A quick-release drone with integrated adjustment device

Abstract

This invention provides a quick-release drone with an integrated adjustment device, belonging to the field of drone technology. It includes a propeller mount, a power mount, a quick-release device, and an adjustment device. The quick-release device includes at least two cooperating irregularly shaped parts and at least one elastic fixing member. The at least two irregularly shaped parts are respectively disposed on the propeller mount and the power mount, and the elastic fixing member is disposed on one of the propeller mount and the power mount. The other propeller mount and the power mount have a fixing groove. The adjustment device is disposed between the propeller mount and the power mount and is used to adjust the gap between the opposite sides of the at least two irregularly shaped parts. This arrangement allows the gap between the propeller mount and the power mount to be compressed again when the assembly precision between them decreases, thus ensuring the assembly precision of the propeller mount and the power mount.

Description

Technical Field

[0001] This invention belongs to the field of unmanned aerial vehicle (UAV) technology, and specifically relates to a quick-release UAV with an integrated adjustment device. Background Technology

[0002] Unmanned aerial vehicles (UAVs), also known as drones, are unmanned aircraft controlled by radio remote control equipment and onboard program control devices, or operated autonomously by an onboard computer, either completely or intermittently. Compared to manned aircraft, the real demand for UAVs lies in industry applications. Currently, UAVs are widely used in aerial photography, agriculture, plant protection, miniature selfies, express delivery, disaster relief, wildlife observation, infectious disease monitoring, surveying, news reporting, power line inspection, disaster relief, film and television shooting, and creating romantic scenes, greatly expanding their uses. Developed countries are also actively expanding industry applications and developing UAV technology.

[0003] In drones, the propeller base and the propeller blades are both important components. How the propeller base and the propeller blades are connected directly affects the service life of the drone. In the existing technology, a corresponding quick-release structure is usually arranged between the propeller base and the propeller blades to complete the quick assembly and disassembly of the propeller base and the propeller blades.

[0004] Then, existing quick-release structures usually use high-precision assembly parts. That is, after the two parts in the quick-release structure are matched, the blade base and blade will be fixed directly. As a result, when the quick-release structure is disassembled and assembled multiple times, the parts are prone to wear. This wear leads to insufficient precision in the assembly of the parts, resulting in misalignment between the parts. This, in turn, increases the vibration amplitude of the blades during the flight of the drone, thereby reducing the flight life of the drone. Summary of the Invention

[0005] Based on this, the purpose of the present invention is to provide a quick-release drone with an integrated adjustment device to solve the technical problem in the prior art where existing quick-release structures typically use high-precision assembly parts. After multiple disassemblies and reassemblies, the parts are prone to wear, resulting in insufficient precision during assembly due to wear. This leads to misalignment between parts, which in turn increases the vibration amplitude of the drone's propellers during flight, thereby reducing the drone's flight life.

[0006] The present invention proposes a quick-release drone with an integrated adjustment device, comprising a blade mounting base for connecting the blades, a power mounting base for connecting to a power source, a quick-release device, and an adjustment device.

[0007] The blade mounting base and the power mounting base are movably connected. The quick-release device includes at least two cooperating irregularly shaped parts and at least one elastic fixing part. The at least two irregularly shaped parts are respectively disposed on the blade mounting base and the power mounting base, so that when one of the blade mounting base and the power mounting base moves relative to the other, the at least two irregularly shaped parts are interlocked to restrict the first direction of movement between the blade mounting base and the power mounting base.

[0008] The elastic fastener is disposed on one of the blade mounting base and the power mounting base. The other irregularly shaped part on the blade mounting base and the power mounting base is provided with a fixing groove for the fixing part of the elastic fastener to pass through. When the two irregularly shaped parts are engaged with each other, the fixing part extends into the fixing groove to restrict the second movement direction between the blade mounting base and the power mounting base. The second movement direction is different from the first movement direction.

[0009] The adjustment device is located between the blade fixing seat and the power fixing seat, and is used to adjust the gap size between the opposite sides of at least two of the irregular parts.

