Bionic machine skeleton

Abstract

The utility model discloses a bionic machine framework, and belongs to the technical field of bionic equipment. The device mainly comprises a main rod and a bionic flight mechanism arranged on the main rod, the main rod is rectangular, and a first fixing frame, a controller mounting frame and a battery mounting frame are sequentially arranged on the main rod in the length direction of the main rod. According to the bionic machine framework, the use of redundant materials is reduced through the rectangular and tubular main rods, the overall weight is reduced through reasonable arrangement of the weight reduction grooves and the weight reduction holes, and secondly, unnecessary material consumption is effectively reduced through the distributed weight reduction grooves in the structural design of the controller mounting frame and the battery mounting frame, so that the cost is reduced. Especially, the battery mounting frame is distributed through symmetrical second weight reduction grooves, the weight is reduced, the overall stability of the framework is improved, through the optimized design, it is ensured that the bionic machine is light in weight, meanwhile, the bionic machine still has enough stability and strength, and the advantages of bionic design can be brought into full play.

Description

Technical Field

[0001] This application relates to the field of bionic equipment technology, specifically a bionic machine skeleton. Background Technology

[0002] Bionic machines are artificial devices designed and manufactured by mimicking the structure, movement, and function of organisms in nature. These machines combine knowledge from fields such as biology, engineering, and computer science, aiming to improve machine efficiency and adaptability by drawing on the high-performance capabilities of organisms in nature. Bionic machines come in many varieties, including bionic robots, bionic aircraft, and bionic underwater robots, and they have wide applications in various fields, such as medicine, agriculture, military, and environmental monitoring.

[0003] Bionic aircraft are a type of biomimetic machine that mimics the flight principles and structure of flying animals (such as butterflies), designing flight devices with wings or other flight organs. The advantage of biomimetic aircraft lies in their ability to achieve higher maneuverability, energy efficiency, and adaptability to complex environments by imitating the flexible flight methods of natural organisms. Bionic aircraft can more effectively cope with airflow changes and perform complex flight maneuvers. They have enormous application potential in fields such as military reconnaissance, environmental monitoring, and unmanned aerial vehicle (UAV) technology.

[0004] However, existing biomimetic aircraft skeleton designs still face some challenges, especially the weight issue. Although the design principle of biomimetic aircraft is to mimic the lightness and efficiency of living organisms as much as possible, due to the limitations of existing materials and manufacturing technologies, the skeleton of biomimetic aircraft is often heavier than the structure of living organisms. This excessive weight will lead to greater energy consumption during flight, affecting flight performance. Especially in missions that require efficient and continuous flight, excessive weight will directly affect the stability, maneuverability, and endurance of the aircraft, preventing it from fully leveraging the advantages of biomimetic design.

[0005] Therefore, it is necessary to provide a bionic machine skeleton to solve the above problems.

[0006] It should be noted that the information disclosed in this background section is only for understanding the background technology of this application concept, and therefore may include information that does not constitute prior art. Summary of the Invention

[0007] Based on the aforementioned problems in the existing technology, the problem to be solved by this application is to provide a bionic machine skeleton to solve the weight problem in the design of bionic machine skeletons.

[0008] The technical solution adopted by this application to solve its technical problem is: a bionic machine skeleton, including a main rod and a bionic flight mechanism disposed on the main rod. The main rod is rectangular in shape, and the main rod is provided with a first fixing frame, a controller mounting frame and a battery mounting frame in sequence along its length.

[0009] The controller mounting bracket includes a plate, and a clamping plate is provided on one side of the plate. The clamping plate is L-shaped and there are four sets, all distributed on one side of the plate. A first weight reduction groove is opened on one side of the plate.

[0010] The battery mounting bracket is a rectangular tubular body. A second weight-reducing groove is provided on the outer side of the battery mounting bracket, and multiple sets of the second weight-reducing groove are provided. The second weight-reducing groove is symmetrically distributed on both sides of the battery mounting bracket.

[0011] The first fixing frame includes a connecting plate and mounting frames inclinedly distributed on both sides of the connecting plate. A weight reduction hole is provided on one side of the mounting frame, and several sets of weight reduction holes are provided. A third weight reduction groove is provided on one side of the connecting plate.

[0012] Furthermore, the biomimetic flight mechanism includes a drive servo mounted on one side of the mounting frame and a servo rocker arm connected to the output end of the drive servo. A fixed block is connected to one side of the servo rocker arm, and a front wing and a rear wing are provided on one side of the fixed block.

