CN110979679A - Be used for photographic unmanned aerial vehicle - Google Patents
Be used for photographic unmanned aerial vehicle Download PDFInfo
- Publication number
- CN110979679A CN110979679A CN201911379419.1A CN201911379419A CN110979679A CN 110979679 A CN110979679 A CN 110979679A CN 201911379419 A CN201911379419 A CN 201911379419A CN 110979679 A CN110979679 A CN 110979679A
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- Prior art keywords
- seat
- camera
- damping
- frame
- unmanned aerial
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- 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.)
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- 238000013016 damping Methods 0.000 claims abstract description 55
- 230000003139 buffering effect Effects 0.000 claims description 3
- 230000000694 effects Effects 0.000 abstract description 4
- 238000000034 method Methods 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000000903 blocking effect Effects 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000004880 explosion Methods 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000011084 recovery Methods 0.000 description 1
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
- B64D47/08—Arrangements of cameras
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F15/00—Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion
- F16F15/02—Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems
- F16F15/04—Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems using elastic means
- F16F15/06—Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems using elastic means with metal springs
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Acoustics & Sound (AREA)
- Mechanical Engineering (AREA)
- Accessories Of Cameras (AREA)
Abstract
The invention relates to the technical field of unmanned aerial vehicle photography, and discloses an unmanned aerial vehicle for photography, which comprises: the camera seat is of a frame structure and is used for mounting a camera; the mounting frames are symmetrically arranged on the photographic seat and are used for mounting external power devices which are convenient to drive the photographic seat to fly; the damping device is arranged at one end of the photography seat and is used for damping the flight of the photography seat; and the lifting devices are symmetrically arranged at one end of the photographic seat opposite to the damping device and are used for supporting the photographic seat and facilitating the shooting of the camera. The external power device provides flying power to drive the camera seat to fly, so that the camera can shoot in the air, the damping device has a damping effect, the camera at the bottom of the camera seat can be conveniently damped, and the stability of shooting is improved; the camera seat is convenient to adjust through the lifting device, and shooting of the camera is facilitated.
Description
Technical Field
The invention relates to the technical field of unmanned aerial vehicle photography, in particular to an unmanned aerial vehicle for photography.
Background
A drone is an unmanned aircraft that is operated by a radio remote control device and a self-contained program control device. The machine has no cockpit, but is provided with an automatic pilot, a program control device and other equipment. The personnel on the ground, the naval vessel or the mother aircraft remote control station can track, position, remotely control, telemeter and digitally transmit the personnel through equipment such as a radar. The aircraft can take off like a common airplane under the radio remote control or launch and lift off by a boosting rocket, and can also be thrown into the air by a mother aircraft for flying. During recovery, the aircraft can automatically land in the same way as a common aircraft landing process, and can also be recovered by a remote control parachute or a blocking net, so that the aircraft can be repeatedly used. Unmanned aerial vehicles are widely used for aerial reconnaissance, surveillance, communication, anti-dive, electronic interference and the like.
In the prior art, the unmanned aerial vehicles currently used for photography are usually small, and the maximum loading weight is usually 1-2 kg. The number of unmanned aerial vehicles equipped with large cameras for shooting movies and broadcasting is small, and the types of unmanned aerial vehicles are limited.
Therefore, how to provide an unmanned aerial vehicle for photography becomes an urgent technical problem to be solved.
Disclosure of Invention
The invention aims to provide an unmanned aerial vehicle for photography.
To this end, according to a first aspect, an embodiment of the present invention discloses an unmanned aerial vehicle for photography, including: the camera seat is of a frame structure and is used for mounting a camera; the mounting frames are symmetrically arranged on the photographic seat and are used for mounting external power devices which are convenient to drive the photographic seat to fly; the damping device is arranged at one end of the photography seat and is used for damping the flight of the photography seat; and the landing gear is symmetrically arranged at one end of the photographic seat opposite to the damping device and is used for supporting the photographic seat and facilitating the shooting of the camera.
