A blade structure for a micro air vehicle

Abstract

The utility model discloses a kind of blade structures for micro flying car, including walking base, storage module and flight frame, supporting member is installed between flight frame and walking base, the upper side and the lower side of flight frame are both installed with plane plate, front rotating block is installed in the both sides of plane plate front end, rear rotating block is installed in the both sides of plane plate rear end, and front rotating block and rear rotating block are set on the same plane front and back staggered. The utility model improves micro flying car, let the flight frame structure of upper portion can form two different states of expansion and storage based on use mode, when carrying and only using ground kinetic energy structure, flight frame can be condensed to surface, to reduce overall space occupation, the triangular structure formed can also form wind-breaking effect.

Description

Technical Field

[0001] This utility model relates to the field of micro flying cars, and in particular to a blade structure for micro flying cars. Background Technology

[0002] Flying cars, also known as micro flying cars, are similar in size to existing RC race cars with added flying components. Conventional flying structures generally have a folding structure. Existing technology with patent number CN113320685B also discloses a similar structure, which mainly involves folding the blade structure to reduce the carrying space.

[0003] However, since micro flying cars sometimes need to use ground-based forward movement for extended periods, the blade structure not only increases wind resistance but also makes overall storage difficult, especially at the extension rods connecting the blades, which cannot meet the portability requirements of the overall structure. Utility Model Content

[0004] The technical problem to be solved by this utility model is to overcome the defects of the prior art and provide a blade structure for micro flying cars, mainly to solve the problems of existing micro flying cars being inconvenient to store and affecting the use of ground driving function after storage.

[0005] To solve the above-mentioned technical problems, this utility model provides the following technical solution:

[0006] This utility model relates to a blade structure for a micro flying car, comprising a base, a storage module, and a flight frame. A support is installed between the flight frame and the base. Flat plates are installed on the upper and lower sides of the flight frame. Front rotating blocks are installed on both sides of the front end of the flat plates, and rear rotating blocks are installed on both sides of the rear end of the flat plates. The front and rear rotating blocks are staggered on the same plane. Each front and rear rotating block is equipped with an extension rod. A mounting base is provided at the end of the extension rod. A rotating module is installed on the top of the mounting base. A fixing member is provided at the top of the rotating module. A clamping member is installed on the top of the fixing member. Flight blades are fixed at both ends of the clamping member. The flight blades are used to fix to the two ends of the clamping member or to rotate circumferentially around the end of the clamping member. The front and rear rotating blocks are used to fold the extension rods to the middle of the flat plate.

[0007] Preferably, the clamping member includes an upper crossbar, a lower crossbar, and a connecting screw. The flight blade is located between the upper crossbar and the lower crossbar and is connected to the surface of the lower crossbar through the connecting screw. The bottom of the lower crossbar is connected to the rotating module through a fixing member for transmission.

[0008] Preferably, a fastening screw is installed on the top of the clamping member, which is used to fix the flight blade to the clamping member. The fastening screw is slidably sleeved with the upper crossbar and threadedly connected to the lower crossbar.

[0009] Preferably, the rotating module is a drive motor, which is used to drive the rotation of the flight blades; the rotating module and the extension rod are fixedly connected by a mounting base, and the height of the mounting base is not lower than the height of the flight frame.

[0010] Preferably, the upper planar plate surface is provided with a limiting groove, which is used to limit the extension rod; the upper surfaces of the front rotating block and the rear rotating block are both provided with spring buckles, which are correspondingly arranged with the limiting groove structure.

[0011] Preferably, the planar plate includes a front plate, a rear plate, and a middle plate, wherein the area of ​​the front plate is smaller than that of the rear plate, and the connection between the middle plate and the rear plate is set at a right angle.

[0012] Preferably, the rotation direction of the front rotating blocks is towards the tail plate, and the rotation direction of the rear rotating blocks is towards the front plate.

[0013] Preferably, the flight blade is rotated by a connecting screw, and the direction of rotation of the flight blade is towards the front plate.