[0013] Furthermore, the front wing includes a first outer contour frame and an elastic film laid on the first outer contour frame, and the rear wing includes a second outer contour frame and an elastic film laid on the second outer contour frame.

[0014] Furthermore, the servo rocker arm is L-shaped, and the surface of the connection end between the servo rocker arm and the fixed block is recessed inward to form a groove.

[0015] Furthermore, the upper end of the plate is provided with a first connecting block, and a first connecting groove is provided through one side of the first connecting block, which is adapted to the main rod.

[0016] Furthermore, the upper end of the battery mounting bracket is provided with a second connecting block, and a second connecting groove is provided through one side of the second connecting block, which is adapted to the main rod.

[0017] Furthermore, a third connecting groove is provided through one side of the connecting plate, and the third connecting groove is adapted to the main rod.

[0018] Furthermore, the main rod is a component made of carbon fiber.

[0019] Furthermore, reinforcing ribs are formed between the multiple sets of the second weight-reducing grooves.

[0020] The beneficial effects of this application are as follows: The bionic machine skeleton provided by this application reduces redundant material usage through the rectangular and tubular design of the main rod, and reduces the overall weight by rationally arranging weight-reducing grooves and holes. Secondly, the structural design of the controller mounting bracket and battery mounting bracket effectively reduces unnecessary material consumption through distributed weight-reducing grooves. In particular, the battery mounting bracket, through the symmetrical distribution of the second weight-reducing grooves, not only reduces the weight but also improves the overall stability of the skeleton. Through the above-mentioned optimized design, it is ensured that the bionic machine, while being lightweight, still has sufficient stability and strength, enabling it to fully leverage the advantages of bionic design.

[0021] In addition to the purposes, features, and advantages described above, this application has other purposes, features, and advantages. A further detailed description of this application will be provided below with reference to the figures. Attached Figure Description

[0022] The accompanying drawings, which form part of this application, are used to provide a further understanding of this application. The illustrative embodiments of this application and their descriptions are used to explain this application and do not constitute an undue limitation of this application.

[0023] In the attached diagram:

[0024] Figure 1 This is a schematic diagram of the overall structure in this application;

[0025] Figure 2 for Figure 1 Top view;

[0026] Figure 3 This is a schematic diagram of the forewing and rearwing structure of this application;

[0027] Figure 4 This is a schematic diagram of the controller mounting bracket structure for this application;

[0028] Figure 5 This is a schematic diagram of the battery mounting bracket structure in this application;

[0029] Figure 6 for Figure 5 The main view;

[0030] Figure 7 This is a schematic diagram of the first fixing frame structure of this application;

[0031] Figure 8 for Figure 7 Top view;

[0032] Figure 9 This is a schematic diagram of the servo rocker arm structure of this application;

[0033] The following are the labeling elements in the figure:

[0034] 1. Main rod; 2. First fixing frame; 21. Connecting plate; 211. Third connecting groove; 212. Third weight reduction groove; 22. Mounting frame; 221. Weight reduction hole; 3. Bionic flight mechanism; 31. Drive servo; 32. Servo rocker arm; 321. Groove; 33. Forewing; 331. First outer contour frame; 34. Rear wing; 341. Second outer contour frame; 35. Fixing block; 36. Elastic membrane; 4. Controller mounting bracket; 41. Plate; 411. Clamping plate; 412. First weight reduction groove; 42. First connecting block; 421. First connecting groove; 5. Battery mounting bracket; 51. Second weight reduction groove; 52. Reinforcing rib; 53. Second connecting block; 531. Second connecting groove. Detailed Implementation

[0035] It should be noted that, unless otherwise specified, the embodiments and features described in this application can be combined with each other. This application will now be described in detail with reference to the accompanying drawings and embodiments.

[0036] To enable those skilled in the art to better understand the present application, the technical solutions in the embodiments of the present application will be clearly and completely described below with reference to the accompanying drawings. Obviously, the described embodiments are only some embodiments of the present application, and not all embodiments. Based on the embodiments in the present application, all other embodiments obtained by those of ordinary skill in the art without creative effort should fall within the scope of protection of the present application.

[0037] like Figures 1 to 9 As shown, this application provides a bionic machine skeleton, including a main rod 1 and a bionic flight mechanism 3 disposed on the main rod 1. The main rod 1 is rectangular in shape, and a first fixing frame 2, a controller mounting frame 4 and a battery mounting frame 5 are arranged sequentially along its length.

