Brachial base structure material of motor West-Cherry-Nu Pensu spacecraft and design method of brachial base structure material

Abstract

The invention relates to the technical field of spaceflight, in particular to a brachial base structure material and a design method of a motor West-odd-female penspace ship, a brachial base structure of a bird is deeply researched and observed, after research data are obtained, the brachial base structure of the bird is applied to the design of the space ship, after the design is completed, a model of the brachial base structure of the space ship is manufactured, and the brachial base structure of the motor West-odd-female penspace ship is obtained. After the model is manufactured, the spaceship brachial base structure is tested, after the test is finished, the spaceship brachial base structure is optimized and improved, and after the performance and efficiency of the spaceship brachial base structure meet certain requirements, the spaceship brachial base structure is applied to an actual spaceship. The skeleton structure of the bionic bird has good rigidity and stability, the structural stability and safety of the spacecraft are guaranteed, the impact resistance of the spacecraft is improved, the bionic bird can flexibly adapt to various spatial layouts, the manufacturing process of the spacecraft can be simplified, the manufacturing cost and the maintenance cost can be reduced, and meanwhile the production efficiency is improved.

Description

Technical Field

[0001] This invention relates to the field of aerospace technology, and in particular to a material and design method for the humeral base structure of the Motor Sich female spacecraft. Background Technology

[0002] The humeral base structure of a spacecraft refers to its supporting structure, typically the connection and support structure between the main body of the spacecraft and components such as the propulsion system and navigation system. The humeral base structure is a crucial part of spacecraft design, needing to withstand various complex environments and loads to ensure the stability and safety of the overall spacecraft structure. Simultaneously, the humeral base structure must also consider factors such as propulsion efficiency, mass distribution, and heat dissipation performance; therefore, its design requires a comprehensive consideration of multiple factors.

[0003] Inspired by the evolution of all things in nature, intelligent biomimetic design has demonstrated many advantages in functional materials and complex optimized structures, but the humerus structure of a spacecraft based on the pheasant as a biomimetic design has not yet been made public. Summary of the Invention

[0004] The purpose of this invention is to provide a humerus base structure material and design method for the Motor Sich female puppet spacecraft, which solves the problem that the humerus base structure of a spacecraft designed with a pheasant as a biomimetic design has not yet been disclosed.

[0005] To achieve the above objectives, the present invention provides a design method for the humeral base structure of the Motor Sich female puppet spacecraft, comprising the following steps: In-depth research and observation of the humeral base structure of the pheasant; After obtaining the research data, the humeral base structure of the pheasant was applied to the design of the spacecraft; After completing the design, a model of the spacecraft's humeral base structure was made; After the model was completed, the spacecraft's humeral base structure was tested. After the test, the spacecraft's humeral base structure was optimized and improved. Once the performance and efficiency of the spacecraft's humerus structure meet certain requirements, it will be applied to actual spacecraft.

[0006] The in-depth study and observation of the humeral base structure of the pheasant includes the following steps: Select pheasant samples; Observe the appearance of the humeral base structure of the pheasant, including its overall shape, size, color and texture. Also, observe the connection between the humeral base structure and surrounding tissues and whether there are any abnormalities or lesions. The humeral base structure of the pheasant was studied in depth using anatomical methods. Tissue samples of the humeral base structure were prepared into slides, and their tissue structure and cellular composition were observed under a microscope. Biomechanical tests were conducted on the humeral base structure of the pheasant to obtain its performance under different loads. Observe and study the functional performance of the humeral base structure of pheasants during flight; By comparing the humeral base structure with those of other birds or organisms, the uniqueness and advantages of the humeral base structure of the pheasant can be obtained; The collected data and observations were organized and analyzed, and the structure and function of the humeral base of the pheasant were explained and inferred by combining the principles and methods of biology, anatomy and biomechanics.

[0007] The step of applying the humeral base structure of the pheasant to the design of the spacecraft after obtaining the research data also includes: The obtained research data were organized and analyzed to extract the morphological, tissue, functional, and biomechanical characteristics and patterns of the humeral base structure of the pheasant. Based on the characteristics of the humerus structure in terms of morphology, material, connection method and stability, a humerus structure suitable for spacecraft was designed.

