Unmanned aerial vehicle wing and unmanned aerial vehicle

Abstract

The utility model provides an unmanned aerial vehicle wing and an unmanned aerial vehicle, and relates to the technical field of unmanned aerial vehicles, the unmanned aerial vehicle wing comprises a main wing and a wingtip, the main wing is movably provided with a locking fastener, the wingtip is provided with a locking rod, and the end, provided with a limiting protrusion, of the locking rod can penetrate through the locking fastener; the first position abuts against the limiting protrusion in a matched mode in the axial direction of the lock rod, the second position relieves abutting against the limiting protrusion in the axial direction of the lock rod, and the lock catch piece is driven to be switched between the first position and the second position. The position switching design of the locking fastener is more flexible, so that the firmness of connection is ensured, the convenience in disassembly is realized, no extra tool is needed in the disassembly and assembly process, and the whole disassembly and assembly process is more efficient.

Description

Technical Field

[0001] The present application relates to the technical field of unmanned aerial vehicles (UAVs), and more specifically, to a UAV wing and a UAV. 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. In the rapid development of modern technology, drones, as an important technological innovation, are leading the transformation of the aviation field. Among them, fixed-wing drones have broad application prospects in fields that require long ranges, high loads and continuous flight time due to their many advantages such as fast flight speed, large payload and long flight time. With the continuous advancement of fixed-wing drone technology, a large wingspan design has become a prerequisite for this type of drone. However, the large wingspan design will make the overall size of the drone large, making it difficult to pack and transport. In order to save transportation space, the wings are usually split into multiple detachable parts, such as designing a detachable connection between the main wing and the wingtip to facilitate disassembly and transportation.

[0003] However, the main wing and wing tips usually require additional tools when being disassembled and assembled, which makes the operation cumbersome, time-consuming and labor-intensive, resulting in low operating efficiency. Utility Model Content

[0004] The purpose of this application is to provide a drone wing and a drone to address the deficiencies in the above-mentioned technology.

[0005] To achieve the above purpose, the technical solution adopted in the embodiment of the present application is as follows:

[0006] According to one aspect of an embodiment of the present application, a wing of a UAV is provided, including a main wing and a wingtip, a locking member is movably arranged on the main wing, a locking rod is arranged on the wingtip, the locking rod has an end with a limiting protrusion which can be passed through the locking member, the locking member has a first position which cooperates and abuts with the limiting protrusion along the axial direction of the locking rod and a second position which releases the abutment with the limiting protrusion along the axial direction of the locking rod, and the locking member is driven to switch between the first position and the second position.

[0007] Optionally, the drone wing further comprises an elastic member connected to the locking member, and the elastic member is used to provide a restoring force to the locking member so that the locking member has a tendency to remain in the first position.

[0008] Optionally, the locking member is provided with a first through hole and a second through hole that are interconnected, the aperture of the first through hole is larger than the aperture of the second through hole, the locking rod is passed through the first through hole and is arranged in the locking member, and the limiting protrusion abuts against the opening of the second through hole.

[0009] Optionally, the limiting protrusion is a conical protrusion, and the conical protrusion gradually shrinks along the penetration direction of the locking rod.

[0010] Optionally, a locking seat is provided on the main wing, and the locking member is slidably provided on the locking seat.

[0011] Optionally, an operating handle is provided at the end of the locking member, and the operating handle protrudes from the top of the main wing.

[0012] Optionally, a positioning rod is further provided at the wing tip, the positioning rod having an extended end extending outward from the wing tip, and a positioning hole corresponding to the positioning rod is further provided on the main wing, and the extended end is inserted into the positioning hole.

[0013] Optionally, a sleeve is installed in the positioning hole, the positioning rod is passed through the sleeve, and the outer wall surface of the positioning rod is in contact with the inner wall surface of the sleeve.

[0014] Optionally, the length direction of the positioning rod is parallel to the length direction of the wing tip.

[0015] In another aspect of an embodiment of the present application, a drone is provided, comprising a drone body and two drone wings of any one of the above-mentioned types, wherein the two drone wings are symmetrically connected to two sides of the drone body.

