Propeller protection frame of unmanned aerial vehicle
By designing the drone propeller protective frame, the fuselage body body, support rod, protective frame, top cover and limit mechanism are used to solve the problem of drone propeller being easily damaged during low altitude flight, and the propeller is realized effective protection and reduction of crash accidents.
Patent Information
- Application Number
- CN202420130771.1
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-01-19
- Publication Date
- 2025-02-07
- Estimated Expiration
- 2034-01-19
AI Technical Summary
When existing drones fly at low altitudes, propellers are prone to collision with branches or birds, resulting in damage and crashes.
A drone propeller protective frame is designed, including the fuselage body, support rod, protective frame, top cover, limit mechanism and other components. Through the cooperation of these components, the propeller is protected and its position is restricted to prevent external objects from contacting.
Effectively prevent the propeller from being damaged during flight, reduce the risk of crashes, and ensure the stability and convenience of the protective frame and roof cover through the design of the limit mechanism.
Smart Images

Figure CN222432623U_ABST
Abstract
Description
Technical Field
[0001] The utility model relates to the technical field of unmanned aerial vehicle protection, in particular to a propeller protection frame for an unmanned aerial vehicle. Background Art
[0002] The function and use of drones is aerial photography. Both photographers and filmmakers cannot do without the support of drones. Drones can also be used in agriculture. Farmers can use drones to spray pesticides on a large scale.
[0003] Some existing drones do not have their propellers protected. When the operator controls the drone to fly at low altitude in a place with trees, the operator may cause the drone's propeller to hit some branches or flying birds if he is not careful. In order to fly, the propeller of the drone often rotates at a faster speed. The high-speed rotating propeller is easily damaged when it hits these things, thus causing a crash. For this reason, we provide a drone propeller protection framework to solve the above problems. Utility Model Content
[0004] 1) Technical issues solved
[0005] The purpose of the utility model is to make up for the deficiencies of the prior art and provide a UAV propeller protection frame.
[0006] 2) Technical solution
[0007] To achieve the above-mentioned purpose, the utility model provides the following technical solutions: a propeller protection frame of a UAV, comprising a fuselage body, the upper surface of the fuselage body is fixedly connected to a support rod, the outer surface of the support rod is threadedly connected to a protection frame, a ventilation hole 1 is opened inside the protection frame, a top cover is slidably connected to the upper surface of the protection frame, a ventilation hole 2 is opened inside the top cover, a limiting block is fixedly connected to the outer surface of the top cover, an insert block is slidably connected to the upper surface of the top cover, a spring 1 is fixedly connected to the outer surface of the insert block, a limiting shell is slidably connected to the outer surface of the insert block, and a limiting mechanism is arranged above the fuselage body.
[0008] Furthermore, the limiting mechanism includes a slider, the outer surface of the slider is slidably connected to the inside of the insert block, the outer surface of the slider is slidably connected to a support block, and the upper surface of the support block is fixedly connected to the bottom surface of the limiting shell.
[0009] Furthermore, the outer surface of the support block contacts the outer surface of the protective frame, the bottom surface of the support block is fixedly connected to the upper surface of the fuselage body, the interior of the support block is slidably connected with a slide rod, and the upper surface of the slide rod is fixedly connected to the bottom surface of the slider.
[0010] Furthermore, a second spring is fixedly connected inside the support block, one end of the second spring away from the support block is fixedly connected to the bottom surface of the slider, and the second spring is sleeved on the outer surface of the slide rod.
[0011] Furthermore, a push block is fixedly connected to the outer surface of the sliding block, and the outer surface of the push block is slidably connected to the inside of the supporting block.
[0012] Furthermore, the outer surface of the limit block is slidably connected to the inside of the protective frame, and one end of the spring away from the insertion block is fixedly connected to the inside of the limit shell.
[0013] Furthermore, a resistance-enhancing block is fixedly connected to the upper surface of the insert block, and a support foot is installed below the fuselage body.
[0014] III) Beneficial effects
[0015] Compared with the prior art, the UAV propeller protection frame has the following beneficial effects:
[0016] The utility model cooperates with the top cover and the limiting mechanism and other components. First, the top cover can protect the propeller. After the top cover is placed inside the protective frame, the propeller will be protected inside the protective frame, so that other objects cannot easily touch the propeller, thereby preventing the propeller from being damaged. The limiting mechanism can limit the position of the plug-in block. After the top cover is inserted into the protective frame, the plug-in block can be inserted into the top cover to fix the position of the top cover. Then the limiting mechanism fixes the position of the plug-in block to prevent the plug-in block from detaching from the top cover, thereby preventing the top cover from falling from the protective frame. It is very convenient and solves the problem that the propeller is easily touched by other objects.