[0008] The process of creating a model of the spacecraft's humeral base structure after completing the design also includes: Materials were selected based on design requirements and the characteristics of the spacecraft's humerus structure. The manufacturing process is determined based on the selected materials and the complexity of the spacecraft's humerus structure; Based on the design drawings and technical requirements, a model of the spacecraft's humeral base structure was made.

[0009] The process of testing the spacecraft's humeral base structure after model creation also includes: Set up the testing platform and environment; Different loads and stresses were applied to the humeral base structure of the spacecraft, and the response and changes of the humeral base structure were observed to evaluate its performance under various conditions. Simulate the movements and attitudes during flight, observe the motion trajectory and change patterns of the humeral base structure, and check whether its coordination and connection with surrounding components are normal; Simulate loads and stresses under unexpected conditions to observe the stability and reliability of the humerus base structure; The stability and durability of the humeral base structure are evaluated through long-term or repeated testing.

[0010] The optimization and improvement of the spacecraft's humeral base structure after testing includes the following steps: Analyze the data collected during the testing process, identify existing problems and shortcomings, and determine the aspects that need to be improved and optimized; Conduct in-depth diagnosis and localization of problems that arise during the testing process, and determine the nature and scope of the problems; Based on the results of the problem diagnosis, develop corresponding optimization plans; Based on the optimization scheme, the design of the spacecraft's humeral base structure was improved; Optimize the manufacturing process of the spacecraft's humeral base structure; Select or replace appropriate materials according to the needs of the optimization plan; Based on the improved design and optimization scheme, a new model of the spacecraft's humeral base structure was fabricated. The optimized and improved spacecraft humeral base structure was verified.

[0011] A material for the humeral base structure of the Motor Sich-Pulp Pon spacecraft, applicable to the aforementioned design method for the humeral base structure of the Motor Sich-Pulp Pon spacecraft.

[0012] This invention discloses a material and design method for the humeral base structure of a spacecraft, specifically the Moto Sich female puppet. First, it involves in-depth research and observation of the humeral base structure of a pheasant, including its morphology, materials, strength, and stability characteristics. This is achieved through field observation, anatomical studies, and computer simulations. After obtaining sufficient research data, the humeral base structure of the spacecraft is designed. The design process fully considers the principles of biomimicry, applying the bird's humeral base structure to the spacecraft design. This includes selecting suitable materials, designing appropriate shapes and sizes, and considering factors such as strength and stability. After completing the design, a model of the spacecraft's humeral base structure is fabricated, taking into full account manufacturing processes and material selection to ensure the model's quality. The model accurately reflects the design intent while also considering factors such as weight, strength, and stability. After model construction, various tests are conducted on the spacecraft's humerus structure, including strength tests, fatigue tests, and stability tests, to help identify design problems and shortcomings and make improvements and optimizations. After the testing phase, the spacecraft's humerus structure is further optimized and improved, including measures such as design improvements, manufacturing process improvements, and material selection optimization, to enhance the spacecraft's performance and efficiency. Finally, once the performance and efficiency of the spacecraft's humerus structure meet certain requirements, it is applied to actual spacecraft, including applications that improve spacecraft stability and safety, and increase propulsion efficiency. The lightweight skeletal structure of the biomimetic pheasant can significantly reduce the weight of a spacecraft, thereby improving its payload and energy efficiency. Its excellent rigidity and stability allow it to effectively withstand various external and internal forces, ensuring the structural stability and safety of the spacecraft. The skeletal structure can absorb and disperse impact forces, enhancing the spacecraft's impact resistance and protecting internal equipment and personnel. Furthermore, its flexible adaptability to various spatial layouts optimizes space utilization, improving habitability and operational performance. Finally, the skeletal structure simplifies spacecraft manufacturing processes, reduces manufacturing and maintenance costs, and increases production efficiency. Attached Figure Description

[0013] To more clearly illustrate the technical solutions in the embodiments of this application or the prior art, the accompanying drawings used in the description of the embodiments or the prior art will be briefly introduced below.

