Aircraft airborne shooting support

Abstract

The utility model discloses an airborne shooting support, and belongs to the technical field of aerial photography. The device mainly comprises a base; the adjusting bracket is mounted on one side of the base, and the adjusting bracket is provided with a fixed seat; the cleaning mechanism is installed on the fixed seat, the cleaning mechanism is provided with a sliding plate, the cleaning mechanism further comprises a sweeping assembly, the sweeping assembly is installed on the sliding plate, the sweeping assembly comprises an air pump, and the air pump is installed on the sliding plate; the output pipe is mounted at the output end of the air pump; the temporary storage chamber is mounted at the output end of the output pipe; and the high-pressure spray head is mounted at the other end of the temporary storage chamber. According to the airborne shooting support of the airplane, the sweeping assembly is arranged, so that the effect of sweeping the camera is achieved.

Description

Technical Field

[0001] This application relates to the field of aerial photography technology, specifically to an aircraft-mounted photography rig. Background Technology

[0002] A fixed-wing aircraft is a heavier-than-air aircraft that flies within the atmosphere by using a power plant to generate forward thrust or pull and fixed wings on the fuselage to generate lift.

[0003] Fixed-wing aircraft, as a filming platform, have the advantages of high-altitude flight, high speed, and wide coverage. These characteristics enable fixed-wing aircraft to capture unique perspectives and broad fields of vision during filming, providing high-quality materials for film and television works, advertisements, news reports, and more.

[0004] In order to maintain stability, flexibility and adaptability, airborne supports are installed on fixed-wing aircraft to support the stable shooting of photography or video equipment.

[0005] For example, the patent with publication number CN201961532U discloses a vibration damping bracket for aerial cameras. This patent can achieve buffering and vibration damping in both vertical and horizontal directions through a set of springs. It has a simple structure, low cost, and is easy to install and maintain.

[0006] During actual filming, when the aircraft is flying at high altitude and shooting downwards, it may encounter various harsh environments, such as salt spray, dust, and rain. These pollutants may contaminate the lens, thereby affecting the shooting quality.

[0007] Therefore, it is necessary to provide an aircraft-mounted shooting rig to solve the above problems.

[0008] It should be noted that the information disclosed in this background section is only for understanding the background technology of this application concept, and therefore may include information that does not constitute prior art. Summary of the Invention

[0009] Based on the aforementioned problems in the existing technology, the problem to be solved by this application is to provide an aircraft-mounted shooting bracket, which solves the problem that pollutants cause contamination to the lens when the aircraft is flying at high altitude, thereby affecting the shooting quality.

[0010] The technical solution adopted by this application to solve its technical problem is: an aircraft-mounted photography bracket, comprising:

[0011] Base;

[0012] An adjustment bracket is mounted on one side of the base and is used to adjust the shooting angle. The adjustment bracket has a fixed base.

[0013] A cleaning mechanism, mounted on the fixed base, is used for cleaning the lens. The cleaning mechanism includes a sliding plate and further comprises:

[0014] A cleaning assembly, mounted on the sliding plate, includes:

[0015] An air pump, which is mounted on the sliding plate;

[0016] An output pipe is installed at the output end of the air pump;

[0017] A temporary storage chamber is installed at the output end of the output pipe;

[0018] A high-pressure nozzle is installed at the other end of the temporary storage chamber.

[0019] Furthermore, the high-pressure nozzle is arranged in a circumferential manner around the temporary storage chamber.

[0020] Furthermore, a first motor is fixedly installed on one side of the base, and the output end of the first motor is fixedly connected to a support base through the base. An L-shaped mounting plate is fixedly installed on the other end of the support base.

[0021] A second motor is fixedly installed on one side of the L-shaped mounting plate, and the output end of the second motor is fixedly installed on the mounting plate. The mounting plate is fixedly connected to the fixed base.

[0022] Furthermore, a camera is installed on the mounting base.

[0023] Furthermore, a fixing frame is fixedly provided at one end of the fixing base, a mounting base is fixedly provided on the fixing frame, a rotating shaft is rotatably provided between the mounting bases, a third motor is fixedly provided on one side of the mounting base, and the output end of the third motor is fixedly connected to the rotating shaft.

[0024] A mounting bracket is fixedly mounted on the rotating shaft. A slide rail is fixedly mounted on one side of the mounting bracket. A slider is slidably mounted on the slide rail. The slider is fixedly connected to the sliding plate. A crossbeam is fixedly mounted between the mounting brackets. A cylinder is fixedly mounted on the crossbeam. The output end of the cylinder is fixedly connected to the sliding plate.