The invention is further arranged such that the damping device comprises: the damper is arranged at one end of the camera seat and used for buffering the vibration of the camera seat so as to reduce the vibration of the camera; the damping frame is arranged at one end, opposite to the photographic seat, of the damper, fixedly connected with the damper and used for fastening the damper.
The invention is further provided that the number of the dampers is six, and the dampers are symmetrically distributed on one end face of the photographic seat.
The invention further provides that the damper comprises: the damping ring is positioned between the photographic seat and the damping frame; and the damping fixed blocks are symmetrically arranged at two opposite ends of the damping ring, are sleeved on the outer side of the damping ring and are used for fixing the damping ring on the photographic seat and the damping frame.
The invention further provides that the landing gear comprises: the first landing frame is of a frame structure and is arranged at one end, opposite to the damping device, of the camera seat; the second landing gear is of a frame structure and is arranged at one end of the photographic seat in parallel with the first landing gear; the first lifting rod is arranged on the first lifting frame and is rotationally connected with the first lifting frame; the second lifting rod is arranged on the second undercarriage and is in rotating connection with the second undercarriage; the cross rod is respectively sleeved with the first lifting rod and the second lifting rod; the first driving motor is arranged on the first falling frame, is fixedly connected with the first falling frame and is used for driving the first falling rod to rotate on the first falling frame so as to facilitate shooting of a camera; and the second driving motor is arranged on the second undercarriage, is fixedly connected with the second undercarriage, and is used for driving the second lifting rod to rotate on the second undercarriage so as to facilitate shooting of a camera.
The invention is further provided that two ends of the cross bar are provided with holding sleeves which are convenient for workers to hold the cross bar.
The invention is further provided that the grip sleeve is sleeved on the outer side wall of the cross bar.
The invention is further configured such that the first drive motor and the second drive motor are both servo motors.
The invention has the following beneficial effects: the external power device provides flying power to drive the camera seat to fly, so that the camera can shoot in the air, the damping device has a damping effect, the camera at the bottom of the camera seat can be conveniently damped, and the stability of shooting is improved; the camera seat is convenient to adjust through the lifting device, and shooting of the camera is facilitated.
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings used in the description of the embodiments or the prior art will be briefly described below, and it is obvious that the drawings in the following description are some embodiments of the present invention, and other drawings can be obtained by those skilled in the art without creative efforts.
Fig. 1 is a schematic perspective view of an unmanned aerial vehicle for photography according to the embodiment;
fig. 2 is an explosion structure diagram of the unmanned aerial vehicle for photography disclosed in the present embodiment.
Reference numerals: 1. a photographic seat; 2. a mounting frame; 3. a damping device; 31. a damper; 311. a damping ring; 312. a damping fixed block; 32. a damping frame; 4. a landing gear; 41. a first landing rack; 42. a second landing gear; 43. a first falling rod; 44. a second landing bar; 45. a cross bar; 46. a first drive motor; 47. a second drive motor; 5. and (4) a holding sleeve.
Detailed Description
In order to make the objects, technical solutions and advantages of the present invention more apparent, the present invention is described in further detail below with reference to the accompanying drawings and embodiments. It should be understood that the specific embodiments described herein are merely illustrative of the invention and are not intended to limit the invention.
In the description of the present invention, it should be noted that, unless otherwise explicitly specified or limited, the terms "mounted," "connected," and "connected" are to be construed broadly, e.g., as meaning either a fixed connection, a removable connection, or an integral connection; can be mechanically or electrically connected; the two elements may be directly connected or indirectly connected through an intermediate medium, or may be communicated with each other inside the two elements, or may be wirelessly connected or wired connected. The specific meanings of the above terms in the present invention can be understood in specific cases to those skilled in the art.