[0016] The beneficial effects of this application include:

[0017] The present application provides a drone wing and a drone, including a main wing and a wing tip, a locking member is movably provided on the main wing, a locking rod is provided on the wing tip, the end of the locking rod having a limiting protrusion can be inserted into the locking member, the locking member has a first position that cooperates with the limiting protrusion along the axial direction of the locking rod and a second position that releases the abutment with the limiting protrusion along the axial direction of the locking rod, and the locking member is driven to switch between the first position and the second position. The present application ensures that the position and cooperation between them can accurately realize the function of connection and disconnection by movably providing a locking member on the main wing and providing a corresponding locking rod on the wing tip, and by providing a limiting protrusion at the end of the locking rod, the end of the locking rod having the limiting protrusion is inserted into the locking member of the main wing, thereby ensuring the firmness of the connection between the main wing and the wing tip. In addition, the locking member has two key positions: the first position and the second position. In the first position, the locking member cooperates with the limiting protrusion along the axial direction of the locking rod, so that the locking rod cannot be removed from the locking member, thereby ensuring the firmness of the connection between the main wing and the wing tip. When the main wing and the wingtip need to be disassembled, the locking member is driven to switch to the second position, and the abutment with the limiting protrusion along the axial direction of the locking rod is released, thereby allowing the locking rod to be removed from the locking member, that is, the connection between the main wing and the wingtip is released, thereby realizing the rapid disassembly of the main wing and the wingtip.

[0018] In general, by designing the position switching of the locking parts to be more flexible, the firmness of the connection is ensured, and the convenience of disassembly is achieved. No additional tools are required during the disassembly and assembly process, making the entire disassembly and assembly process more efficient. BRIEF DESCRIPTION OF THE DRAWINGS

[0019] In order to more clearly illustrate the technical solutions of the embodiments of the present application, the drawings required for use in the embodiments will be briefly introduced below. It should be understood that the following drawings only show certain embodiments of the present application and therefore should not be regarded as limiting the scope. For ordinary technicians in this field, other related drawings can be obtained based on these drawings without paying creative work.

[0020] Figure 1 An exploded view of a drone wing provided in an embodiment of the present application;

[0021] Figure 2 for Figure 1 A magnified view of middle;

[0022] Figure 3 A schematic diagram of the structure of a locking member and a locking rod connected to each other provided in an embodiment of the present application;

[0023] Figure 4 A schematic diagram of the structure of a locking member provided in an embodiment of the present application;

[0024] Figure 5 A structural schematic diagram of a locking member provided in an embodiment of the present application, which is installed on a locking seat and connected to a locking rod.

[0025] Icons: 100-main wing; 200-wing tip; 300-locking piece; 310-first through hole; 320-second through hole; 330-operating handle; 400-locking rod; 410-limiting protrusion; 500-elastic piece; 600-locking seat; 700-positioning rod; 800-sleeve. DETAILED DESCRIPTION

[0026] In order to make the purpose, technical solution and advantages of the embodiments of the present application clearer, the technical solution in the embodiments of the present application will be clearly and completely described below in conjunction with the drawings in the embodiments of the present application. Obviously, the described embodiments are part of the embodiments of the present application, rather than all the embodiments. The components of the embodiments of the present application described and shown in the drawings here can be arranged and designed in various different configurations.

[0027] Therefore, the following detailed description of the embodiments of the present application provided in the accompanying drawings is not intended to limit the scope of the present application for protection, but merely represents selected embodiments of the present application. It should be noted that, in the absence of conflict, the various features in the embodiments of the present application can be combined with each other, and the combined embodiments are still within the scope of protection of the present application.

[0028] It should be noted that similar reference numerals and letters denote similar items in the following drawings, and therefore, once an item is defined in one drawing, further definition and explanation thereof is not required in subsequent drawings.

[0029] In the description of this application, it should be noted that the terms "upper", "lower", "top", "bottom", "inside", "outside", etc. indicate positions or positional relationships based on the positions or positional relationships shown in the accompanying drawings, or the positions or positional relationships in which the product of the application is usually placed when in use. They are only for the convenience of describing this application and simplifying the description, and do not indicate or imply that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and therefore cannot be understood as a limitation on this application. In addition, the terms "first", "second", etc. are only used to distinguish the description, and cannot be understood as indicating or implying relative importance.