[0025] The beneficial effects of this application are: the aircraft-mounted camera mounting bracket provided by this application achieves the effect of cleaning the camera by setting up a cleaning component.

[0026] In addition to the purposes, features, and advantages described above, this application has other purposes, features, and advantages. A further detailed description of this application will be provided below with reference to the figures. Attached Figure Description

[0027] The accompanying drawings, which form part of this application, are used to provide a further understanding of this application. The illustrative embodiments of this application and their descriptions are used to explain this application and do not constitute an undue limitation of this application.

[0028] In the attached diagram:

[0029] Figure 1 This is an overall schematic diagram of an aircraft-mounted camera mounting bracket according to this application;

[0030] Figure 2 for Figure 1 Exploded view of the adjustment bracket;

[0031] Figure 3 for Figure 1 A schematic diagram of the central cleaning agency;

[0032] Figure 4 for Figure 1 A cross-sectional schematic diagram of the cleaning mechanism;

[0033] Figure 5 for Figure 4 A schematic diagram of the cleaning component;

[0034] The following are the labeling elements in the figure:

[0035] 1. Base; 2. Adjustment bracket; 20. First motor; 21. Support base; 22. L-shaped mounting plate; 23. Second motor; 24. Mounting plate; 25. Fixed base; 3. Camera; 4. Cleaning mechanism; 40. Fixed frame; 41. Mounting base; 42. Rotating shaft; 43. Third motor; 44. Mounting frame; 45. Crossbeam; 46. Cylinder; 47. Slide rail; 48. Slider; 49. Sliding plate; 5. Cleaning assembly; 50. Air pump; 51. Output pipe; 52. High-pressure nozzle; 53. Temporary storage chamber. Detailed Implementation

[0036] It should be noted that, unless otherwise specified, the embodiments and features described in this application can be combined with each other. This application will now be described in detail with reference to the accompanying drawings and embodiments.

[0037] To enable those skilled in the art to better understand the present application, the technical solutions in the embodiments of the present application will be clearly and completely described below with reference to the accompanying drawings. Obviously, the described embodiments are only some embodiments of the present application, and not all embodiments. Based on the embodiments in the present application, all other embodiments obtained by those of ordinary skill in the art without creative effort should fall within the scope of protection of the present application.

[0038] like Figures 1-2 As shown, this application provides an aircraft-mounted shooting bracket, including a base 1. The base 1 is used to connect to a fixed-wing aircraft via an external connector so that it can be used to shoot downwards smoothly during flight. In order to adjust the angle according to the actual situation when shooting downwards, an adjustment bracket 2 is provided on one side of the base 1. The adjustment bracket 2 includes a first motor 20 fixedly installed on one side of the base 1. The output end of the first motor 20 passes through the base 1 and is fixedly connected to a support 21. An L-shaped mounting plate 22 is fixedly installed on the other end of the support 21. Thus, starting the first motor 20 can drive the L-shaped mounting plate 22 to rotate on the upper end of the base 1.

[0039] Meanwhile, a second motor 23 is fixedly installed on one side of the L-shaped mounting plate 22. The output end of the second motor 23 is fixedly installed on the mounting plate 24, and a fixed seat 25 is fixedly installed on the other side of the mounting plate 24. Thus, starting the second motor 23 can drive the fixed seat 25 to rotate on the L-shaped mounting plate 22.

[0040] Furthermore, a camera 3 is installed on the fixed base 25. The camera 3 is used to complete the shooting operation. When it is necessary to adjust the angle according to the shooting needs, it is only necessary to start the first motor 20 to drive the L-shaped mounting plate 22 to rotate. After the adjustment is completed, the second motor 23 can be started to drive the camera 3 to rotate through the fixed base 25, thereby achieving the purpose of adjusting the angle of the camera 3.

[0041] like Figure 1 and Figures 3-5 As shown, in order to prevent the camera 3 from being contaminated by pollutants during the shooting operation, thereby affecting the shooting quality, a cleaning mechanism 4 is provided on the mounting base 25. The cleaning mechanism 4 is used to clean the camera 3 when it is contaminated.

[0042] The cleaning mechanism 4 includes a fixed frame 40 fixedly installed at one end of the fixed base 25, a mounting base 41 fixedly installed on the fixed frame 40, a rotating shaft 42 rotatably installed between the mounting bases 41, and a third motor 43 fixedly installed on one side of the mounting base 41. The output end of the third motor 43 is fixedly connected to the rotating shaft 42, so that starting the third motor 43 can drive the rotating shaft 42 to rotate between the mounting bases 41.

