Undercarriage device of logistics distribution unmanned aerial vehicle

Abstract

The utility model relates to the field of unmanned aerial vehicles, in particular to a logistics distribution unmanned aerial vehicle undercarriage device which comprises a vehicle body, a distribution box is fixedly connected to the bottom of the vehicle body, supporting mechanisms are installed on the two sides of the bottom of the vehicle body, each supporting mechanism comprises a fixing base, and the top of each fixing base is fixedly connected with the bottom of the vehicle body. A positioning groove is formed in the bottom of the fixed seat; the supporting mechanism is arranged, a motor is started through an external power source, the motor drives a rotating shaft to rotate, the rotating shaft rotates to drive a rotating seat to rotate, the rotating seat rotates to drive a supporting plate to rotate, and the supporting plate rotates to drive a buffering cushion to rotate. Therefore, it can be ensured that the unmanned aerial vehicle can stably land on the ground, and the problems that an undercarriage usually adopts a fixed structure, when the ground environment is uneven, the undercarriage possibly cannot adapt to the gradient of the ground, and then the unmanned aerial vehicle turns on one side and damages goods are solved.

Description

Technical Field

[0001] This utility model relates to the field of unmanned aerial vehicles (UAVs), specifically a landing gear device for a logistics delivery UAV. Background Technology

[0002] Unmanned aerial vehicles (UAVs) are unmanned aircraft controlled by radio remote control equipment and onboard program control devices. They can carry different payloads to complete diverse tasks and are regarded as "aerial robots". In terms of logistics and delivery, UAVs have advantages such as high efficiency, flexibility and low cost, and are gradually reshaping the logistics industry landscape.

[0003] Landing gear is an essential component in the use of drones. Its main function is to support, cushion, and protect the drone, and to ensure stability and safety during takeoff, landing, and taxiing. However, existing landing gear usually adopts a fixed structure. When the ground environment is uneven, the landing gear may not be able to adapt to the slope of the ground, which may cause the drone to tip over and damage the cargo. Utility Model Content

[0004] To overcome the shortcomings of existing technologies, landing gear usually adopts a fixed structure. When the ground environment is uneven, the landing gear may not be able to adapt to the slope of the ground, which may lead to the drone tipping over and damaging the cargo. This utility model proposes a landing gear device for logistics delivery drones.

[0005] The technical solution adopted by this utility model to solve its technical problem is: a landing gear device for a logistics delivery drone, including a body, a delivery box fixedly connected to the bottom of the body, and support mechanisms installed on both sides of the bottom of the body;

[0006] The support mechanism includes a fixed base, the top of which is fixedly connected to the bottom of the machine body. A positioning groove is provided at the bottom of the fixed base, and a support frame is engaged in the inner cavity of the positioning groove. A motor is fixedly connected to the back side of the support frame, and a rotating shaft is fixedly connected to the output end of the motor. A rotating seat is fixedly connected to the surface of the rotating shaft, and a ventilation groove is provided in the inner cavity of the rotating seat. A support plate is fixedly connected to the bottom of the rotating seat.

[0007] Preferably, the bottom of the support plate is provided with a fixing groove, and a buffer pad made of rubber is fixedly connected to the inner cavity of the fixing groove.

[0008] Preferably, the bottom of the buffer pad is fixedly connected with a protrusion, and the number of the protrusions is several and arranged in multiple rows and columns.

[0009] Preferably, the bottom of the fixing base is provided with a connecting groove, the inner cavity of the connecting groove is inserted with a connecting plate, the bottom of the connecting plate is fixedly connected with a fixing plate, and the top of the fixing plate is in contact with the surfaces of the fixing base and the support frame respectively.

[0010] Preferably, both the support frame and the fixing plate have a fixing slot in their inner cavity, and an elastic block is engaged in the inner cavity of the fixing slot. The surface of the elastic block is fixedly connected to the inner cavity of the positioning slot, and the elastic block is made of nylon.