[0030] In the description of this application, it should also be noted that, unless otherwise clearly specified and limited, the terms "set", "install", "connect", and "connect" should be understood in a broad sense, for example, it can be a fixed connection, a detachable connection, or an integral connection; it can be a mechanical connection or an electrical connection; it can be a direct connection, or it can be indirectly connected through an intermediate medium, or it can be the internal communication of two elements. For ordinary technicians in this field, the specific meanings of the above terms in this application can be understood according to specific circumstances.

[0031] With the continuous advancement of fixed-wing UAV technology, a large wingspan design has become an essential feature of this type of UAV. However, one challenge brought about by this design is the increase in the overall size of the UAV, which in turn leads to difficulties in packing and transportation. In order to save space during transportation, the strategy of splitting the wing into multiple detachable parts is often adopted, such as designing a detachable connection between the main wing 100 and the wing tip 200 to facilitate disassembly and transportation.

[0032] However, although this design solves some transportation problems, it introduces new challenges. The main wing 100 and the wing tip 200 usually require additional tools during the disassembly process, which brings inconvenience to the operation and makes the whole process cumbersome, time-consuming and labor-intensive. This additional operation step not only increases the time cost of transportation preparation, but also reduces the operation efficiency, which may affect the rapid deployment and use of the drone.

[0033] In order to solve the cumbersome and time-consuming problems in the disassembly and assembly process of a drone wing, one aspect of an embodiment of the present application provides a drone wing, including a main wing 100 and a wing tip 200, wherein a locking member 300 is movably arranged on the main wing 100, and a locking rod 400 is arranged on the wing tip 200, and the locking rod 400 has an end portion with a limiting protrusion 410 which can be passed through the locking member 300, and the locking member 300 has a first position in which the locking member 300 is axially matched and abutted with the limiting protrusion 410 along the locking rod 400, and a second position in which the locking member 300 is released from the abutment with the limiting protrusion 410 along the axial direction of the locking rod 400, and the locking member 300 is driven to switch between the first position and the second position.

[0034] like Figures 1 to 3 As shown, by movably setting a locking member 300 on the main wing 100 and setting a corresponding locking rod 400 on the wing tip 200, it is ensured that the position and cooperation between them can accurately realize the function of connection and disconnection, and a limiting protrusion 410 is set at the end of the locking rod 400, and the end of the locking rod 400 with the limiting protrusion 410 is inserted into the locking member 300 of the main wing 100, so as to ensure the firmness of the connection between the main wing 100 and the wing tip 200. In addition, the locking member 300 has two key positions: a first position and a second position. In the first position, the locking member 300 and the limiting protrusion 410 are matched and abutted along the axial direction of the locking rod 400, so that the locking rod 400 cannot be removed from the locking member 300, thereby ensuring the firmness of the connection between the main wing 100 and the wing tip 200. When the main wing 100 and the wingtip 200 need to be disassembled, the locking member 300 is driven to switch to the second position, and the abutment with the limiting protrusion 410 is released along the axial direction of the locking rod 400, thereby allowing the locking rod 400 to be removed from the locking member 300, that is, the connection between the main wing 100 and the wingtip 200 is released, thereby achieving rapid disassembly of the main wing 100 and the wingtip 200, facilitating easy replacement and maintenance of the wingtip 200 as a wearing part, and reducing costs.

[0035] In general, by designing the position switching of the locking member 300 to be more flexible, the firmness of the connection is ensured, and the convenience of disassembly is achieved. No additional tools are required during the disassembly and assembly process, making the entire disassembly and assembly process more efficient.

[0036] Optionally, the drone wing further comprises an elastic member 500 connected to the locking member 300 , and the elastic member 500 is used to provide a restoring force to the locking member 300 , so that the locking member 300 has a tendency to remain in the first position.