[0014] Figure 1 This is a step diagram of the design method for the humeral base structure of the Motor Sich female puppet spacecraft of the present invention.

[0015] Figure 2 This is a step diagram illustrating the in-depth study and observation of the humeral base structure of the pheasant according to the present invention.

[0016] Figure 3This is a flowchart illustrating the steps of applying the humeral base structure of the pheasant to the design of a spacecraft after obtaining research data.

[0017] Figure 4 This is a diagram showing the steps involved in creating a model of the spacecraft's humeral base structure after the completion of the design of this invention.

[0018] Figure 5 This diagram illustrates the steps involved in testing the spacecraft's humeral base structure after the completion of the model fabrication.

[0019] Figure 6 This is a flowchart illustrating the steps involved in optimizing and improving the spacecraft's humerus structure after testing, as per the present invention. Detailed Implementation

[0021] The embodiments of the present invention are described in detail below. Examples of the embodiments are shown in the accompanying drawings. The embodiments described below with reference to the accompanying drawings are exemplary and intended to explain the present invention, but should not be construed as limiting the present invention.

[0022] The first embodiment of this application is as follows: Please see Figures 1 to 6 ,in, Figure 1 This is a step diagram of the design method for the humeral base structure of the Motor Sich female puppet spacecraft of the present invention. Figure 2 This is a step diagram illustrating the in-depth study and observation of the humeral base structure of the pheasant according to the present invention. Figure 3 This is a flowchart illustrating the steps of applying the humeral base structure of the pheasant to the design of a spacecraft after obtaining research data. Figure 4 This is a diagram showing the steps involved in creating a model of the spacecraft's humeral base structure after the completion of the design of this invention. Figure 5 This diagram illustrates the steps involved in testing the spacecraft's humeral base structure after the completion of the model fabrication. Figure 6 This invention presents a step-by-step diagram illustrating the optimization and improvement of the spacecraft's humeral base structure after testing. The invention provides a design method for the humeral base structure of the Motor Sich female spacecraft, comprising the following steps: S100: Conduct in-depth research and observation on the humeral base structure of the pheasant; S101: Select a pheasant sample; S102: Observe the appearance of the humeral base structure of the pheasant, including the overall shape, size, color and texture of the humeral base structure. At the same time, pay attention to the connection between the humeral base structure and the surrounding tissues and the presence of any abnormalities or lesions. S103: Conduct in-depth research on the humeral base structure of the pheasant using anatomical methods; S104: Prepare tissue samples of the humeral base structure and observe their tissue structure and cellular composition under a microscope; S105: Biomechanical tests were conducted on the humeral base structure of the pheasant to obtain the performance of the humeral base structure under different loads; S106: Observe and study the functional performance of the humeral base structure of pheasants during flight; S107: Comparative study of the humeral base structure with other birds or organisms to obtain the uniqueness and advantages of the humeral base structure of the pheasant; S108: Organize and analyze the collected data and observations, and explain and infer the structure and function of the humeral base of the pheasant by combining the principles and methods of biology, anatomy and biomechanics.

[0023] Specifically, representative specimens of pheasants are selected, either live or deceased, ensuring the specimens have intact and healthy humeral base structures for subsequent research and observation. First, the external morphology of the humeral base structure is observed, including its overall shape, size, color, and texture. Attention is paid to its connection with surrounding tissues and the presence of any abnormalities or lesions. Anatomical methods are then used to conduct in-depth research on the humeral base structure, including separating surrounding muscles, nerves, and blood vessels to observe its internal structure and function. The tissue samples are prepared and examined under a microscope to observe their tissue structure and cellular composition, understanding information such as tissue type, cell morphology, and arrangement. This process is crucial for understanding the pheasant's health. Biomechanical tests were conducted on the humeral base structure of the pheasant to understand its performance under different loads. Different forces and torques were applied to the humeral base structure using experimental equipment, and its response and changes were observed. The functional performance of the humeral base structure of the pheasant during flight was observed and studied. Its movements and postures in flight, as well as the movement trajectory and change patterns of the humeral base structure, were recorded using high-speed cameras. Comparative studies were conducted with the humeral base structures of other birds or organisms to understand the uniqueness and advantages of the pheasant's humeral base structure, and to better understand its characteristics and mechanisms of adaptation to flight. The collected data and observation results were organized and analyzed to gain a deeper understanding of the pheasant's humeral base structure. Its structure and function were explained and inferred by combining the principles and methods of biology, anatomy, and biomechanics.