[0011] Preferably, a guide groove is provided at the top of the inner cavity of the support frame and the fixing plate, and a guide rod is inserted into the inner cavity of the guide groove, with one end of the guide rod being fixedly connected to the inner cavity of the positioning groove.

[0012] Preferably, a protective cover is fixedly connected to the surface of the motor, the front side of the protective cover is fixedly connected to the back side of the support frame, and the protective cover is made of aluminum alloy.

[0013] The advantages of this utility model are:

[0014] This invention, by setting up a support mechanism, starts a motor through an external power source, drives a rotating shaft to rotate, which in turn drives a rotating seat to rotate, which in turn drives a support plate to rotate, and the support plate to rotate a buffer pad. This ensures that the drone can land stably on the ground, solving the problem that landing gear, which is usually a fixed structure, may not be able to adapt to the slope of the ground when the ground is uneven, thus causing the drone to tip over and damage the cargo. Attached Figure Description

[0015] To more clearly illustrate the technical solutions in the embodiments of this utility model or the prior art, the drawings used in the description of the embodiments or the prior art will be briefly introduced below. Obviously, the drawings described below are only some embodiments of this utility model. For those skilled in the art, other drawings can be obtained based on these drawings without creative effort.

[0016] Figure 1 This is a schematic diagram of the structure of this utility model;

[0017] Figure 2 This is a schematic diagram of the structure of the body of this utility model;

[0018] Figure 3 This is a schematic diagram of the structure of the fixing base of this utility model;

[0019] Figure 4 This is a schematic diagram of the support frame of this utility model;

[0020] Figure 5 This is a partial connection diagram of the support frame of this utility model.

[0021] In the diagram: 1. Body; 2. Support mechanism; 201. Fixed seat; 202. Support frame; 203. Support plate; 204. Buffer pad; 205. Protrusion; 206. Protective cover; 207. Rotating shaft; 208. Ventilation slot; 209. Rotating seat; 210. Fixed plate; 211. Motor; 212. Fixed slot; 213. Guide rod; 214. Elastic locking block; 215. Positioning slot; 216. Connecting slot; 217. Connecting plate; 218. Fixed slot; 219. Guide slot; 3. Delivery box. Detailed Implementation

[0022] The technical solutions of the present utility model will be clearly and completely described below with reference to the accompanying drawings of the embodiments. Obviously, the described embodiments are only some embodiments of the present utility model, and not all embodiments. Based on the embodiments of the present utility model, all other embodiments obtained by those of ordinary skill in the art without creative effort are within the scope of protection of the present utility model.

[0023] The following is in conjunction with the appendix Figure 1-5 This application will be described in further detail.

[0024] This application discloses a landing gear device for a logistics delivery drone. (Refer to...) Figure 1 , Figure 2 , Figure 3 , Figure 4 and Figure 5 A landing gear device for a logistics delivery drone includes a body 1, a delivery box 3 fixedly connected to the bottom of the body 1, and support mechanisms 2 installed on both sides of the bottom of the body 1.

[0025] The support mechanism 2 includes a fixed base 201, the top of which is fixedly connected to the bottom of the body 1. A positioning groove 215 is provided at the bottom of the fixed base 201. A support frame 202 is engaged in the inner cavity of the positioning groove 215. A motor 211 is fixedly connected to the back side of the support frame 202. A rotating shaft 207 is fixedly connected to the output end of the motor 211. A rotating seat 209 is fixedly connected to the surface of the rotating shaft 207. A ventilation groove 208 is provided in the inner cavity of the rotating seat 209. A support plate 203 is fixedly connected to the bottom of the rotating seat 209.