[0010] Furthermore, the quick-release device includes at least one first irregularly shaped component and at least one second irregularly shaped component, the first irregularly shaped component and the second irregularly shaped component being respectively disposed on the blade fixing seat and the power fixing seat;

[0011] The first irregularly shaped component has a first snap-fit ​​space on one side opposite to the blade fixing seat for accommodating the second irregularly shaped component, and the second irregularly shaped component has a second snap-fit ​​space on one side opposite to the power fixing seat for accommodating the first irregularly shaped component.

[0012] Furthermore, the first irregularly shaped part and the second irregularly shaped part each have a first inclined portion and a second inclined portion on their opposite sides;

[0013] The tilting direction of the first tilting portion is opposite to that of the tilting direction of the second tilting portion, so that when one of the blade fixing seat and the power fixing seat moves relative to the other, the gap between the blade fixing seat and the power fixing seat gradually decreases from large to small.

[0014] Furthermore, the quick-release device includes multiple first irregularly shaped parts and multiple second irregularly shaped parts;

[0015] Multiple first irregular-shaped parts are spaced apart on one side edge of the blade fixing seat with the center of the blade fixing seat as the origin, and multiple second irregular-shaped parts are spaced apart on one side edge of the power fixing seat with the center of the power fixing seat as the origin;

[0016] Each of the first irregularly shaped components has a first irregularly shaped component arranged opposite to it, and there is a gap between the two first irregularly shaped components arranged opposite to it to form an active space for the power fixing seat and the plurality of second irregularly shaped components to move, so that when the power fixing seat extends into the active space to move, each second irregularly shaped component and each first irregularly shaped component are engaged with each other.

[0017] Furthermore, the quick-release device includes multiple elastic fasteners, all of which are disposed on the blade fixing seat;

[0018] Each of the first irregular-shaped parts is provided with the fixing groove, and each fixing groove is arranged opposite to each of the elastic fixing parts, so that when each of the second irregular-shaped parts and each of the first irregular-shaped parts are engaged with each other, the fixing part of each elastic fixing part extends into a fixing groove for engagement.

[0019] Furthermore, the elastic fastener also includes a lever arm portion, which passes through one side of the blade fixing seat and extends outward.

[0020] Furthermore, the adjustment device includes an adjustment member, a first boss and a second boss, the first boss and the second boss being arranged opposite to each other and respectively disposed on the blade fixing seat and the power fixing seat;

[0021] The adjusting member is movably connected to one of the blade fixing seat and the power fixing seat, and is used to drive one of the first boss or the second boss to move in order to adjust the gap size between the first irregular part and the second irregular part.

[0022] Furthermore, the adjusting member is disposed within the blade fixing seat, and the adjusting member and the blade fixing seat are threadedly connected.

[0023] Furthermore, the adjusting component includes an adjusting part and a retaining tooth part, and the adjusting part is threadedly connected to the blade fixing seat;

[0024] The adjustment device further includes at least one limiting member, which is detachably connected to the blade fixing seat to move toward and engage with the locking tooth portion.

[0025] Furthermore, the adjusting device also includes a plurality of limiting members, and at least two of the plurality of limiting members are arranged opposite to each other.

[0026] Compared with the prior art, the beneficial effects of the present invention are as follows:

[0027] In the quick-release drone with integrated adjustment device provided by this invention, a shaped component on the propeller mounting base and a shaped component on the power mounting base are interlocked to restrict the first direction of movement of the propeller mounting base and the power mounting base. After the first and second interlocking components are engaged, an elastic fixing component extends into the fixing groove to restrict the second direction of movement between the propeller mounting base and the power mounting base. By restricting the first and second directions of movement, the propeller mounting base and the power mounting base are basically fixed. However, due to the repeated assembly, the assembly accuracy between the two shaped components decreases, resulting in a misalignment between the propeller mounting base and the power mounting base. The quick-release drone also includes an adjustment device located on the propeller mounting base. Between the propeller mount and the power mount, the gap between the opposite sides of at least two irregularly shaped parts is adjusted. This allows the gap between the propeller mount and the power mount to be compressed again when the assembly accuracy between them decreases, thus ensuring the assembly accuracy of the propeller mount and the power mount. Furthermore, it eliminates the need to consider the initial accuracy of the propeller mount and the power mount. This solves the technical problem in existing quick-release structures where high-precision assembly parts are commonly used. After repeated disassembly and assembly, the parts are prone to wear, leading to insufficient precision during assembly and resulting in misalignment between parts. This, in turn, increases the vibration amplitude of the propeller blades during flight, reducing the drone's flight life. Attached Figure Description