[0014] Preferably, the flight frame surface includes an electronic control module and a wireless connection module. The electronic control module is an MCU microcontroller or an STM32 microcontroller, and the wireless connection module is a cellular network or a Bluetooth module.

[0015] Compared with the prior art, the beneficial effects of this utility model are as follows:

[0016] This invention improves upon the micro flying car, allowing the upper flying frame structure to be deployed and retracted depending on the usage method. When carried or when using only the ground kinetic energy structure, the flying frame can be retracted to the surface to reduce the overall space occupied, while the resulting triangular structure can also create a wind-breaking effect. Attached Figure Description

[0017] The accompanying drawings are provided to further illustrate the present invention and form part of the specification. They are used together with the embodiments of the present invention to explain the present invention, but do not constitute a limitation thereof. In the drawings:

[0018] Figure 1 This is a schematic diagram of the overall structure of this utility model;

[0019] Figure 2 This is a partial structural schematic diagram of the present invention;

[0020] Figure 3This is a schematic diagram of the flight blade structure of this utility model;

[0021] Figure 4 This is a diagram showing the structure and storage of the flight blade of this utility model;

[0022] Figure 5 This is a schematic diagram of the spring buckle structure of this utility model;

[0023] In the diagram: 1. Walking base; 101. Storage module; 102. Flight frame; 103. Support component; 2. Flat plate; 201. Front plate; 202. Tail plate; 203. Middle plate; 3. Front rotating block; 4. Rear rotating block; 5. Extension rod; 6. Mounting base; 7. Rotating module; 8. Fixing component; 9. Clamping component; 901. Upper crossbar; 902. Lower crossbar; 903. Connecting screw; 904. Fastening screw; 10. Flight blade; 11. Limiting groove; 12. Spring buckle. Detailed Implementation

[0024] The preferred embodiments of the present invention will be described below with reference to the accompanying drawings. It should be understood that the preferred embodiments described herein are for illustration and explanation only and are not intended to limit the present invention.

[0025] In the attached diagram, all identical reference numerals refer to the same components.

[0026] like Figure 1-5 As shown, this utility model provides a blade structure for a micro flying car, including a walking base 1, a storage module 101 and a flight frame 102. A support member 103 is installed between the flight frame 102 and the walking base 1. A flat plate 2 is installed on the upper and lower sides of the flight frame 102. Front rotating blocks 3 are installed on both sides of the front end of the flat plate 2, and rear rotating blocks 4 are installed on both sides of the rear end of the flat plate 2. The front rotating blocks 3 and the rear rotating blocks 4 are staggered on the same plane.

[0027] Both the front rotating block 3 and the rear rotating block 4 are equipped with extension rods 5. The end of the extension rod 5 is provided with a mounting base 6. The top of the mounting base 6 is equipped with a rotating module 7. The top of the rotating module 7 is provided with a fixing member 8. The top of the fixing member 8 is equipped with a clamping member 9. Both ends of the clamping member 9 are fixed with flying blades 10. The flying blades 10 are used to fix to both ends of the clamping member 9 or to rotate around the end of the clamping member 9. The front rotating block 3 and the rear rotating block 4 are used to fold the extension rod 5 to the middle of the flat plate 2.

[0028] The surface of the flight frame 102 includes an electronic control module and a wireless connection module. The electronic control module is an MCU microcontroller or an STM32 microcontroller, and the wireless connection module is a cellular network or a Bluetooth module.

[0029] Its structure is mainly based on the walking base 1, the storage module 101, and the flight frame 102, such as Figure 1 As shown, the walking base 1 is equipped with a motor and tires, and the flight frame 102 forms the conversion between flight and ground movement. The storage module 101 is mainly used to transport or store the target object to the destination. Because the conventional structure is large when unfolded, it is not convenient to carry or store. Therefore, a foldable front rotating block 3 and a rear rotating block 4 are provided. Together with the clamping part 9, the rotating module 7 can be folded to both sides of the flight frame 102 to complete the storage function.