[0037] Specifically, Figure 1 and Figure 2As shown, when the locking member 300 is located in the first position, the elastic member 500 can be in a slightly deformed state or a normal state. Among them, when the elastic member 500 is in a slightly deformed state, it can provide appropriate force when the locking member 300 needs to be kept in the first position to ensure that the locking rod 400 and the locking member 300 are reliably connected. When the main wing 100 and the wing tip 200 need to be disassembled, the locking member 300 is driven by an external force to switch to the second position to remove the locking rod 400 from the locking member 300. In this process, the elastic member 500 will continue to deform and store energy. When the main wing 100 and the wing tip 200 need to be connected, the locking rod 400 is inserted into the locking member 300 and the external force is removed. In this process, the elastic member 500 begins to release energy and provides a reset force to the locking member 300, so that the locking member 300 switches from the second position to the first position and remains firmly in the first position. At the same time, since the elastic member 500 itself is light in weight, it will not add too much load to the drone and affect its flight condition. In addition, the setting of the elastic member 500 can also play a buffering role, so that when the drone is impacted by external force, the connection between the main wing 100 and the wing tip 200 can remain stable and not easily loosened or fallen off. The drone wing can work stably and reliably during operation and flight, providing reliable protection for the flight mission.

[0038] It should be noted that the elastic member 500 must be able to ensure that an appropriate reset force is provided to the locking member 300 while maintaining appropriate elasticity. Therefore, factors such as the material selection, size and shape of the elastic member 500 need to be considered during the design process to ensure that it can function effectively. Specific types of elastic members 500 may include compression springs, rubber gaskets, elastic plastics, and the like. Among them, compression springs have strong elasticity and restoring force, can provide a stable reset force, and have a strong ability to withstand long-term use in drone wing connections. When selecting the type of elastic member 500, it is necessary to consider the specific design and requirements of the drone wing connection, as well as the characteristics of the working environment, so as to select the most suitable type of elastic member 500 to ensure a stable and reliable connection.

[0039] With this design, the assembly and disassembly of the drone wing becomes more reliable and efficient. The presence of the elastic member 500 enables the locking member 300 to remain in a suitable position when it does not need to be disassembled, thereby reducing the instability of the drone wing connection. In practical applications, this technical solution improves the reliability and efficiency of the drone, and provides more reliable and stable technical support for the widespread application of drones.

[0040] Optionally, a first through hole 310 and a second through hole 320 that are interconnected are opened in the locking member 300, the aperture of the first through hole 310 is larger than the aperture of the second through hole 320, the locking rod 400 is passed through the first through hole 310 and is disposed in the locking member 300, and the limiting protrusion 410 abuts against the opening of the second through hole 320.

[0041] Specifically, Figure 4 As shown, a first through hole 310 and a second through hole 320 that are interconnected are provided on the locking member 300, and these two through holes play an important role in the connection of the drone wing. The aperture of the first through hole 310 is significantly larger than the aperture of the second through hole 320, and such a design helps to ensure that the locking rod 400 can be smoothly passed through and fixed on the locking member 300. Through the first through hole 310, the locking rod 400 can easily pass through the locking member 300 to achieve the connection between the main wing 100 and the wing tip 200. After the connection is completed, the limiting protrusion 410 of the locking rod 400 can abut against the orifice of the second through hole 320, thereby ensuring the stability and safety of the connection. This design ensures that the connection between the locking member 300 and the locking rod 400 has good adaptability and firmness, and effectively prevents the drone wing from loosening or falling off during flight.

[0042] This design not only takes into account the cooperation between the locking member 300 and the locking rod 400, but also makes full use of the design of the through hole to make the connection more firm and reliable. The locking rod 400 is passed from the first through hole 310 to the locking member 300, and the limiting protrusion 410 is abutted against the opening of the second through hole 320, so as to achieve double locking of the drone wing connection. This design not only improves the stability of the connection, but also reduces the risk of loosening or falling off of the connection due to external factors. In practical applications, it is necessary to consider the precise processing of the through hole and the appropriate size of the locking rod 400 to ensure that the cooperation between the locking member 300 and the locking rod 400 can achieve the best effect. The size and position of the through hole need to be precisely designed to meet the requirements of the penetration and limiting of the locking rod 400. At the same time, the size and shape of the locking rod 400 also need to match the through hole to ensure the tightness and stability of the connection.