[0028] Figure 1 This is a perspective view of a quick-release drone with an integrated adjustment device according to an embodiment of the present invention;

[0029] Figure 2 This is a top view of a quick-release drone with an integrated adjustment device according to an embodiment of the present invention.

[0030] Figure 3 for Figure 2 AA section view;

[0031] Figure 4 An exploded view of a quick-release drone with an integrated adjustment device according to an embodiment of the present invention;

[0032] Figure 5 This is a diagram showing the usage state of the quick-release device in one embodiment of the present invention;

[0033] Figure 6 This is a perspective view of the blade fixing seat in one embodiment of the present invention;

[0034] Figure 7 This is a perspective view of the power mounting base in one embodiment of the present invention.

[0035] Figure label:

[0036] 100, Blade holder; 200, Power holder; 300, Quick release device; 310, First irregular part; 311, First inclined part; 320, Second irregular part; 321, Second inclined part; 330, Elastic fastener; 331, Fixing part; 332, Lever arm; 340, Fixing groove; 350, First snap-fit ​​space; 360, Second snap-fit ​​space; 400, Adjustment device; 410, Adjustment part; 411, Adjustment part; 412, Snap-fit ​​tooth; 420, First boss; 430, Second boss; 440, Limiting part. Detailed Implementation

[0037] To facilitate understanding of the present invention, a more complete description will be given below with reference to the accompanying drawings. Several embodiments of the invention are illustrated in the drawings. However, the invention can be implemented in many different forms and is not limited to the embodiments described herein. Rather, these embodiments are provided so that this disclosure will be thorough and complete.

[0038] It should be noted that when a component is said to be "fixed to" another component, it can be directly on the other component or there may be an intervening component. When a component is said to be "connected to" another component, it can be directly connected to the other component or there may be an intervening component. The terms "vertical," "horizontal," "left," "right," and similar expressions used in this document are for illustrative purposes only.

[0039] Unless otherwise defined, all technical and scientific terms used herein have the same meaning as commonly understood by one of ordinary skill in the art to which this invention pertains. The terminology used herein in the description of the invention is for the purpose of describing particular embodiments only and is not intended to be limiting of the invention. The term "and / or" as used herein includes any and all combinations of one or more of the associated listed items.

[0040] Please see Figures 1-7 The image shows a quick-release drone with an integrated adjustment device provided in an embodiment of the present invention, including a blade mounting base 100 for connecting the blades, a power mounting base 200 for connecting to a power source, a quick-release device 300, and an adjustment device 400.

[0041] It should be noted that in this embodiment, the propellers in the UAV will be directly mounted on the propeller mounting base 100. The mounting method can be bolts or other fixing methods. Similarly, the power mounting base 200 will be directly connected to the power output end in the UAV.

[0042] To avoid precision issues and misalignment between components during blade assembly, in this embodiment, the blade mounting base 100 and the power mounting base 200 are movably connected. The quick-release device 300 includes at least two cooperating irregularly shaped parts and at least one elastic fixing part 330. The at least two irregularly shaped parts are respectively disposed on the blade mounting base 100 and the power mounting base 200, so that when one of the blade mounting base 100 and the power mounting base 200 moves relative to the other, the at least two irregularly shaped parts are interlocked to restrict the first direction of movement between the blade mounting base 100 and the power mounting base 200.

