Data acquisition unmanned aerial vehicle for topographic survey

Abstract

The data acquisition unmanned aerial vehicle comprises a vehicle body assembly, a protection assembly is arranged on one side of the vehicle body assembly, the protection assembly is detachably connected to the vehicle body assembly, a reconnaissance assembly is arranged on one side of the vehicle body assembly, the reconnaissance assembly is installed and connected in the vehicle body assembly, and supporting assemblies are arranged on the two sides of the reconnaissance assembly. One side of the supporting assembly is fixedly connected to the machine body assembly, wings and a machine body can be protected through the protection assembly, the lifting work of the wings cannot be affected through the open type design, the temperature of a current road section can be detected through the temperature detection piece, and the exploration camera can be controlled through the air cylinder to enter the base for protection.

Description

Technical Field

[0001] The invention relates to an unmanned aerial vehicle, in particular to an unmanned aerial vehicle for data collection for terrain survey. Background Art

[0002] Unmanned aircraft, also known as "drones", are unmanned aircraft that are controlled by radio remote control equipment and self-contained program control devices. Drones are actually a general term for unmanned aerial vehicles, which can be divided into several categories from a technical perspective: unmanned helicopters, unmanned fixed-wing aircraft, unmanned multi-rotor aircraft, unmanned airships, and unmanned paragliders.

[0003] Existing survey drones need to conduct survey work in designated areas, but the environment and landing conditions of the working area of ​​the survey drones are unknown. They are easily damaged by collisions during survey work, causing economic losses. Summary of the invention

[0004] The purpose of the present invention is to provide a data collection drone for terrain survey to solve the problems raised in the above background technology.

[0005] To achieve the above object, the present invention provides the following technical solutions:

[0006] A data collection drone for terrain surveying, a protective component is provided on one side of a body component, the protective component is detachably connected to the body component, a survey component is provided on one side of the body component, the survey component is installed and connected in the body component, support components are provided on both sides of the survey component, one side of the support component is fixedly connected to the body component.

[0007] As a further solution of the present invention: the body assembly includes a fuselage, an extension bracket, a propeller, a bearing, a temperature detection component and a base, the fuselage is provided with an extension bracket around the fuselage, the extension bracket is integrally formed on the fuselage, the extension bracket is provided with a propeller, the propeller is rotatably connected to the extension bracket through a bearing, and the bearing is installed and connected to the extension bracket.

[0008] As a further solution of the present invention: a temperature detection component is provided on the upper side of the fuselage, the temperature detection component is fixedly connected to the fuselage, and a base is provided on the lower side of the fuselage, the base is fixedly connected to the fuselage.

[0009] As a further solution of the present invention: the protective assembly includes a protective outer frame, connecting rods, and support rods. A plurality of connecting rods are provided on one side of the protective outer frame, and the connecting rods are fixedly connected to the protective outer frame. The protective outer frame is fixedly connected to the extension bracket through the connecting rods. A plurality of support rods are provided in the protective outer frame, and the support rods are fixedly connected to the protective outer frame.

[0010] As a further solution of the present invention: the protective assembly includes a protective outer frame, connecting rods, and support rods. A plurality of connecting rods are provided on one side of the protective outer frame, and the connecting rods are fixedly connected to the protective outer frame. The protective outer frame is fixedly connected to the extension bracket through the connecting rods. A plurality of support rods are provided in the protective outer frame, and the support rods are fixedly connected to the protective outer frame.

[0011] As a further solution of the present invention: the survey component includes a cylinder and a survey camera, the cylinder is fixedly connected to the base, the output end of the cylinder is provided with a survey camera, and the survey camera is fixedly connected to the output end of the cylinder.