[0030] In a further embodiment, such as Figure 2 As shown, the clamping member 9 includes an upper crossbar 901, a lower crossbar 902, and a connecting screw 903. The flight blade 10 is located between the upper crossbar 901 and the lower crossbar 902, and is connected to the surface of the lower crossbar 902 by the connecting screw 903. The bottom of the lower crossbar 902 is connected to the rotating module 7 via a fixing member 8. A fastening screw 904 is installed on the top of the clamping member 9. The fastening screw 904 is used to fix the flight blade 10 to the clamping member 9. The fastening screw 904 is slidably sleeved with the upper crossbar 901, and the fastening screw 904 is threadedly connected to the lower crossbar 902. In this embodiment, the clamping member 9 mainly completes the clamping of the flight blade through the upper crossbar 901 and the lower crossbar 902. The clamping of the blade 10 is based on the connecting screw 903 passing through the flight blade 10 to the lower crossbar 902, allowing the flight blade 10 to rotate around the connecting screw 903, thus satisfying the function of circumferential rotation of the flight blade 10 around the end of the clamping member 9, that is, realizing the function of storage; when the flight blade 10 is used for flight, it is only necessary to rotate the fastening screw 904 downwards to make the upper crossbar 901 and the lower crossbar 902 clamp and fix it; if further simplification is required, the connecting screw 903 can be directly connected to the upper crossbar 901 and the lower crossbar 902 respectively, and when the flight blade 10 needs to rotate circumferentially, only the connecting screw 903 needs to be loosened, and the fastening screw 904 is only used as a secondary fixing structure.

[0031] In a further embodiment, such as Figure 5 As shown, the rotating module 7 is a drive motor, which is used to drive the rotation of the flight blade 10; the rotating module 7 and the extension rod 5 are fixedly connected by the mounting base 6; the upper side flat plate 2 has a limiting groove 11, which is used to limit the extension rod 5; the upper surfaces of the front rotating block 3 and the rear rotating block 4 are both provided with spring buckles 12, which are structurally corresponding to the limiting grooves 11; conventionally, the front rotating block 3 and the rear rotating block 4 can be provided with damping structures to prevent their own rotation. In order to improve their stability, spring buckles 12 are provided on the top of the front rotating block 3 and the rear rotating block 4, such as Figure 1As shown, the spring buckle 12 is used in conjunction with the limiting groove 11. In order to cooperate with the storage structure, the limiting groove 11 can be set in different positions on the flat plate 2 to achieve the limiting function after the front rotating block 3 and the rear rotating block 4 rotate, so that the extension rod 5 can be fixed and limited when stored and unfolded.

[0032] In a further embodiment, such as Figure 3-4 As shown, the planar plate 2 includes a front plate 201, a tail plate 202, and a middle plate 203, wherein the area of ​​the front plate 201 is smaller than that of the tail plate 202, and the connection between the middle plate 203 and the tail plate 202 is set at a right angle; the rotation direction of the front rotating blocks 3 is all towards the tail plate 202, and the rotation direction of the rear rotating blocks 4 is all towards the front plate 201; the flight blades 10 rotate via connecting screws 903, and the rotation direction of the flight blades 10 is towards the front plate 201; as shown... Figure 3 As can be seen in its unfolded state, during normal flight or use, the extension rod 5 extends outward from the four corners of the flat plate 2; when retracted, first rotate the front rotating block 3 until it forms the shape shown. Figure 4 In form, Figure 4 The planar plate 2 in the middle is the lower planar plate 2, and the fastening screw 904 is loosened so that the flight blade 10 faces the front plate 201. At this time, the end of the extension rod 5 of the front rotating block 3 is located at the right angle connection between the middle plate 203 and the tail plate 202, and the height of the rotating module 7 is above the upper planar plate 2; the rear rotating block 4 is then retracted as follows. Figure 4 The mode is covered on the outside, and the flight blade 10 also faces the front plate 201. This allows the rotating module 7 to be offset to the left and right, while the overall structure can also form a triangular structure facing forward. When the ground walking function is used alone, it can create a wind-breaking effect and reduce the wind resistance of the blade.

[0033] In summary, this utility model improves the micro flying car by allowing the upper flying frame structure to be deployed and retracted depending on the usage method. When carried or when only the ground kinetic energy structure is used, the flying frame can be retracted to the surface to reduce the overall space occupied, while the resulting triangular structure can also create a wind-breaking effect.