[0017] The utility model cooperates between the insert block and the limit shell, so that when the top cover is put into the protective frame, the top cover will move with the limit block, so that the limit block is inserted into the protective frame first, so as to prevent one side of the top cover from tilting up during the take-off of the drone. The limit shell can limit the position of the insert block, so that the top cover cannot move directly upward, so as to prevent the insert block from being unable to limit the position of the top cover, which is very easy to use. BRIEF DESCRIPTION OF THE DRAWINGS
[0018] Figure 1 This is the overall structure diagram of the utility model;
[0019] Figure 2 This is the structure diagram of the limit mechanism of the utility model;
[0020] Figure 3 This is a cross-sectional structural diagram of the protective frame of the utility model;
[0021] Figure 4 This is a cross-sectional structural diagram of the limit shell of the utility model;
[0022] Figure 5 It is a top view of the connection relationship of the top cover of the utility model.
[0023] In the figure: 1. body; 2. support rod; 3. protective frame; 4. ventilation hole 1; 5. top cover; 6. ventilation hole 2; 7. limit block; 8. plug block; 9. spring 1; 10. limit shell; 11. limit mechanism; 1101. slider; 1102. support block; 1103. slide rod; 1104. spring 2; 1105. push block; 12. resistance increasing block; 13. support foot. DETAILED DESCRIPTION
[0024] The following will be combined with the drawings in the embodiments of the utility model to clearly and completely describe the technical solutions in the embodiments of the utility model. Obviously, the described embodiments are only part of the embodiments of the utility model, not all of the embodiments. Based on the embodiments in the utility model, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the utility model.
[0025] like Figure 1-Figure 5 As shown, the utility model provides a technical solution: a drone propeller protection frame, including a fuselage body 1, a support rod 2 is fixedly connected to the upper surface of the fuselage body 1, and a protection frame 3 is threadedly connected to the outer surface of the support rod 2. The fuselage body 1 will fix the position of the support rod 2, and the protection frame 3 can be fixed to the support rod 2 by threads, so that the protection frame 3 can be disassembled.
[0026] A ventilation hole 1 4 is provided inside the protective frame 3, a top cover 5 is slidably connected to the upper surface of the protective frame 3, a ventilation hole 2 6 is provided inside the top cover 5, air can be transmitted to the propeller through the ventilation hole 1 4, the top cover 5 can be put into the protective frame 3, and the ventilation hole 2 6 allows air to pass through the top cover 5.
[0027] The outer surface of the top cover 5 is fixedly connected to the limit block 7, and the upper surface of the top cover 5 is slidably connected to the insert block 8. The top cover 5 will fix the position of the limit block 7, and will move with the limit block 7 when the top cover 5 moves. The position of the top cover 5 is limited by inserting the insert block 8 into the interior of the top cover 5.
[0028] The outer surface of the plug block 8 is fixedly connected with a spring 9, and the outer surface of the plug block 8 is slidably connected with a limit shell 10. A limit mechanism 11 is arranged above the fuselage body 1. The spring 9 can push the plug block 8 to move after being compressed, and the limit shell 10 can limit the direction in which the plug block 8 can move, thereby avoiding deviation in the moving position of the plug block 8.
[0029] The limiting mechanism 11 includes a slider 1101, the outer surface of the slider 1101 is slidably connected to the inside of the plug block 8, the outer surface of the slider 1101 is slidably connected to a support block 1102, the upper surface of the support block 1102 is fixedly connected to the bottom surface of the limiting shell 10, and the position of the plug block 8 is limited by inserting the slider 1101 into the inside of the plug block 8, so that the plug block 8 cannot move, and the support block 1102 can control the position to which the slider 1101 can move, thereby avoiding deviation in the moving position of the slider 1101.
[0030] The outer surface of the support block 1102 contacts the outer surface of the protective frame 3, and the bottom surface of the support block 1102 is fixedly connected to the upper surface of the fuselage body 1. The support block 1102 can prevent the protective frame 3 from vibrating, and the position of the support block 1102 is fixed by the fuselage body 1.
[0031] The support block 1102 is internally slidably connected to a slide bar 1103, the upper surface of the slide bar 1103 is fixedly connected to the bottom surface of the slider 1101, and the support block 1102 can control the direction of movement of the slide bar 1103 to avoid deviation in the position of the slide bar 1103, and will move with the slide bar 1103 when the slider 1101 moves.