In the description of the present invention, it should be noted that the terms "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inner", "outer", etc., indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are only for convenience of description and simplicity of description, but do not indicate or imply that the device or element being referred to must have a particular orientation, be constructed and operated in a particular orientation, and thus, should not be construed as limiting the present invention. Furthermore, the terms "first," "second," and "third" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance.
In addition, the technical features involved in the different embodiments of the present invention described below may be combined with each other as long as they do not conflict with each other.
The embodiment of the invention discloses an unmanned aerial vehicle for photography, as shown in figure 1, comprising: photographic seat 1, mounting bracket 2, damping device 3 and landing gear 4, wherein: the camera seat 1 is of a frame structure, and the camera seat 1 is used for mounting a camera; the mounting frames 2 are symmetrically arranged on the photographic seat 1, and the mounting frames 2 are used for mounting external power devices which are convenient to drive the photographic seat 1 to fly; the damping device 3 is arranged at one end of the photography seat 1, and the damping device 3 is used for damping the flight of the photography seat 1; the landing gear 4 is symmetrically arranged at one end of the camera seat 1 opposite to the damping device 3, and the landing gear 4 is used for supporting the camera seat 1 and facilitating the shooting of a camera.
It should be noted that, the external power device provides flight power to drive the camera seat 1 to fly, so that the camera takes pictures in the air, and the damping device 3 plays a damping role, so as to conveniently damp the camera at the bottom of the camera seat 1 and improve the stability of shooting; the camera seat 1 is convenient to adjust through the lifting device 4, and therefore shooting of the camera is facilitated.
It should be further noted that the unmanned aerial vehicle for photography disclosed by the application is convenient for replacing different power devices and assembling and disassembling, and can select a required model according to the load weight of the motor, the electric regulator and the battery; applicable motors are about 3500W-10000W; the motor installation can select 35mm and 40 mm's pipeline, and the length can freely set up.
In the implementation process, the photographic seat 1 is provided with a folding device for folding the mounting frame 2. The folding device plays a role in folding and is convenient for folding the mounting frame 2.
As shown in fig. 1 and 2, the damper device 3 includes: a damper 31 and a damping frame 32, wherein the damper 31 is arranged at one end of the camera seat 1, and the damper 31 is used for buffering the vibration of the camera seat 1 so as to reduce the vibration of the camera; the damper frame 32 is provided at one end of the damper 31 with respect to the camera mount 1, the damper frame 32 is fixedly connected to the damper 31, and the damper frame 32 is used to fasten the damper 31. In a specific implementation, the damper 31 is a wire damper.
As shown in fig. 2, the number of the dampers 31 is six, and the dampers are symmetrically arranged on one end surface of the camera seat 1.
It should be noted that, the six dampers 31 are symmetrically distributed on an end face of the camera seat 1, so that vibration of the camera seat 1 can be effectively reduced, and a camera can conveniently shoot.
As shown in fig. 2, the damper 31 includes: a damping ring 311 located between the camera mount 1 and the damping frame 32; the damping fixing blocks 312 are symmetrically disposed at two opposite ends of the damping ring 311, and are sleeved outside the damping ring 311 to fix the damping ring 311 to the camera mount 1 and the damping frame 32.
As shown in fig. 1 and 2, the landing gear 4 includes: a first landing gear 41, a second landing gear 42, a first landing rod 43, a second landing rod 44, a cross bar 45, a first drive motor 46 and a second drive motor 47, wherein: the first landing frame 41 is a frame structure, and the first landing frame 41 is arranged at one end of the photography base 1 opposite to the damping device 3; the second undercarriage 42 is a frame structure, and the second undercarriage 42 and the first landing gear 41 are arranged at one end of the photography seat 1 in parallel; the first lifting rod 43 is arranged on the first lifting frame 41, and the first lifting rod 43 is rotatably connected with the first lifting frame 41; the second landing bar 44 is arranged on the second landing gear 42, and the second landing bar 44 is rotatably connected with the second landing gear 42; the cross bar 45 is respectively sleeved with the first lifting bar 43 and the second lifting bar 44; the first driving motor 46 is arranged on the first falling frame 41, the first driving motor 46 is fixedly connected with the first falling frame 41, and the first driving motor 46 is used for driving the first falling rod 43 to rotate on the first falling frame 41 so as to facilitate shooting of the camera; the second driving motor 47 is disposed on the second landing gear 42, the second driving motor 47 is fixedly connected to the second landing gear 42, and the second driving motor 47 is used for driving the second landing rod 44 to rotate on the second landing gear 42, so as to facilitate shooting by the camera.