[0024] S200: After obtaining the research data, the humeral base structure of the pheasant was applied to the design of the spacecraft; S201: Organize and analyze the obtained research data, and extract the morphological, tissue, functional and biomechanical characteristics and patterns of the humeral base structure of the pheasant; S202: Based on the characteristics of the humerus structure of the pheasant, including its morphology, materials, connection methods, and stability, design a humerus structure suitable for a spacecraft.

[0025] Specifically, the research data obtained was organized and analyzed to extract the characteristics and patterns of the morphology, organization, function, and biomechanics of the pheasant's humeral base structure. This data served as the basis for designing the spacecraft's humeral base structure. Based on the research results and the needs of the spacecraft design, biomimetic design was initiated, including designing a humeral base structure suitable for the spacecraft based on the characteristics of the bird's humeral base structure in terms of morphology, materials, connection methods, and stability.

[0026] S300: After completing the design, a model of the spacecraft's humeral base structure will be made; S301: Select materials based on design requirements and the characteristics of the spacecraft's humerus structure; S302: Determine the manufacturing process based on the selected materials and the complexity of the spacecraft's humerus structure; S303: Based on the design drawings and technical requirements, create a model of the spacecraft's humeral base structure.

[0027] Specifically, based on the design requirements and the characteristics of the spacecraft's humerus structure, suitable materials are selected, taking into account factors such as the material's strength, stability, durability, and machinability. Depending on the selected materials and the complexity of the spacecraft's humerus structure, appropriate manufacturing processes are determined, including machining, 3D printing, and casting. Based on the design drawings and technical requirements, the model of the spacecraft's humerus structure is then manufactured, strictly adhering to the design requirements to ensure that the model's dimensions, shape, and precision meet the design standards.

[0028] S400: After the model is completed, the spacecraft's humeral base structure is tested; S401: Set up the test platform and environment; S402: Apply different loads and stresses to the humeral base structure of the spacecraft, observe the response and changes of the humeral base structure, and evaluate its performance under various conditions; S403: Simulate the actions and attitudes during flight, observe the motion trajectory and change patterns of the humeral base structure, and check whether its coordination and connection with surrounding components are normal; S404: Simulate loads and stresses under unexpected conditions to observe the stability and reliability of the humerus base structure; S405: Evaluate the stability and durability of the humerus base structure through long-term or repeated testing.

[0029] Specifically, according to the testing requirements, a suitable test platform and environment are built, including test equipment, support devices, sensors, etc., to ensure that the test environment can simulate the conditions in the real flight environment, such as temperature, pressure, and vibration. The performance of the spacecraft's humerus structure is tested, including tests on strength, stiffness, and fatigue life. By applying different loads and stresses, the response and changes of the humerus structure are observed to evaluate its performance under various conditions and check whether the spacecraft's humerus structure functions normally. By simulating the movements and attitudes during flight, the motion trajectory and change patterns of the humerus structure are observed to check whether its cooperation and connection with surrounding components are normal. Safety tests are conducted, including tests for collisions, impacts, and vibrations. By simulating loads and stresses under unexpected conditions, the stability and reliability of the humeral base structure are observed to ensure it can withstand various potential risks. Reliability tests are conducted on the spacecraft's humeral base structure, including tests for long-term operation and repeated use. Through long-term or repeated testing, the stability and durability of the humeral base structure are evaluated to ensure that it can maintain stable performance within its expected service life. During the testing process, sensors and measuring equipment are used to collect relevant data, such as loads, stresses, displacements, and vibrations. The collected data is then processed and analyzed to evaluate the performance and safety of the spacecraft's humeral base structure.

