (5), cloud platform camera (6) set up on pitch axis (5).
2. The full-angle multi-load-capacity collocated modular aerial unmanned aerial vehicle of claim 1, wherein: the rotation angle of the pitch axis (5) is 360 degrees, and the holder camera (6) is positioned on the rotation joint of the pitch axis (5) and rotates along with the pitch axis (5).
3. The full-angle multi-load-capacity collocated modular aerial unmanned aerial vehicle of claim 2, wherein: the holder camera (6) is of a detachable structure, and is in butt joint with the pitching shaft (5) through a modular assembly interface.
4. The full-angle multi-load-capacity collocated modular aerial unmanned aerial vehicle of claim 3, wherein: the fixed fuselage (2) internally mounted has the flight controller, and the edge of fixed fuselage is provided with fuselage connection module (7).
5. The full-angle multi-load-capacity collocated modular aerial unmanned aerial vehicle of claim 4, wherein: the power machine body (1) is provided with a connecting joint matched with the machine body connecting module (7) and is movably connected with the fixed machine body (2) through the matching of the connecting joint and the machine body connecting module (7).
6. The full-angle multi-load-capacity collocated modular aerial unmanned aerial vehicle of claim 4, wherein: the bottom of the full-angle holder (4) is provided with a plurality of racks (3).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121468818.8U CN215399373U (en) | 2021-06-30 | 2021-06-30 | Full-angle multi-load matched modular aerial photography unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121468818.8U CN215399373U (en) | 2021-06-30 | 2021-06-30 | Full-angle multi-load matched modular aerial photography unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN215399373U true CN215399373U (en) | 2022-01-04 |
Family
ID=79643325
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202121468818.8U Active CN215399373U (en) | 2021-06-30 | 2021-06-30 | Full-angle multi-load matched modular aerial photography unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN215399373U (en) |
-
2021
- 2021-06-30 CN CN202121468818.8U patent/CN215399373U/en active Active
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN207366911U (en) | A kind of reflective twin-lens bi-axial tilt camera for aircraft | |
| US11155344B2 (en) | Load assembly and unmanned aerial vehicle | |
| CN104580606B (en) | A kind of mobile phone shell that can be changed into unmanned plane | |
| CN210391577U (en) | Small-size two optical nacelle of triaxial | |
| EP3303124A1 (en) | Electric aircraft and power supply device | |
| CN205661673U (en) | 360 degrees carry mechanisms that take photo by plane of unmanned aerial vehicle | |
| WO2019084818A1 (en) | Flight control method and device for multi-rotor unmanned aerial vehicle, and multi-rotor unmanned aerial vehicle | |
| CN206012982U (en) | A kind of small-sized electric fixed-wing unmanned plane for oblique photograph | |
| WO2021190216A1 (en) | Unmanned aerial vehicle capable of panoramic image capture | |
| CN106347693A (en) | Replaceable unmanned aerial vehicle miniature pod | |
| CN105346709A (en) | Multi-rotor craft capable of transforming combination | |
| CN205396569U (en) | Unmanned vehicles with battery formula counter weight device | |
| CN215399373U (en) | Full-angle multi-load matched modular aerial photography unmanned aerial vehicle | |
| CN207985196U (en) | A kind of unmanned plane of taking photo by plane convenient for adjusting camera | |
| CN207631492U (en) | Unmanned vehicle | |
| CN105775152A (en) | Unmanned aerial vehicle with battery type counterweight device and counterweight method thereof | |
| CN206485583U (en) | A kind of unmanned plane oblique photograph head | |
| CN206171830U (en) | Aircraft and system of taking photo by plane | |
| CN210000581U (en) | physical combined unmanned aerial vehicle cluster | |
| CN217416130U (en) | Camera and unmanned aerial vehicle | |
| CN207631491U (en) | Unmanned vehicle | |
| CN207826552U (en) | A kind of portable V R panorama aerial photography unmanned aerial vehicles | |
| CN208530844U (en) | Modularization can tiltrotor aircraft | |
| CN109050951A (en) | A kind of unmanned plane taken photo by plane suitable for 3D | |
| CN211494498U (en) | Unmanned vehicles carries diaxon cloud platform and contains its unmanned vehicles |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20230320 Address after: 710000 Room 208, Block B, Qinhan Innovation Center, Yaodian Sub District Office, Qinhan New City, Xixian New District, Xi'an City, Shaanxi Province Patentee after: Xi'an Beiteng Aviation Technology Co.,Ltd. Address before: 715300 No.11 Houwan lane, Xinchi Town, Xinchi village, Heyang County, Weinan City, Shaanxi Province Patentee before: Che Xin |
|
| TR01 | Transfer of patent right |