[0043] In general, this design significantly improves the connection effect of the drone wing. The through-hole design makes the connection between the locking member 300 and the locking rod 400 more secure and reliable, effectively preventing the drone wing from loosening or falling off during operation. The implementation of this technical solution not only simplifies the disassembly and connection process of the drone wing, but also improves the flight safety and stability of the drone, providing more reliable and effective technical support for the widespread application of drones.

[0044] Optionally, the limiting protrusion 410 is a conical protrusion, and the conical protrusion gradually shrinks along the penetration direction of the locking rod 400.

[0045] Specifically, Figure 3 As shown, the conical protrusion gradually decreases along the direction of the locking rod 400 passing through. When the locking rod 400 passes through the locking member 300, the smaller end face of the conical protrusion first passes through the locking member 300. As a result, the locking rod 400 can pass through the first through hole 310 in the locking member 300 relatively easily. In addition, the larger end face of the conical protrusion abuts against the opening of the second through hole 320, and the abutment area is larger, so that the position of the locking rod 400 can be more firmly fixed to ensure the stability of the connection. It should be noted that the design of the conical protrusion must meet the requirements of the passing and limiting of the locking rod 400, and the stability and reliability of the connection of the drone wing must also be considered. Therefore, precise processing is required during the implementation process to ensure that the conical protrusion can play the best limiting effect.

[0046] Optionally, a locking seat 600 is provided on the main wing 100 , and the locking member 300 is slidably disposed on the locking seat 600 .

[0047] Specifically, Figure 1 and Figure 5 As shown, the main wing 100 is also provided with a locking seat 600, which provides a stable support platform for the locking member 300, further enhancing the connection stability and the convenience of disassembly and assembly of the drone wing. The locking member 300 is slidably arranged on the locking seat 600, and the locking seat 600 is fixedly arranged on the main wing 100, so that the locking member 300 can stably slide relative to the main wing 100 to achieve the stable switching of the locking member 300 between the first position and the second position, thereby ensuring the stability and reliability of the connection and disassembly process of the main wing 100 and the wing tip 200. The locking seat 600 can be detachably connected to the main wing 100 by means of bolts or the like, which can ensure the stable and reliable connection between the locking seat 600 and the main wing 100 on the one hand, and on the other hand, the locking seat 600 can be flexibly installed and disassembled, which is convenient for maintenance and replacement.

[0048] Optionally, an operating handle 330 is provided at the end of the locking member 300 , and the operating handle 330 protrudes from the top of the main wing 100 .

[0049] Specifically, Figure 4As shown, an operating handle 330 is provided at the end of the locking member 300. This design further improves the convenience of operating the locking member 300. The operating handle 330 protrudes from the top of the main wing 100, so that the operator can easily reach and operate the locking member 300 without additional tools. This design not only simplifies the disassembly and assembly process of the drone wing, but also improves the comfort and efficiency of the operation. It is worth noting that the protruding height of the operating handle 330 should be greater than or equal to the distance from the first position to the second position to ensure that the operating handle 330 does not hinder the sliding of the locking member 300 when the locking member 300 is switched from the first position to the second position.

[0050] In addition, the portion of the locking member 300 other than the operating handle 330 and the locking seat 600 can be arranged in the skin of the main wing 100. Such a design not only makes the appearance of the drone wing more beautiful, but also makes the locking member 300 and the locking seat 600 hidden in the skin less susceptible to damage or pollution from the external environment, effectively extending their service life. At the same time, this design is also conducive to reducing the impact of the external structure on the aerodynamic performance of the drone wing, further improving flight efficiency and performance stability. Therefore, the hidden locking member 300 and the locking seat 600 not only achieve a beautiful appearance, but also improve the overall quality and reliability of the drone wing.

[0051] Optionally, a positioning rod 700 is further provided at the wing tip 200 , and the positioning rod 700 has an extended end extending outward from the wing tip 200 , and a positioning hole corresponding to the positioning rod 700 is also provided on the main wing 100 , and the extended end is inserted into the positioning hole.