It should be noted that the first landing bar 43 is driven by the first driving motor 46 to rotate on the first landing frame 41, the second landing bar 44 is driven by the second driving motor 47 to rotate on the second landing gear 42, so as to drive the cross bar 45 to rotate, and adjust the horizontal position of the camera seat 1, thereby facilitating the shooting of the camera.
As shown in fig. 2, the two ends of the cross bar 45 are provided with holding sleeves 5 for the worker to hold the cross bar 45.
As shown in fig. 2, the grip sheath 5 is sleeved on the outer side wall of the cross bar 45.
As shown in fig. 2, the first driving motor 46 and the second driving motor 47 are both servo motors.
The working principle is as follows: the external power device provides flying power to drive the camera seat 1 to fly, so that the camera can shoot in the air, the damping device 3 has a damping effect, and the damping effect of the damper 31 is realized, so that the camera at the bottom of the camera seat 1 can be conveniently damped, and the stability of shooting is improved; the first landing rod 43 is driven to rotate on the first landing frame 41 by the first driving motor 46, the second landing rod 44 is driven to rotate on the second landing frame 42 by the second driving motor 47, and then the cross rod 45 is driven to rotate, so that the horizontal position of the camera base 1 is adjusted, and shooting by the camera is facilitated.
It should be understood that the above examples are only for clarity of illustration and are not intended to limit the embodiments. Other variations and modifications will be apparent to persons skilled in the art in light of the above description. And are neither required nor exhaustive of all embodiments. And obvious variations or modifications therefrom are within the scope of the invention.
Claims (8)
1. A unmanned aerial vehicle for photography, comprising:
a camera mount (1) having a frame structure for mounting a camera;
the mounting frames (2) are symmetrically arranged on the photographic seat (1) and are used for mounting external power devices which are convenient to drive the photographic seat (1) to fly;
the damping device (3) is arranged at one end of the photographing seat (1) and is used for damping the flight of the photographing seat (1);
and the lifting devices (4) are symmetrically arranged at one end of the photographic seat (1) relative to the damping device (3) and are used for supporting the photographic seat (1) and facilitating shooting of a camera.
2. Unmanned aerial vehicle for photography according to claim 1, characterized in that the damping device (3) comprises:
the damper (31) is arranged at one end of the camera seat (1) and is used for buffering the vibration of the camera seat (1) so as to reduce the vibration of the camera;
and the damping frame (32) is arranged at one end of the damper (31) relative to the photographic seat (1), is fixedly connected with the damper (31), and is used for fastening the damper (31).
3. Unmanned aerial vehicle for photography according to claim 2, wherein the number of dampers (31) is set to six and symmetrically distributed on one end face of the photography seat (1).
4. Unmanned aerial vehicle for photography according to claim 2 or 3, characterized in that the damper (31) comprises:
a damping ring (311) located between the camera mount (1) and the damping frame (32);
and the damping fixed blocks (312) are symmetrically arranged at two opposite ends of the damping ring (311), are sleeved on the outer side of the damping ring (311), and are used for fixing the damping ring (311) on the photographic seat (1) and the damping frame (32).