[0043] Meanwhile, a mounting bracket 44 is fixedly installed on the rotating shaft 42. A slide rail 47 is fixedly installed on one side of the mounting bracket 44, and a slider 48 is slidably installed on the slide rail 47. A sliding plate 49 is fixedly installed on the slider 48, and a crossbeam 45 is fixedly installed between the mounting brackets 44. A cylinder 46 is fixedly installed on the crossbeam 45, and the output end of the cylinder 46 is fixedly connected to the sliding plate 49. Thus, starting the cylinder 46 can push the sliding plate 49 to slide along the slide rail 47.

[0044] In order to clean the camera 3 smoothly, a cleaning component 5 is provided on the sliding plate 49. The cleaning component 5 includes an air pump 50 fixedly installed on one side of the sliding plate 49. An output pipe 51 is fixedly installed at the output end of the air pump 50. A temporary storage chamber 53 is fixedly connected to the output end of the output pipe 51 through the sliding plate 49. At the same time, a high-pressure nozzle 52 is fixedly installed at the other end of the temporary storage chamber 53. The high-pressure nozzle 52 is arranged in a circle around the temporary storage chamber 53 so that the area around the camera 3 can be cleaned in the future.

[0045] When it is necessary to clean the camera 3, the third motor 43 can be started to drive the mounting bracket 44 to rotate through the rotating shaft 42 until it rotates to the appropriate position. Then, the cylinder 46 is started to drive the high-pressure nozzle 52 to move closer to the camera 3 through the sliding plate 49 until it moves to the appropriate position. Then, the air pump 50 is started to pump the gas into the temporary storage chamber 53 through the output pipe 51. Finally, the high-pressure nozzle 52 sprays the gas onto the camera 3, thereby achieving the purpose of cleaning the surface of the camera 3.

[0046] The above description is merely a preferred embodiment of this application and is not intended to limit this application. Various modifications and variations can be made to this application by those skilled in the art. Any modifications, equivalent substitutions, improvements, etc., made within the spirit and principles of this application should be included within the protection scope of this application.

Claims

1. An aircraft onboard camera mount, characterized by: Include: Base (1); Adjustment bracket (2) is installed on one side of the base (1), the adjustment bracket (2) is used for adjusting the shooting angle, the adjustment bracket (2) has a fixed seat (25); Cleaning mechanism (4) is installed on the fixed seat (25), the cleaning mechanism (4) is used for cleaning the lens, the cleaning mechanism (4) has a sliding plate (49), the cleaning mechanism (4) further comprises: Sweeping assembly (5) is installed on the sliding plate (49), the sweeping assembly (5) comprises: Air pump (50) is installed on the sliding plate (49); Output pipe (51) is installed at the output end of the air pump (50); Temporary storage chamber (53) is installed at the output end of the output pipe (51); High pressure spray head (52) is installed at the other end of the temporary storage chamber (53).

2. The aircraft onboard camera mount of claim 1, wherein: The high pressure spray head (52) is circumferentially arranged around the temporary storage chamber (53).

3. The aircraft onboard camera mount of claim 1, wherein: The base (1) is fixedly provided with a first motor (20) on one side, the output end of the first motor (20) is fixedly connected with a support seat (21) penetrating the base (1), the other end of the support seat (21) is fixedly provided with an L-shaped mounting plate (22); The L-shaped mounting plate (22) is fixedly provided with a second motor (23) on one side, the output end of the second motor (23) is fixedly provided with a mounting plate (24), and the mounting plate (24) is fixedly connected with the fixed seat (25).

4. The aircraft onboard camera mount of claim 1, wherein: The fixed seat (25) is provided with a camera (3).

5. The aircraft onboard camera mount of claim 1, wherein: The fixed seat (25) is fixedly provided with a fixed frame (40) at one end, the fixed frame (40) is fixedly provided with a mounting seat (41), the mounting seat (41) is rotatably provided with a rotating shaft (42), the mounting seat (41) is fixedly provided with a third motor (43) on one side, and the output end of the third motor (43) is fixedly connected with the rotating shaft (42); The rotating shaft (42) is fixedly provided with a mounting frame (44), the mounting frame (44) is fixedly provided with a sliding rail (47) on one side, the sliding rail (47) is slidably provided with a sliding block (48), the sliding block (48) is fixedly connected with the sliding plate (49), the mounting frame (44) is fixedly provided with a cross beam (45) between the mounting frame (44), the cross beam (45) is fixedly provided with an air cylinder (46), and the output end of the air cylinder (46) is fixedly connected with the sliding plate (49).

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