[0043] The elastic fastener 330 is provided on one of the blade mounting base 100 and the power mounting base 200. The other irregular part on the blade mounting base 100 and the power mounting base 200 is provided with a fixing groove 340 for the fixing part 331 in the elastic fastener 330 to pass through. When the two irregular parts are engaged with each other, the fixing part 331 extends into the fixing groove 340 to restrict the second movement direction between the blade mounting base 100 and the power mounting base 200. The second movement direction is different from the first movement direction.

[0044] The adjusting device 400 is located between the blade fixing seat 100 and the power fixing seat 200, and is used to adjust the gap size between the opposite sides of at least two irregular parts.

[0045] In other words, in this embodiment, when it is necessary to assemble the blade, the blade and the blade mounting base 100 are first installed to form a whole. After the blade mounting base 100 and the power mounting base 200 are assembled, the blade will be installed.

[0046] In some preferred embodiments, the central cross-section of the blade mounting base 100 is circular, and its left and right edges extend outward to form an expanded surface that can be connected to a shaped component. Correspondingly, the power mounting base 200 is circular, and the central cross-sections of the power mounting base 200 and the blade mounting base 100 correspond. When assembling the blade mounting base 100 and the power mounting base 200, the central part of the blade mounting base 100 corresponds to and moves with the power mounting base 200. This movement can be rotation. During rotation, a shaped component on the blade mounting base 100 and a shaped component on the power mounting base 200... The two parts will be interlocked, thereby restricting the first direction of movement of the blade fixing seat 100 and the power fixing seat 200. The first direction of movement can be vertical. After the first and second interlocking parts are interlocked, the elastic fixing part 330 in this embodiment extends into the fixing groove 340, thereby restricting the second direction of movement between the blade fixing seat 100 and the power fixing seat 200. The second direction of movement can be a horizontal rotation direction. By restricting the first and second directions of movement, the blade fixing seat 100 and the power fixing seat 200 are basically fixed.

[0047] However, in some practical situations, the repeated assembly can reduce the assembly precision between the two irregularly shaped parts, causing misalignment between the propeller mounting base 100 and the power mounting base 200. Therefore, in this embodiment, the quick-release drone also includes an adjustment device 400, located between the propeller mounting base 100 and the power mounting base 200. This adjustment device 400 is used to adjust the gap between the opposite sides of at least two irregularly shaped parts, so that when the assembly precision between the propeller mounting base 100 and the power mounting base 200 decreases, the adjustment function of the adjustment device 400 can be used to readjust the assembly precision between the propeller mounting base 100 and the power mounting base 200. The gap between the power mounting bases 200 is compressed to ensure the assembly accuracy between the propeller mounting base 100 and the power mounting base 200. Furthermore, it eliminates the need to consider the accuracy of the propeller mounting base 100 and the power mounting base 200 in the initial state. This solves the technical problem in existing quick-release structures where high-precision assembly parts are typically used. After multiple disassemblies and reassemblies, the parts are prone to wear, leading to insufficient precision during assembly due to wear. This results in misalignment between parts, which in turn increases the vibration amplitude of the propeller blades during flight, thus reducing the flight life of the UAV.

[0048] Furthermore, for a better understanding of this case, please refer to [link / reference]. Figure 4As shown, in this embodiment, the quick-release device 300 includes at least one first irregularly shaped component 310 and at least one second irregularly shaped component 320. The first irregularly shaped component 310 and the second irregularly shaped component 320 are respectively disposed on the blade fixing seat 100 and the power fixing seat 200. A first snap-fit ​​space 350 for accommodating the second irregularly shaped component 320 is provided on one side of the first irregularly shaped component 310 and the opposite side of the blade fixing seat 100. A second snap-fit ​​space 360 ​​for accommodating the first irregularly shaped component 310 is provided on one side of the second irregularly shaped component 320 and the opposite side of the power fixing seat 200.

[0049] It should be noted that the first irregular part 310 and the second irregular part 320 are not limited to a certain number of irregular parts, and can be other numbers. Specifically, when assembling the power mounting base 200 and the blade mounting base 100, the second irregular part 320 can be snapped into place using the first snap-fit ​​space 350, and the first irregular part 310 can be snapped into place using the second snap-fit ​​space 360.