[0030] S500: After the test, the spacecraft's humeral base structure was optimized and improved; S501: Analyze the data collected during the testing process, identify existing problems and deficiencies, and determine the aspects that need to be improved and optimized; S502: Conduct in-depth diagnosis and localization of problems that arise during the testing process, and determine the nature and scope of the problem; S503: Based on the results of the problem diagnosis, formulate corresponding optimization plans; S504: Based on the optimization scheme, the design of the spacecraft's humeral base structure was improved; S505: Optimize the manufacturing process of the spacecraft's humerus structure; S506: Select or replace appropriate materials according to the needs of the optimization plan; S507: Based on the improved design and optimization scheme, a new model of the spacecraft's humeral base structure was made; S508: Verify the optimized and improved spacecraft humeral base structure.

[0031] Specifically, a detailed analysis of the data collected during the testing process is conducted to understand the performance and safety of the spacecraft's humeral base structure, identify existing problems and deficiencies, and determine aspects requiring improvement and optimization. In-depth diagnosis and localization of problems encountered during testing are performed, analyzing their causes, nature, and scope of impact. This helps determine the direction and focus of optimization and improvement. Based on the problem diagnosis results, corresponding optimization plans are formulated, including measures such as design improvements, manufacturing process improvements, and material selection optimization. Taking into account various factors, a practical optimization plan is developed. Based on the optimization plan, the design of the spacecraft's humeral base structure is improved, including adjustments to structural dimensions, changes in material distribution, and optimization of connection methods, ensuring that the improvements are effective. The design addresses existing problems and improves the spacecraft's performance and safety. It optimizes the manufacturing process of the spacecraft's humeral base structure, selecting appropriate manufacturing processes and optimizing process parameters based on the improved design requirements. This ensures the manufactured humeral base structure meets design requirements, improves production efficiency and product quality, selects or replaces suitable materials according to the optimization scheme, compares the performance parameters and applicability of different materials, and selects materials that meet performance and safety requirements. It also considers factors such as material machinability, cost, and environmental friendliness. Based on the improved design and optimization scheme, a new model of the spacecraft's humeral base structure is fabricated. Through testing and verification, it ensures that the improved model has significant improvements in performance and safety. If necessary, further adjustments and improvements are made.

[0032] S600: Once the performance and efficiency of the spacecraft's humerus structure meet certain requirements, it will be applied to actual spacecraft.

[0033] Specifically, the optimized and improved spacecraft humeral base structure will be verified in practical applications. Through actual flight or simulated flight experiments, its performance in real environments will be observed to ensure that it meets design requirements and safety standards. In practical applications, the performance and problem feedback of the spacecraft humeral base structure will be continuously monitored, and necessary adjustments and improvements will be made according to the actual situation to maintain the continuous improvement of its performance and safety.

[0034] The lightweight skeletal structure of the biomimetic pheasant significantly reduces the weight of spacecraft, thereby improving its payload and energy efficiency. Its excellent rigidity and stability allow it to effectively withstand various external and internal forces, ensuring the structural stability and safety of the spacecraft. The skeletal structure absorbs and disperses impact forces, enhancing the spacecraft's shock resistance and protecting internal equipment and personnel. It can flexibly adapt to various spatial layouts, optimizing space utilization and improving habitability and operational performance. The skeletal structure simplifies spacecraft manufacturing processes, reduces manufacturing and maintenance costs, and increases production efficiency. Finally, the skeletal structure uses biodegradable, environmentally friendly materials, meeting ecological and environmental protection requirements.

[0035] The second embodiment of this application is as follows: Based on the first embodiment, the humeral structure material of the Motor Sich female puppet spacecraft in this embodiment is a designable smart material built upon existing natural materials, artificially synthesized materials, and organic polymer materials. The greatest characteristic of biomimetic materials is their designability. People can extract biological prototypes from nature, including the human body structure, explore their functional principles, and design new functional materials that can effectively sense external environmental stimuli and react rapidly. This eliminates the boundary between structural and functional materials, achieving the integration of intelligent, information-based, and structurally functional materials.