[0026] Reference Figure 2 and Figure 4The bottom of the support plate 203 is provided with a fixing groove 212, and a buffer pad 204 is fixedly connected to the inner cavity of the fixing groove 212. The buffer pad 204 is made of rubber. By setting the buffer pad 204, the friction force received by the support plate 203 when in contact with the ground is increased, ensuring the stability of the support plate 203 when in contact with the ground. At the same time, the support plate 203, which is made of rubber, has high elasticity. When the aircraft 1 lands, it can absorb the impact energy through its own elastic deformation, thereby reducing the damage to the fuselage structure from direct impact and ensuring the smooth landing of the aircraft 1.

[0027] Reference Figure 2 The bottom of the buffer pad 204 is fixedly connected with protrusions 205. There are several protrusions 205 arranged in multiple rows and columns. By setting the protrusions 205, the roughness of the bottom of the support plate 203 can be increased, forming a physical interlock with the ground. At the same time, through the independent deformation of multiple protrusions 205, uneven areas of the ground can be automatically filled, ensuring that the support plate 203 as a whole is in full contact with the ground.

[0028] Reference Figure 4 and Figure 5 The bottom of the fixed base 201 is provided with a connecting groove 216, and a connecting plate 217 is inserted into the inner cavity of the connecting groove 216. A fixing plate 210 is fixedly connected to the bottom of the connecting plate 217. The top of the fixing plate 210 contacts the surfaces of the fixed base 201 and the support frame 202 respectively. The fixing plate 210 limits the support frame 202 and prevents the support frame 202 from detaching from the inside of the positioning groove 215 during use. When the fixing plate 210 is in place, the surface of the connecting plate 217 will engage with the inside of the connecting groove 216, thereby positioning the fixing plate 210 and preventing the fixing plate 210 from detaching from the bottom of the support frame 202 during use.

[0029] Reference Figure 4 and Figure 5Both the support frame 202 and the fixing plate 210 have fixing slots 218 inside their cavities. An elastic block 214 engages with the cavity of the fixing slot 218. The surface of the elastic block 214 is fixedly connected to the cavity of the positioning groove 215. The elastic block 214 is made of nylon. The fixing slots 218 allow the surface of the elastic block 214 to engage with the interior of the support frame 202 and the fixing plate 210, thus initially positioning the support frame 202 and ensuring its stable fit within the positioning groove 215. Simultaneously, the fixing plate 210 can be fixed... The position is reinforced to further improve the fixing effect of the fixing plate 210 and ensure the stable use of the fixing plate 210. The elastic block 214 made of nylon has the characteristics of environmental aging resistance, wear resistance, impact resistance and high tensile strength, ensuring the stability of the elastic block 214 during use, reducing the time required to disassemble the support frame 202, and avoiding the loosening that can easily occur during use when fixed with bolts. The nylon molecular chain structure is compact and achieves quick insertion through elastic deformation. The interlocking force is stable and there is no risk of loosening or falling off during use.

[0030] Reference Figure 4 and Figure 5 The top of the inner cavity of the support frame 202 and the fixing plate 210 is provided with a guide groove 219. A guide rod 213 is inserted into the inner cavity of the guide groove 219. One end of the guide rod 213 is fixedly connected to the inner cavity of the positioning groove 215. The guide rod 213 guides the movement of the support frame 202 and the fixing plate 210, ensuring that the support frame 202 and the fixing plate 210 can be stably attached to the surface of the fixing seat 201, and preventing the position of the support frame 202 and the fixing plate 210 from shifting during the movement, which would affect the subsequent normal positioning.

[0031] Reference Figure 3 and Figure 4 A protective cover 206 is fixedly connected to the surface of the motor 211. The front side of the protective cover 206 is fixedly connected to the back side of the support frame 202. The protective cover 206 is made of aluminum alloy. The protective cover 206 protects the surface of the motor 211. The protective cover 206, made of aluminum alloy, has excellent thermal conductivity, which can help the motor 211 dissipate heat. It also has the ability to prevent splashing, moisture and dust, and can adapt to various weather conditions to ensure the stable operation of the motor 211.