[0012] As a further solution of the present invention: the supporting assembly includes a fixed rod, a movable rod, a support block, a spring, and a damper. Fixed rods are provided on both sides of the base, the fixed rods are fixedly connected to the base, a movable rod is provided in the fixed rod, the movable rod is slidably connected in the fixed rod, one end of the movable rod is fixedly connected to the support block, the support block is fixedly connected to the movable rod, a spring is provided on one side of the movable rod, one end of the spring is fixedly connected to the movable rod, and the other end is fixedly connected to the fixed rod, a damper is provided in the spring, and the damper is installed and connected between the fixed rod and the movable rod.

[0013] Compared with the prior art, the present invention has the following beneficial effects:

[0014] The wings and fuselage can be protected by protective components. The open design will not affect the lifting of the wings. The temperature of the road section at that time can be detected by the temperature detection part, and the exploration camera can be controlled by the cylinder to enter the base for protection. BRIEF DESCRIPTION OF THE DRAWINGS

[0015] Figure 1 The figure is a schematic diagram of the structure of a data collection UAV for terrain survey.

[0016] Figure 2 This is a schematic diagram of the structure of a front section of a data collection drone used for terrain survey.

[0017] Figure 3 The diagram is a bird's-eye view of the structure of a data collection drone used for terrain survey.

[0018] Figure 4 This is a schematic diagram of the structure of a data collection drone used for terrain survey when viewed from above.

[0019] Figure 5 A schematic diagram of the structure of a data collection drone for terrain survey, enlarged at point A DETAILED DESCRIPTION

[0020] The following will be combined with the drawings in the embodiments of the present invention to clearly and completely describe the technical solutions in the embodiments of the present invention. Obviously, the described embodiments are only part of the embodiments of the present invention, not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the present invention.

[0021] See also Figures 1 to 5 In an embodiment of the present invention, a data collection drone for terrain survey includes a body component 100, a protection component 200, a survey component 300, and a support component 400.

[0022] A protection component 200 is provided on one side of the body component 100, and the protection component 200 is detachably connected to the body component 100. A survey component 300 is provided on one side of the body component 100, and the survey component 300 is installed and connected in the body component 100. Support components 400 are provided on both sides of the survey component 300, and one side of the support component 400 is fixedly connected to the body component 100.

[0023] The body assembly 100 includes a fuselage 101, an extension bracket 102, a propeller 103, a bearing 104, a temperature detection component 105 and a base 106. The fuselage 101 is provided with an extension bracket 102 around it. The extension bracket 102 is integrally formed on the fuselage 101. The extension bracket 102 is provided with a propeller 103. The propeller 103 is rotatably connected to the extension bracket 102 through a bearing 104. The bearing 104 is installed and connected to the extension bracket 102.

[0024] A temperature detection component 105 is provided on the upper side of the body 101 , and the temperature detection component 105 is fixedly connected to the body 101 . A base 106 is provided on the lower side of the body 101 , and the base 106 is fixedly connected to the body 101 .

[0025] The protective assembly 200 includes a protective outer frame 201, connecting rods 202, and support rods 203. A plurality of connecting rods 202 are provided on one side of the protective outer frame 201, and the connecting rods 202 are fixedly connected to the protective outer frame 201. The protective outer frame 201 is fixedly connected to the extension bracket 102 through the connecting rods 202. A plurality of support rods 203 are provided in the protective outer frame 201, and the support rods 203 are fixedly connected to the protective outer frame 201.

[0026] The survey component 300 includes a cylinder 301 and a survey camera 302 . The cylinder 301 is fixedly connected to the base 106 . The output end of the cylinder 301 is provided with the survey camera 302 . The survey camera 302 is fixedly connected to the output end of the cylinder 301 .

[0027] The support assembly 400 includes a fixed rod 401, a movable rod 402, a support block 403, a spring 404, and a damper 405. Fixed rods 401 are provided on both sides of the base 106, and the fixed rod 401 is fixedly connected to the base 106. A movable rod 402 is provided in the fixed rod 106, and the movable rod 402 is slidably connected to the fixed rod 401. One end of the movable rod 402 is fixedly connected to the support block 403, and the support block 403 is fixedly connected to the movable rod 402. A spring 404 is provided on one side of the movable rod 402, and one end of the spring 404 is fixedly connected to the movable rod 402, and the other end is fixedly connected to the fixed rod 401. A damper 405 is provided in the spring 404, and the damper 405 is installed and connected between the fixed rod 401 and the movable rod 402.