[0050] In some other preferred embodiments, the first irregular member 310 and the second irregular member 320 each include a first inclined portion 311 and a second inclined portion 321 on opposite sides. The inclination directions of the first inclined portion 311 and the second inclined portion 321 are opposite, so that when one of the blade fixing seat 100 and the power fixing seat 200 moves relative to the other, the gap between the blade fixing seat 100 and the power fixing seat 200 gradually decreases. Specifically, please refer to... Figure 4 As shown, when the first irregular part 310 and the second irregular part 320 are assembled together, the blade fixing seat 100 and the power fixing seat 200 will become increasingly close together during rotation due to the relative inclined surfaces of the first inclined part 311 and the second inclined part 321.

[0051] Furthermore, to ensure the stability of the blade mounting base 100 and the power mounting base 200, in some practical situations, the quick-release device 300 includes multiple first irregularly shaped parts 310 and multiple second irregularly shaped parts 320. The multiple first irregularly shaped parts 310 are spaced apart on one side edge of the blade mounting base 100 with the center of the blade mounting base 100 as the origin, and the multiple second irregularly shaped parts 320 are spaced apart on one side edge of the power mounting base 200 with the center of the power mounting base 200 as the origin. Each first irregularly shaped part 310 has one first irregularly shaped part 310 opposite to it, and there is a gap between the two oppositely arranged first irregularly shaped parts 310 to form an active space for the power mounting base 200 and the multiple second irregularly shaped parts 320 to move. When the power mounting base 200 extends into the active space to move, each second irregularly shaped part 320 and each first irregularly shaped part 310 are interlocked with each other.

[0052] It should be noted that the active space can correspond to the middle part of the blade fixing seat 100, and the number of multiple first irregular parts 310 and multiple second irregular parts 320 can both be two. In some preferred embodiments, the two first irregular parts 310 are symmetrically arranged on both sides of the blade fixing seat 100, and similarly, the two second irregular parts 320 are also symmetrically arranged on both sides of the power fixing seat 200.

[0053] Specifically, with the length direction of the second irregular part 320 as the target, the thickness of the second irregular part 320 gradually decreases from large to small, and the cross-section of the second irregular part 320 also gradually decreases from large to small along with the thickness. In some practical cases, after the first irregular part 310 and the second irregular part 320 are snapped together, they are snapped together with the first irregular part 310 at the thickest point of the second irregular part 320, which is also the point with the largest cross-section. This ensures the snapping strength of the first irregular part 310 and the second irregular part 320 while reducing costs and saving processing steps. It should be noted that the length direction of the second irregular part 320 extends along the length direction of the power fixing seat 200.

[0054] In addition, the quick-release device 300 includes a plurality of elastic fasteners 330, all of which are provided on the blade fixing seat 100. Each first irregular part 310 is provided with a fixing groove 340, and each fixing groove 340 is arranged opposite to each elastic fastener 330 so that when each second irregular part 320 and each first irregular part 310 are engaged with each other, the fixing part 331 of each elastic fastener 330 extends into a fixing groove 340 for engagement. Specifically, the fixing groove 340 may be provided on the first irregular part 310.

[0055] Furthermore, the elastic fastener 330 also includes a lever arm 332, which passes through one side of the blade fixing seat 100 and extends outward.

[0056] Specifically, the elastic fastener 330 also has an elastic part, which can be a spring, and the fastener 331 and the lever arm 332 are fixedly connected to each other to form an L-structure.

[0057] In addition, to facilitate the adjustment of the gap between the blade mounting base 100 and the power mounting base 200, the adjustment device 400 includes an adjustment member 410, a first boss 420 and a second boss 430, the first boss 420 and the second boss 430 being arranged opposite to each other and respectively disposed on the blade mounting base 100 and the power mounting base 200.

[0058] The adjusting member 410 is movably connected to one of the blade fixing seat 100 and the power fixing seat 200, and is used to drive one of the first boss 420 or the second boss 430 to move in order to adjust the gap size between the first irregular member 310 and the second irregular member 320.

