CN211592942U

CN211592942U - Be used for photographic unmanned aerial vehicle

Info

Publication number: CN211592942U
Application number: CN201922407001.9U
Authority: CN
Inventors: 铃木一史
Original assignee: Shenzhen Infinite Sky Technology Co ltd
Current assignee: Shenzhen Infinite Sky Technology Co ltd
Priority date: 2019-12-27
Filing date: 2019-12-27
Publication date: 2020-09-29
Anticipated expiration: 2029-12-27

Abstract

The utility model relates to an unmanned aerial vehicle photography technique field discloses an unmanned aerial vehicle for it is photographic, include: 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

Be used for photographic unmanned aerial vehicle

Technical Field

The utility model relates to an unmanned aerial vehicle photography technique field especially relates to an unmanned aerial vehicle for it is photographic.

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.

SUMMERY OF THE UTILITY MODEL

The to-be-solved technical problem of the utility model lies in how to provide an unmanned aerial vehicle for photography.

For this reason, according to the first aspect, the embodiment of the utility model discloses an unmanned aerial vehicle for photography, include: 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 utility model discloses further set up to, damping device includes: 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 utility model discloses further set up to, the quantity of attenuator sets up to six, and symmetric distribution in the one end terminal surface of photographic seat.

The utility model discloses further set up as, the attenuator includes: 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 utility model discloses further set up to, landing gear includes: 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 utility model discloses further set up to, the both ends of horizontal pole are equipped with and make things convenient for the staff to grip the cover that grips of horizontal pole.

The utility model discloses further set up to, grip the cover cup joint in the lateral wall of horizontal pole.

The utility model discloses further set up to, first driving motor with second driving motor is servo motor.

The utility model discloses following beneficial effect has: 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 embodiments or the technical solutions in 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 for those skilled in the art, other drawings can be obtained according to these drawings 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 clearly understood, the present invention is further described in 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 is to be noted that, unless otherwise explicitly specified or limited, the terms "mounted," "connected," and "connected" are to be construed broadly, and may be, for example, fixedly connected, detachably connected, or integrally connected; 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 meaning 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", and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are only for convenience of description and simplification of description, but do not indicate or imply that the device or element referred to must have a specific orientation, be constructed and operated in a specific 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.

Furthermore, the technical features mentioned in the different embodiments of the invention described below can be combined with each other as long as they do not conflict with each other.

The embodiment of the utility model discloses an unmanned aerial vehicle for it is photographic, as shown in figure 1, include: 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 can be made without departing from the scope of the invention.

Claims

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.