5. Unmanned aerial vehicle for photography according to claim 1, characterized in that the landing gear (4) comprises:
a first landing frame (41) having a frame structure and provided at one end of the photographic seat (1) opposite to the damper device (3);
a second undercarriage (42) having a frame structure, and disposed at one end of the camera mount (1) in parallel with the first undercarriage (41);
a first lifting rod (43) arranged on the first lifting frame (41) and rotationally connected with the first lifting frame (41);
a second landing gear (42) rotatably connected to the second landing gear (44);
a cross bar (45) which is sleeved with the first lifting bar (43) and the second lifting bar (44) respectively;
the first driving motor (46) is arranged on the first falling frame (41), is fixedly connected with the first falling frame (41), and is used for driving the first falling rod (43) to rotate on the first falling frame (41) so as to facilitate shooting of a camera;
and the second driving motor (47) is arranged on the second landing gear (42), is fixedly connected with the second landing gear (42), and is used for driving the second lifting rod (44) to rotate on the second landing gear (42) so as to be convenient for shooting by a camera.
6. Unmanned aerial vehicle for photography according to claim 5, wherein both ends of the crossbar (45) are provided with a grip sleeve (5) for facilitating a worker to grip the crossbar (45).
7. Unmanned aerial vehicle for photography according to claim 6, wherein the grip sleeve (5) is sleeved on the outer side wall of the crossbar (45).
8. Unmanned aerial vehicle for photography according to claim 5, wherein the first drive motor (46) and the second drive motor (47) are both servo motors.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201911379419.1A CN110979679A (en) | 2019-12-27 | 2019-12-27 | Be used for photographic unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201911379419.1A CN110979679A (en) | 2019-12-27 | 2019-12-27 | Be used for photographic unmanned aerial vehicle |
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| Publication Number | Publication Date |
|---|---|
| CN110979679A true CN110979679A (en) | 2020-04-10 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201911379419.1A Pending CN110979679A (en) | 2019-12-27 | 2019-12-27 | Be used for photographic unmanned aerial vehicle |
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Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN206243457U (en) * | 2016-12-02 | 2017-06-13 | 深圳市九天创新科技有限责任公司 | A kind of automatic deploying and retracting landing gear structure for multi-rotor unmanned aerial vehicle |
| CN206265292U (en) * | 2016-11-18 | 2017-06-20 | 捷西迪（广州）光学科技有限公司 | A kind of unmanned aerial vehicle with retractable landing gear device |
| CN206420477U (en) * | 2016-12-02 | 2017-08-18 | 深圳市九天创新科技有限责任公司 | The oblique photograph system that five cameras are constituted according to special angle |
| CN206511113U (en) * | 2016-11-28 | 2017-09-22 | 昆明理工大学 | A kind of multi-rotor unmanned aerial vehicle damping undercarriage |
| CN211592942U (en) * | 2019-12-27 | 2020-09-29 | 深圳市无限天空科技有限公司 | Be used for photographic unmanned aerial vehicle |
-
2019
- 2019-12-27 CN CN201911379419.1A patent/CN110979679A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN206265292U (en) * | 2016-11-18 | 2017-06-20 | 捷西迪（广州）光学科技有限公司 | A kind of unmanned aerial vehicle with retractable landing gear device |
| CN206511113U (en) * | 2016-11-28 | 2017-09-22 | 昆明理工大学 | A kind of multi-rotor unmanned aerial vehicle damping undercarriage |
| CN206243457U (en) * | 2016-12-02 | 2017-06-13 | 深圳市九天创新科技有限责任公司 | A kind of automatic deploying and retracting landing gear structure for multi-rotor unmanned aerial vehicle |
| CN206420477U (en) * | 2016-12-02 | 2017-08-18 | 深圳市九天创新科技有限责任公司 | The oblique photograph system that five cameras are constituted according to special angle |
| CN211592942U (en) * | 2019-12-27 | 2020-09-29 | 深圳市无限天空科技有限公司 | Be used for photographic unmanned aerial vehicle |
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