[0059] The adjusting member 410 is disposed within the blade fixing seat 100, and the adjusting member 410 and the blade fixing seat 100 are threadedly connected. The adjusting member 410 includes an adjusting part 411 and a locking tooth part 412, and the adjusting part 411 and the blade fixing seat 100 are threadedly connected. The adjusting device 400 also includes at least one limiting member 440, which is detachably connected to the blade fixing seat 100 for moving toward and locking toward the locking tooth part 412.

[0060] In some preferred embodiments, to ensure its stability, the adjusting device 400 further includes a plurality of limiting members 440, and at least two of the plurality of limiting members 440 are arranged opposite to each other.

[0061] In other words, after the blade mounting base 100 and the power mounting base 200 are assembled, the locking member 440 engages the locking teeth on the locking tooth part 412 to complete the locking and fixation, thereby further improving stability.

[0062] In summary, the quick-release drone with integrated adjustment device provided in an embodiment of the present invention has at least the following advantages compared with the disassembly methods of drones in the prior art:

[0063] In the quick-release drone of the integrated adjustment device 400 provided by the present invention, a shaped component on the propeller fixing seat 100 and a shaped component on the power fixing seat 200 are interlocked to restrict the first direction of movement of the propeller fixing seat 100 and the power fixing seat 200. After the first and second interlocking components are engaged, the elastic fixing component 330 extends into the fixing groove 340 to restrict the second direction of movement between the propeller fixing seat 100 and the power fixing seat 200. By restricting the first and second directions of movement, the propeller fixing seat 100 and the power fixing seat 200 are basically fixed. Due to the repeated assembly, the assembly accuracy between the two shaped components decreases, resulting in a misalignment between the propeller fixing seat 100 and the power fixing seat 200. The quick-release drone also includes an adjustment device 400, which is designed with... Between the propeller mounting base 100 and the power mounting base 200, the gap between the opposite sides of at least two irregularly shaped parts is adjusted. When the assembly accuracy between the propeller mounting base 100 and the power mounting base 200 decreases, the gap between the propeller mounting base 100 and the power mounting base 200 can be compressed again using the adjustment function of the adjustment device 400 to ensure the assembly accuracy between the propeller mounting base 100 and the power mounting base 200. Furthermore, it is not necessary to consider the accuracy of the propeller mounting base 100 and the power mounting base 200 in the initial state. This solves the technical problem in the prior art where existing quick-release structures typically use high-precision assembly parts. After multiple disassemblies and reassemblies, the parts are prone to wear, resulting in insufficient accuracy during assembly due to wear. This leads to misalignment between the parts, which in turn increases the vibration amplitude of the propeller blades during the flight of the UAV, thereby reducing the flight life of the UAV.

[0064] In the description of this specification, references to terms such as "one embodiment," "some embodiments," "example," "specific example," or "some examples," etc., indicate that a specific feature, structure, material, or characteristic described in that embodiment or example is included in at least one embodiment or example of the invention. In this specification, the illustrative expressions of the above terms do not necessarily refer to the same embodiment or example. Furthermore, the specific features, structures, materials, or characteristics described can be referred to in any suitable manner in one or more embodiments or examples.

[0065] The above embodiments merely illustrate several implementation methods of the present invention, and their descriptions are relatively specific and detailed, but they should not be construed as limiting the scope of the present invention. It should be noted that those skilled in the art can make various modifications and improvements without departing from the concept of the present invention, and these all fall within the protection scope of the present invention. Therefore, the protection scope of this patent should be determined by the appended claims.