[0034] Finally, it should be noted that the above description is merely a preferred embodiment of this utility model and is not intended to limit the utility model. Although the utility model has been described in detail with reference to the foregoing embodiments, those skilled in the art can still modify the technical solutions described in the foregoing embodiments or make equivalent substitutions for some of the technical features. Any modifications, equivalent substitutions, improvements, etc., made within the spirit and principles of this utility model should be included within the protection scope of this utility model.

Claims

1. A blade structure for a micro flying car, comprising a base (1), a storage module (101), and a flight frame (102), wherein a support member (103) is installed between the flight frame (102) and the base (1), characterized in that, The flight frame (102) is equipped with a flat plate (2) on both the upper and lower sides. Front rotating blocks (3) are installed on both sides of the front end of the flat plate (2), and rear rotating blocks (4) are installed on both sides of the rear end of the flat plate (2). The front rotating blocks (3) and the rear rotating blocks (4) are staggered on the same plane. Both the front rotating block (3) and the rear rotating block (4) are equipped with extension rods (5). The end of the extension rod (5) is provided with a mounting seat (6). The top of the mounting seat (6) is equipped with a rotating module (7). The top of the rotating module (7) is provided with a fixing member (8). The top of the fixing member (8) is equipped with a clamping member (9). Both ends of the clamping member (9) are fixed with flight blades (10). The flight blades (10) are used to fix to both ends of the clamping member (9) or to rotate circumferentially around the end of the clamping member (9). The front rotating block (3) and the rear rotating block (4) are used to fold the extension rod (5) to the middle of the flat plate (2).

2. The blade structure for a micro flying car according to claim 1, characterized in that, The clamping member (9) includes an upper crossbar (901), a lower crossbar (902), and a connecting screw (903). The flying blade (10) is located between the upper crossbar (901) and the lower crossbar (902), and is connected to the surface of the lower crossbar (902) by the connecting screw (903). The bottom of the lower crossbar (902) is connected to the rotating module (7) by a fixing member (8).

3. The blade structure for a micro flying car according to claim 2, characterized in that, The clamping member (9) is equipped with a fastening screw (904) on its top. The fastening screw (904) is used to fix the flight blade (10) to the clamping member (9). The fastening screw (904) is slidably sleeved with the upper crossbar (901) and threadedly connected with the lower crossbar (902).

4. The blade structure for a micro flying car according to claim 3, characterized in that, The rotating module (7) is a drive motor, and its rotating module (7) is used to drive the flight blade (10) to rotate; the rotating module (7) and the extension rod (5) are fixedly connected by the mounting base (6), and the height of the mounting base (6) is not lower than the height of the flight frame (102).

5. A blade structure for a micro flying car according to claim 4, characterized in that, The upper flat plate (2) is provided with a limiting groove (11), which is used to limit the extension rod (5); the upper surfaces of the front rotating block (3) and the rear rotating block (4) are provided with spring buckles (12), which are structurally corresponding to the limiting groove (11).

6. The blade structure for a micro flying car according to claim 5, characterized in that, The planar plate (2) includes a front plate (201), a rear plate (202) and a middle plate (203), wherein the area of ​​the front plate (201) is smaller than that of the rear plate (202), and the connection between the middle plate (203) and the rear plate (202) is set at a right angle.

7. A blade structure for a micro flying car according to claim 6, characterized in that, The rotation direction of the front rotating block (3) is towards the tail plate (202), and the rotation direction of the rear rotating block (4) is towards the front plate (201).

8. A blade structure for a micro flying car according to claim 7, characterized in that, The flight blade (10) rotates via a connecting screw (903), and the direction of rotation of the flight blade (10) is toward the front plate (201).

9. A blade structure for a micro flying car according to claim 8, characterized in that, The surface of the flight frame (102) includes an electronic control module and a wireless connection module. The electronic control module is an MCU microcontroller or an STM32 microcontroller, and the wireless connection module is a cellular network or a Bluetooth module.

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