[0032] Working principle: Before landing, the aircraft 1 automatically observes the ground conditions through its camera. If the landing surface is uneven, the motor 211 is started by an external power source. The motor 211 drives the rotating shaft 207 to rotate, which in turn drives the rotating seat 209 to rotate. The rotation of the rotating seat 209 drives the support plate 203 to rotate, adjusting the angle of the support plate 203 to ensure that it is roughly in contact with the ground. The rotation of the support plate 203 drives the buffer pad 204 to rotate, allowing the buffer pad 204 to fit more stably against the ground, thus ensuring that the aircraft 1 can land stably on the ground.

[0033] It should be noted that parts have a lifespan and can be replaced during regular maintenance when they no longer meet performance requirements. Deterioration in performance due to prolonged use of parts is not a design defect of this application.

[0034] The foregoing has shown and described the basic principles, main features, and advantages of this utility model. Those skilled in the art should understand that this utility model is not limited to the above embodiments. The embodiments and descriptions in the specification are merely illustrative of the principles of this utility model. Various changes and modifications can be made to this utility model without departing from its spirit and scope, and all such changes and modifications fall within the scope of the claimed utility model.

Claims

1. A landing gear device for a logistics delivery drone, comprising a body (1), characterized in that: The bottom of the body (1) is fixedly connected to a delivery box (3), and support mechanisms (2) are installed on both sides of the bottom of the body (1). The support mechanism (2) includes a fixed seat (201), the top of which is fixedly connected to the bottom of the body (1). The bottom of the fixed seat (201) is provided with a positioning groove (215). A support frame (202) is engaged in the inner cavity of the positioning groove (215). A motor (211) is fixedly connected to the back side of the support frame (202). A rotating shaft (207) is fixedly connected to the output end of the motor (211). A rotating seat (209) is fixedly connected to the surface of the rotating shaft (207). A ventilation groove (208) is provided in the inner cavity of the rotating seat (209). A support plate (203) is fixedly connected to the bottom of the rotating seat (209).

2. The landing gear device for a logistics delivery drone according to claim 1, characterized in that: The bottom of the support plate (203) is provided with a fixing groove (212), and a buffer pad (204) is fixedly connected to the inner cavity of the fixing groove (212). The buffer pad (204) is made of rubber.

3. The landing gear device for a logistics delivery drone according to claim 2, characterized in that: The bottom of the buffer pad (204) is fixedly connected with a protrusion (205), and the number of protrusions (205) is several and arranged in multiple rows and columns.

4. The landing gear device for a logistics delivery drone according to claim 1, characterized in that: The bottom of the fixed base (201) is provided with a connecting groove (216), and a connecting plate (217) is inserted into the inner cavity of the connecting groove (216). A fixing plate (210) is fixedly connected to the bottom of the connecting plate (217), and the top of the fixing plate (210) is in contact with the surfaces of the fixed base (201) and the support frame (202).

5. The landing gear device for a logistics delivery drone according to claim 4, characterized in that: The inner cavity of the support frame (202) and the fixing plate (210) is provided with a fixing slot (218). The inner cavity of the fixing slot (218) is fitted with an elastic block (214). The surface of the elastic block (214) is fixedly connected to the inner cavity of the positioning groove (215). The elastic block (214) is made of nylon.

6. The landing gear device for a logistics delivery drone according to claim 4, characterized in that: The top of the inner cavity of the support frame (202) and the fixing plate (210) is provided with a guide groove (219), and a guide rod (213) is inserted into the inner cavity of the guide groove (219). One end of the guide rod (213) is fixedly connected to the inner cavity of the positioning groove (215).

7. The landing gear device for a logistics delivery drone according to claim 1, characterized in that: A protective cover (206) is fixedly connected to the surface of the motor (211). The front side of the protective cover (206) is fixedly connected to the back side of the support frame (202). The protective cover (206) is made of aluminum alloy.

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