Claims

1. A quick-release drone with an integrated adjustment device, characterized in that, It includes a blade mounting base for connecting the blades, a power mounting base for connecting to the power source, a quick-release device, and an adjustment device. The blade mounting base and the power mounting base are movably connected. The quick-release device includes at least two cooperating irregularly shaped parts and at least one elastic fixing part. The at least two irregularly shaped parts are respectively disposed on the blade mounting base and the power mounting base, so that when one of the blade mounting base and the power mounting base moves relative to the other, the at least two irregularly shaped parts are interlocked to restrict the first direction of movement between the blade mounting base and the power mounting base. The elastic fastener is disposed on one of the blade mounting base and the power mounting base. The other irregularly shaped part on the blade mounting base and the power mounting base is provided with a fixing groove for the fixing part of the elastic fastener to pass through. When the two irregularly shaped parts are engaged with each other, the fixing part extends into the fixing groove to restrict the second movement direction between the blade mounting base and the power mounting base. The second movement direction is different from the first movement direction. The adjusting device is located between the blade fixing seat and the power fixing seat, and is used to adjust the gap size between the opposite sides of at least two of the irregular parts; The quick-release device includes at least one first irregularly shaped component and at least one second irregularly shaped component, the first irregularly shaped component and the second irregularly shaped component being respectively disposed on the blade fixing seat and the power fixing seat; Wherein, a first snap-fit ​​space is provided on one side of the first irregular part and the opposite side of the blade fixing seat for accommodating the second irregular part, and a second snap-fit ​​space is provided on one side of the second irregular part and the opposite side of the power fixing seat for accommodating the first irregular part. The adjustment device includes an adjustment component, a first boss and a second boss, the first boss and the second boss are arranged opposite to each other and are respectively provided on the blade fixing seat and the power fixing seat; The adjusting member is movably connected to one of the blade fixing seat and the power fixing seat, and is used to drive one of the first boss or the second boss to move in order to adjust the gap size between the first irregular part and the second irregular part.

2. The quick-release UAV with integrated adjustment device according to claim 1, characterized in that, The first irregularly shaped part and the second irregularly shaped part each have a first inclined portion and a second inclined portion on their opposite sides; The tilting direction of the first tilting portion is opposite to that of the tilting direction of the second tilting portion, so that when one of the blade fixing seat and the power fixing seat moves relative to the other, the gap between the blade fixing seat and the power fixing seat gradually decreases from large to small.

3. The quick-release UAV with integrated adjustment device according to claim 2, characterized in that, The quick-release device includes multiple first irregular-shaped parts and multiple second irregular-shaped parts; Multiple first irregular-shaped parts are spaced apart on one side edge of the blade fixing seat with the center of the blade fixing seat as the origin, and multiple second irregular-shaped parts are spaced apart on one side edge of the power fixing seat with the center of the power fixing seat as the origin; Each of the first irregularly shaped components has a first irregularly shaped component arranged opposite to it, and there is a gap between the two first irregularly shaped components arranged opposite to it to form an active space for the power fixing seat and the plurality of second irregularly shaped components to move, so that when the power fixing seat extends into the active space to move, each second irregularly shaped component and each first irregularly shaped component are engaged with each other.

4. The quick-release UAV with integrated adjustment device according to claim 3, characterized in that, The quick-release device includes multiple elastic fasteners, all of which are disposed on the blade fixing seat; Each of the first irregular-shaped parts is provided with the fixing groove, and each fixing groove is arranged opposite to each of the elastic fixing parts, so that when each of the second irregular-shaped parts and each of the first irregular-shaped parts are engaged with each other, the fixing part of each elastic fixing part extends into a fixing groove for engagement.

5. The quick-release UAV with integrated adjustment device according to claim 4, characterized in that, The elastic fastener also includes a lever arm that passes through one side of the blade fixing seat and extends outward.

6. The quick-release UAV with integrated adjustment device according to claim 1, characterized in that, The adjusting member is disposed within the blade fixing seat, and the adjusting member and the blade fixing seat are threadedly connected.

7. The quick-release UAV with integrated adjustment device according to claim 1, characterized in that, The adjusting component includes an adjusting part and a retaining tooth part, and the adjusting part is threadedly connected to the blade fixing seat; The adjustment device further includes at least one limiting member, which is detachably connected to the blade fixing seat to move toward and engage with the locking tooth portion.

8. The quick-release UAV with integrated adjustment device according to claim 1, characterized in that, The adjusting device also includes a plurality of limiting members, and at least two of the plurality of limiting members are arranged opposite to each other.

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