[0038] The controller mounting bracket 4 includes a plate 41. A clamping plate 411 is provided on one side of the plate 41. The clamping plate 411 is L-shaped and there are four sets, all distributed on one side of the plate 41. A first weight reduction groove 412 is provided on one side of the plate 41.

[0039] The battery mounting bracket 5 is a rectangular tubular body. A second weight reduction groove 51 is provided on the outer side of the battery mounting bracket 5, and multiple sets of the second weight reduction groove 51 are provided. The second weight reduction groove 51 is symmetrically distributed on both sides of the battery mounting bracket 5.

[0040] The first fixing frame 2 includes a connecting plate 21 and an installation frame 22 inclinedly distributed on both sides of the connecting plate 21. A weight reduction hole 221 is provided on one side of the installation frame 22, and several sets of weight reduction holes 221 are provided. A third weight reduction groove 212 is provided on one side of the connecting plate 21.

[0041] In this embodiment, the rectangular main rod 1 ensures sufficient load-bearing capacity and reduces unnecessary material usage. When installing the controller, it is inserted from the side of the L-shaped clamp 411 and made to fit against the plate 41. The controller can be stably fixed by the four clamps 411. At the same time, the first weight-reducing groove 412 can reduce the overall weight of the controller mounting frame 4 and increase air circulation when the controller is fitted against the plate 41, so that the controller can dissipate heat quickly during operation. When installing the battery, the battery is inserted into the rectangular tubular battery mounting frame 5. The weight of the battery mounting frame 5 can be greatly reduced by the multiple sets of second weight-reducing grooves 51, while also allowing the battery to dissipate heat, reducing material usage without affecting the installation and protection of the battery. The multiple sets of symmetrically distributed second weight-reducing grooves 51 can effectively balance the overall strength of the structure and ensure stability during flight. By connecting the plate 21 and the mounting frame 22, the weight-reducing hole 221 is combined with the third weight-reducing groove 212, further reducing the overall weight of the structure while ensuring the stability and strength of the mounting frame 22.

[0042] The main rod 1, with its rectangular and tubular design, reduces redundant material usage. The overall weight is also reduced through the rational arrangement of weight-reducing grooves and holes 221. Furthermore, the structural design of the controller mounting bracket 4 and the battery mounting bracket 5 effectively reduces unnecessary material consumption through distributed weight-reducing grooves. In particular, the battery mounting bracket 5, with its symmetrical distribution of second weight-reducing grooves 51, not only reduces weight but also improves the overall stability of the frame. Through the above optimized design, the bionic machine is ensured to maintain sufficient strength and durability while being lightweight.

[0043] like Figure 2 As shown, the bionic flight mechanism 3 includes a drive servo motor 31 mounted on one side of the mounting frame 22 and a servo arm 32 connected to the output end of the drive servo motor 31. A fixing block 35 is connected to one side of the servo arm 32, and a front wing 33 and a rear wing 34 are provided on one side of the fixing block 35.

[0044] In this embodiment, when the drive servo motor 31 receives the control signal, it controls the servo arm 32 to make corresponding movements, thereby adjusting the angles of the forewing 33 and the rearwing 34 to mimic the wing movements during butterfly flight, thereby generating thrust and lift, enabling it to fly flexibly and complete flight maneuvers.

[0045] like Figure 3 As shown, the front wing 33 includes a first outer contour frame 331 and an elastic film 36 laid on the first outer contour frame 331, and the rear wing 34 includes a second outer contour frame 341 and an elastic film 36 laid on the second outer contour frame 341.

[0046] In this embodiment, the elastic film 36 is supported by the first outer contour frame 331 and the second outer contour frame 341. The elastic film 36 has good elasticity, durability and tensile strength, and can effectively withstand air resistance during flight. At the same time, its own weight is small, which can further meet the requirements of lightweighting.

[0047] like Figure 9 As shown, the servo rocker arm 32 is L-shaped, and the surface of the connection end between the servo rocker arm 32 and the fixed block 35 is recessed inward to form a groove 321.

[0048] In this embodiment, the groove 321 not only reduces the weight of the servo arm 32, thus helping to reduce the overall weight of the aircraft, but also helps to reduce airflow interference to a certain extent, thereby reducing the air resistance of the aircraft during flight and improving the overall flight efficiency.