[0052] Specifically, Figure 1 and Figure 2As shown, the positioning rod 700 has an extended end extending outward from the wing tip 200, and the extended end usually has a certain length. In the design of the main wing 100, a positioning hole corresponding to the positioning rod 700 is provided to ensure that the extended end can be firmly inserted into the positioning hole, that is, the positioning rod 700 can be accurately inserted into the main wing 100. Such a design is used for positioning guidance on the one hand, so that when the positioning rod 700 is inserted into the positioning hole, the locking rod 400 can also be accurately inserted into the locking member 300; on the other hand, through the cooperation between the positioning rod 700 and the positioning hole, the locking rod 400 can be prevented from rotating or twisting in the locking member 300, thereby preventing the main wing 100 from being connected to the wing tip 200. It should be noted that the positioning rod 700 can be one or more. When there are multiple positioning rods 700, such as 2 or 4, the positioning rods 700 should be symmetrically arranged on both sides of the locking rod 400 along the width of the wing tip 200. At this time, the positioning holes are also correspondingly arranged on both sides of the locking member 300, so as to achieve accurate positioning and connection of the main wing 100 and the wing tip 200 while enhancing the stability and reliability of the connection, thereby effectively preventing the loosening or falling off of the drone wing during operation. It should also be noted that the positioning rod 700 is usually made of materials such as carbon tubes, which are lightweight and high-strength, can meet the material requirements of the drone wing connection, and provide good stability and support.

[0053] Optionally, a sleeve 800 is installed in the positioning hole, the positioning rod 700 is passed through the sleeve 800 , and the outer wall surface of the positioning rod 700 is in contact with the inner wall surface of the sleeve 800 .

[0054] Specifically, Figure 1 and Figure 2 As shown, a sleeve 800 is installed in the positioning hole, and the number of the sleeves 800 corresponds to the number of the positioning rods 700. By inserting the positioning rod 700 into the sleeve 800, and the outer wall surface of the positioning rod 700 is attached to the inner wall surface of the sleeve 800, this design ensures that the positioning rod 700 can be accurately inserted into the sleeve 800 and maintains a close fit with the sleeve 800, so as to enhance the stability and firmness of the connection between the main wing 100 and the wing tip 200. Through the setting of the positioning hole and the sleeve 800, as well as the cooperation between the positioning rod 700 and the sleeve 800, and ensuring the consistency of the center distance and relative position between the positioning rods 700, the stability and reliability of the UAV in flight are improved, and the accurate alignment and interchange consistency between the main wing 100 and the wing tip 200 are achieved, providing more reliable and stable technical support for the wide application of UAVs.

[0055] Optionally, the length direction of the positioning rod 700 is parallel to the length direction of the wing tip 200 .

[0056] Specifically, multiple frames are provided in the main wing 100 and the wing tip 200, and the positioning rod 700 is vertically connected to the multiple frames of the wing tip 200. Positioning holes are provided in the multiple frames of the main wing 100, and the connecting line of the multiple positioning holes is perpendicular to the frames, that is, the sleeve 800 installed in the positioning hole is vertically connected to the multiple frames, so that the two ends of the positioning rod 700 are respectively vertically inserted into the wing tip 200 and the main wing 100, that is, the length direction of the positioning rod 700 is parallel to the length direction of the wing tip 200 or the main wing 100. As an important component of the connection, the positioning rod 700 can effectively fix the position of each part of the drone wing by vertically inserting into the wing tip 200 and the main wing 100, preventing them from relative movement or distortion during flight, increasing the firmness of the connection, and improving the stability and flight performance of the drone wing during flight.

[0057] The specific working process is as follows:

[0058] When the main wing 100 and the wing tip 200 are not connected, the locking member 300 is located at the first position. When the main wing 100 and the wing tip 200 need to be disconnected, the positioning rod 700 is inserted into the sleeve 800. At this time, the smaller end face of the conical protrusion of the locking rod 400 first passes through the locking member 300, and drives the locking member 300 to slide from the first position to the second position, so that the larger end face of the conical protrusion also passes through the first through hole 310 of the locking member 300. In this process, the elastic member 500 connected to the locking member 300 is deformed. After the conical protrusion passes through the locking member 300, the locking member 300 is restored to the first position under the restoring force of the elastic member 500, so that the conical protrusion abuts against the opening of the second through hole 320 of the locking member 300, thereby completing the reliable connection between the locking rod 400 and the locking member 300. When it is necessary to disconnect the main wing 100 and the wing tip 200, the operating handle 330 is pressed so that the locking member 300 compresses the elastic member 500 and slides from the first position to the second position. At this time, the conical protrusion is released from the abutment with the opening of the second through hole 320, and the position of the conical protrusion corresponds to the position of the first through hole 310. Thus, the locking rod 400 can be removed from the locking member 300, and the positioning rod 700 can also be removed from the sleeve 800, thereby completing the rapid disassembly of the main wing 100 and the wing tip 200.

[0059] Another aspect of the embodiment of the present application provides a drone, including a drone body and two drone wings of any of the above, wherein the two drone wings are symmetrically connected to the two sides of the drone body. Through the symmetrical connection, a stable and reliable connection is achieved between the drone wings and the drone body, thereby ensuring the balance and stability of the drone during flight. This design not only improves the flight performance and maneuverability of the drone, but also enhances the structural stability and safety of the drone. Through reasonable arrangement and optimized design, the connection between the two drone wings and the drone body can give full play to its function, providing more reliable and efficient technical support for the flight of the drone.

[0060] The above description is only the preferred embodiment of the present application and is not intended to limit the present application. For those skilled in the art, the present application may have various modifications and variations. Any modification, equivalent replacement, improvement, etc. made within the spirit and principle of the present application shall be included in the protection scope of the present application.

Claims

1. A drone wing, characterized in that: The invention comprises a main wing (100) and a wing tip (200), wherein a locking member (300) is movably arranged on the main wing (100), and a locking rod (400) is arranged on the wing tip (200); the locking rod (400) has an end portion with a limiting protrusion (410) which can be passed through the locking member (300); the locking member (300) has a first position in which the locking member is axially matched with the limiting protrusion (410) and abutted along the axial direction of the locking rod (400); and a second position in which the locking member is axially released from the abutment with the limiting protrusion (410) and the locking member (300) is driven to switch between the first position and the second position.

2. The drone wing according to claim 1, characterized in that: The drone wing further comprises an elastic member (500) connected to the locking member (300), wherein the elastic member (500) is used to provide a restoring force to the locking member (300) so that the locking member (300) has a tendency to remain in the first position.

3. The drone wing according to claim 1 or 2, characterized in that: The locking member (300) is provided with a first through hole (310) and a second through hole (320) which are interconnected, the diameter of the first through hole (310) is larger than the diameter of the second through hole (320), the locking rod (400) is passed through the first through hole (310) and is arranged in the locking member (300), and the limiting protrusion (410) is abutted against the opening of the second through hole (320).

4. The drone wing according to claim 1 or 2, characterized in that: The limiting protrusion (410) is a conical protrusion, and the conical protrusion gradually shrinks along the penetration direction of the locking rod (400).

5. The drone wing according to claim 1 or 2, characterized in that: The main wing (100) is provided with a locking seat (600), and the locking member (300) is slidably arranged on the locking seat (600).

6. The drone wing according to claim 1 or 2, characterized in that: An operating handle (330) is provided at the end of the locking member (300), and the operating handle (330) protrudes from the top of the main wing (100).

7. The drone wing according to claim 1 or 2, characterized in that: A positioning rod (700) is also provided on the wing tip (200), and the positioning rod (700) has an extended end extending outward from the wing tip (200). A positioning hole corresponding to the positioning rod (700) is also provided on the main wing (100), and the extended end is inserted into the positioning hole.

8. The drone wing according to claim 7, characterized in that: A sleeve (800) is installed in the positioning hole, the positioning rod (700) is inserted into the sleeve (800), and the outer wall surface of the positioning rod (700) is in contact with the inner wall surface of the sleeve (800).

9. The drone wing according to claim 7, characterized in that: The length direction of the positioning rod (700) is parallel to the length direction of the wing tip (200).

10. A drone, characterized in that: It comprises a drone body and two drone wings according to any one of claims 1 to 9, wherein the two drone wings are symmetrically connected to two sides of the drone body.

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