[0028] The working principle of the present invention is:

[0029] The wings and fuselage 101 can be protected by the protective component 200. The open design will not affect the lifting of the wings. The temperature of the road section at that time can be detected by the temperature detection component 105, and the exploration camera can be controlled by the cylinder 301 to enter the base 106 for protection.

[0030] Although the present invention has been described in detail with reference to the aforementioned embodiments, it is still possible for those skilled in the art to modify the technical solutions described in the aforementioned embodiments, or to make equivalent substitutions for some of the technical features therein. Any modifications, equivalent substitutions, improvements, etc. made within the spirit and principles of the present invention should be included in the protection scope of the present invention.

Claims

1. A data collection drone for terrain survey, comprising a body component (100), a protection component (200), a survey component (300), and a support component (400), characterized in that: A protection component (200) is provided on one side of the body component (100), and the protection component (200) is detachably connected to the body component (100). A survey component (300) is provided on one side of the body component (100), and the survey component (300) is installed and connected in the body component (100). Support components (400) are provided on both sides of the survey component (300), and one side of the support component (400) is fixedly connected to the body component (100).

2. The data collection drone for terrain survey according to claim 1, characterized in that: The body assembly (100) comprises a body (101), an extension bracket (102), a propeller (103), a bearing (104), a temperature detection component (105) and a base (106); the extension bracket (102) is arranged around the body (101); the extension bracket (102) is integrally formed on the body (101); the extension bracket (102) is provided with a propeller (103); the propeller (103) is rotatably connected to the extension bracket (102) via a bearing (104); and the bearing (104) is installed and connected to the extension bracket (102).

3. The data collection drone for terrain survey according to claim 1, characterized in that: A temperature detection component (105) is provided on the upper side of the fuselage (101), and the temperature detection component (105) is fixedly connected to the fuselage (101). A base (106) is provided on the lower side of the fuselage (101), and the base (106) is fixedly connected to the fuselage (101).

4. The data collection drone for terrain survey according to claim 1, characterized in that: The protection component (200) comprises a protection outer frame (201), connecting rods (202), and support rods (203); a plurality of groups of connecting rods (202) are provided on one side of the protection outer frame (201); the connecting rods (202) are fixedly connected to the protection outer frame (201); the protection outer frame (201) is fixedly connected to the extension bracket (102) via the connecting rods (202); a plurality of groups of support rods (203) are provided in the protection outer frame (201); the support rods (203) are fixedly connected to the protection outer frame (201).

5. The data collection drone for terrain survey according to claim 1, characterized in that: The survey component (300) comprises a cylinder (301) and a survey camera (302). The cylinder (301) is fixedly connected to the base (106). The output end of the cylinder (301) is provided with a survey camera (302). The survey camera (302) is fixedly connected to the output end of the cylinder (301).

6. The data collection drone for terrain survey according to claim 1, characterized in that: The support assembly (400) comprises a fixed rod (401), a movable rod (402), a support block (403), a spring (404), and a damper (405). The fixed rods (401) are arranged on both sides of the base (106). The fixed rods (401) are fixedly connected to the base (106). The fixed rods (106) are provided with movable rods (402). The movable rods (402) are slidably connected to the fixed rods (401). One end of the movable rods (402) A support block (403) is fixedly connected, and the support block (403) is fixedly connected to the movable rod (402). A spring (404) is provided on one side of the movable rod (402), and one end of the spring (404) is fixedly connected to the movable rod (402), and the other end is fixedly connected to the fixed rod (401). A damper (405) is provided in the spring (404), and the damper (405) is installed and connected between the fixed rod (401) and the movable rod (402).

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