[0049] like Figures 4 to 8 As shown, the upper end of the plate 41 is provided with a first connecting block 42, and a first connecting groove 421 is provided through one side of the first connecting block 42. The first connecting groove 421 is adapted to the main rod 1.

[0050] The upper end of the battery mounting bracket 5 is provided with a second connecting block 53, and a second connecting groove 531 is provided through one side of the second connecting block 53. The second connecting groove 531 is adapted to the main rod 1.

[0051] A third connecting groove 211 is provided through one side of the connecting plate 21, and the third connecting groove 211 is adapted to the main rod 1.

[0052] In this embodiment, during assembly, the first connecting slot 421 is aligned with the main rod 1 and inserted, then the second connecting slot 531 is aligned with the main rod 1 and inserted, and then the third connecting slot 211 is aligned with the main rod 1 and inserted. The controller mounting bracket 4, the battery mounting bracket 5, and the first fixing bracket 2 are positioned in appropriate positions to achieve the connection of each frame.

[0053] like Figure 1 As shown, the main rod 1 is a component made of carbon fiber.

[0054] In this embodiment, the main rod 1, made of carbon fiber, not only significantly reduces weight but also has high strength, effectively ensuring the lightweight and stability of the overall structure.

[0055] like Figures 5 to 6 As shown, reinforcing ribs 52 are formed between multiple sets of second weight-reducing grooves 51.

[0056] In this embodiment, the battery mounting bracket 5 needs to bear the weight of the battery pack, and the second weight-reducing groove 51 can effectively reduce the overall weight. The second weight-reducing groove 51 is connected by the reinforcing rib 52, which can improve its strength and stability while reducing the overall weight.

[0057] The above description is merely a preferred embodiment of this application and is not intended to limit this application. Various modifications and variations can be made to this application by those skilled in the art. Any modifications, equivalent substitutions, improvements, etc., made within the spirit and principles of this application should be included within the protection scope of this application.

Claims

1. A biomimetic robotic skeleton, characterized in that, It includes a main rod and a biomimetic flight mechanism mounted on the main rod. The main rod is rectangular in shape, and along its length, it is provided with a first fixing frame, a controller mounting frame, and a battery mounting frame in sequence. The controller mounting bracket includes a plate, and a clamping plate is provided on one side of the plate. The clamping plate is L-shaped and there are four sets, all distributed on one side of the plate. A first weight reduction groove is opened on one side of the plate. The battery mounting bracket is a rectangular tubular body. A second weight-reducing groove is provided on the outer side of the battery mounting bracket, and multiple sets of the second weight-reducing groove are provided. The second weight-reducing groove is symmetrically distributed on both sides of the battery mounting bracket. The first fixing frame includes a connecting plate and mounting frames inclinedly distributed on both sides of the connecting plate. A weight reduction hole is provided on one side of the mounting frame, and several sets of weight reduction holes are provided. A third weight reduction groove is provided on one side of the connecting plate.

2. The bionic robotic skeleton according to claim 1, characterized in that: The biomimetic flight mechanism includes a drive servo mounted on one side of the mounting frame and a servo rocker arm connected to the output end of the drive servo. A fixed block is connected to one side of the servo rocker arm, and a front wing and a rear wing are provided on one side of the fixed block.

3. The bionic robotic skeleton according to claim 2, characterized in that: The front wing includes a first outer contour frame and an elastic film laid on the first outer contour frame, and the rear wing includes a second outer contour frame and an elastic film laid on the second outer contour frame.

4. The bionic robotic skeleton according to claim 2, characterized in that: The servo arm is L-shaped, and the surface of the connection end between the servo arm and the fixed block is recessed inward to form a groove.

5. The bionic robotic skeleton according to claim 1, characterized in that: The upper end of the plate is provided with a first connecting block, and a first connecting groove is provided through one side of the first connecting block, which is adapted to the main rod.

6. The bionic robotic skeleton according to claim 1, characterized in that: The upper end of the battery mounting bracket is provided with a second connecting block, and a second connecting groove is provided through one side of the second connecting block, which is adapted to the main rod.

7. The bionic robotic skeleton according to claim 1, characterized in that: A third connecting groove is provided through one side of the connecting plate, and the third connecting groove is adapted to the main rod.

8. The bionic robotic skeleton according to claim 1, characterized in that: The main rod is a component made of carbon fiber.

9. The bionic robotic skeleton according to claim 1, characterized in that: Reinforcing ribs are formed between multiple sets of the second weight-reducing grooves.

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