[0032] A spring 2 1104 is fixedly connected inside the support block 1102. One end of the spring 2 1104 away from the support block 1102 is fixedly connected to the bottom surface of the slider 1101. The spring 2 1104 is sleeved on the outer surface of the slide bar 1103. The support block 1102 will fix the position of the spring 2 1104, and when the spring 2 1104 is compressed, it can push the slider 1101 to move.
[0033] The outer surface of the slider 1101 is fixedly connected to a push block 1105, and the outer surface of the push block 1105 is slidably connected to the inside of the support block 1102. The slider 1101 can fix the position of the push block 1105, and when the push block 1105 moves, it will move with the slider 1101, and the support block 1102 will limit the position to which the slider 1101 can move.
[0034] The outer surface of the limit block 7 is slidably connected to the inside of the protective frame 3, and the end of the spring 9 away from the plug block 8 is fixedly connected to the inside of the limit shell 10. When the top cover 5 is placed into the protective frame 3, it will be inserted into the protective frame 3 with the limit block 7, so that one end of the top cover 5 will be tilted when the drone moves, and the limit shell 10 will fix the position of the spring 9.
[0035] The upper surface of the insert block 8 is fixedly connected with a resistance-increasing block 12, and a support foot 13 is installed under the fuselage body 1. The resistance-increasing block 12 allows the user to move the insert block 8 more easily, and the support foot 13 can make it easier for the fuselage body 1 to land.
[0036] Working principle: When using the device, you first need to screw the protective frame 3 onto the support rod 2, then install the propeller on the fuselage body 1, and put the top cover 5 onto the protective frame 3. At this time, you need to insert the limit block 7 into the protective frame 3 first, and then put the top cover 5 flat. The spring 1 9 will push the plug block 8 into the top cover 5, so that the top cover 5 cannot move. After the plug block 8 is inserted into the appropriate position inside the top cover 5, the spring 2 1104 will push the support block 1102 into the plug block 8, thereby completely fixing the position of the plug block 8, so that the propeller will be protected in the protective frame 3 and the top cover 5.
Claims
1. A propeller protection frame for an unmanned aerial vehicle, comprising a fuselage body (1), characterized in that: The upper surface of the fuselage body (1) is fixedly connected to a support rod (2), the outer surface of the support rod (2) is threadedly connected to a protection frame (3), a ventilation hole (4) is provided inside the protection frame (3), a top cover (5) is slidably connected to the upper surface of the protection frame (3), a ventilation hole (6) is provided inside the top cover (5), a limiting block (7) is fixedly connected to the outer surface of the top cover (5), an insert block (8) is slidably connected to the upper surface of the top cover (5), a spring (9) is fixedly connected to the outer surface of the insert block (8), a limiting shell (10) is slidably connected to the outer surface of the fuselage body (1), and a limiting mechanism (11) is provided above the fuselage body (1).
2. The UAV propeller protection frame according to claim 1, characterized in that: The limiting mechanism (11) comprises a slider (1101), the outer surface of the slider (1101) being slidably connected to the inside of the insert block (8), the outer surface of the slider (1101) being slidably connected to a support block (1102), and the upper surface of the support block (1102) being fixedly connected to the bottom surface of the limiting shell (10).
3. The UAV propeller protection frame according to claim 2, characterized in that: The outer surface of the support block (1102) contacts the outer surface of the protective frame (3), the bottom surface of the support block (1102) is fixedly connected to the upper surface of the fuselage body (1), the interior of the support block (1102) is slidably connected to a slide rod (1103), and the upper surface of the slide rod (1103) is fixedly connected to the bottom surface of the slider (1101).
4. The UAV propeller protection frame according to claim 3, characterized in that: A second spring (1104) is fixedly connected inside the support block (1102), one end of the second spring (1104) away from the support block (1102) is fixedly connected to the bottom surface of the slider (1101), and the second spring (1104) is sleeved on the outer surface of the slide rod (1103).
5. The UAV propeller protection frame according to claim 2, characterized in that: The outer surface of the sliding block (1101) is fixedly connected to a push block (1105), and the outer surface of the push block (1105) is slidably connected to the inside of the supporting block (1102).
6. The drone propeller protection frame according to claim 1, characterized in that: The outer surface of the limit block (7) is slidably connected to the inside of the protective frame (3), and the end of the spring (9) away from the plug block (8) is fixedly connected to the inside of the limit shell (10).
7. The UAV propeller protection frame according to claim 1, characterized in that: A resistance increasing block (12) is fixedly connected to the upper surface of the insert block (8), and a support foot (13) is installed below the fuselage body (1).