[0036] The above-disclosed embodiments are merely one or more preferred embodiments of this application and should not be construed as limiting the scope of this application. Those skilled in the art can understand that all or part of the processes for implementing the above embodiments and equivalent changes made in accordance with the claims of this application still fall within the scope of this application.

Claims

1. A design method for the humeral base structure of the Motor Sich female puppet Pon spacecraft, characterized in that, Includes the following steps: In-depth research and observation of the humeral base structure of the pheasant; After obtaining the research data, the humeral base structure of the pheasant was applied to the design of the spacecraft; After completing the design, a model of the spacecraft's humeral base structure was made; After the model was completed, the spacecraft's humeral base structure was tested. After the test, the spacecraft's humeral base structure was optimized and improved. Once the performance and efficiency of the spacecraft's humerus structure meet certain requirements, it will be applied to actual spacecraft.

2. The design method for the humeral base structure of the Motor Sich female puppet Pon spacecraft as described in claim 1, characterized in that, The steps involved in the in-depth study and observation of the humeral base structure of the pheasant also include: Select pheasant samples; Observe the appearance of the humeral base structure of the pheasant, including its overall shape, size, color and texture. Also, observe the connection between the humeral base structure and surrounding tissues and whether there are any abnormalities or lesions. The humeral base structure of the pheasant was studied in depth using anatomical methods. Tissue samples of the humeral base structure were prepared into slides, and their tissue structure and cellular composition were observed under a microscope. Biomechanical tests were conducted on the humeral base structure of the pheasant to obtain its performance under different loads. Observe and study the functional performance of the humeral base structure of pheasants during flight; By comparing the humeral base structure with those of other birds or organisms, the uniqueness and advantages of the humeral base structure of the pheasant can be obtained; The collected data and observations were organized and analyzed, and the structure and function of the humeral base of the pheasant were explained and inferred by combining the principles and methods of biology, anatomy and biomechanics.

3. The design method for the humeral base structure of the Motor Sich female puppet spacecraft as described in claim 2, characterized in that, After obtaining the research data, the humeral base structure of the pheasant was applied to the design of the spacecraft. The steps also included: The obtained research data were organized and analyzed to extract the morphological, tissue, functional, and biomechanical characteristics and patterns of the humeral base structure of the pheasant. Based on the characteristics of the humerus structure in terms of morphology, material, connection method and stability, a humerus structure suitable for spacecraft was designed.

4. The design method for the humeral base structure of the Motor Sich female puppet spacecraft as described in claim 3, characterized in that, After the design is completed, a model of the spacecraft's humeral base structure is made. This step also includes: Materials were selected based on design requirements and the characteristics of the spacecraft's humerus structure. The manufacturing process is determined based on the selected materials and the complexity of the spacecraft's humerus structure; Based on the design drawings and technical requirements, a model of the spacecraft's humeral base structure was made.

5. The design method for the humeral base structure of the Motor Sich female puppet spacecraft as described in claim 4, characterized in that, After the model is completed, the spacecraft's humeral base structure is tested. The steps also include: Set up the testing platform and environment; Different loads and stresses were applied to the humeral base structure of the spacecraft, and the response and changes of the humeral base structure were observed to evaluate its performance under various conditions. Simulate the movements and attitudes during flight, observe the motion trajectory and change patterns of the humeral base structure, and check whether its coordination and connection with surrounding components are normal; Simulate loads and stresses under unexpected conditions to observe the stability and reliability of the humerus base structure; The stability and durability of the humeral base structure are evaluated through long-term or repeated testing.

6. The design method for the humeral base structure of the Motor Sich female puppet spacecraft as described in claim 5, characterized in that, After the test, the spacecraft's humeral base structure was optimized and improved, and the steps included: Analyze the data collected during the testing process, identify existing problems and shortcomings, and determine the aspects that need to be improved and optimized; Conduct in-depth diagnosis and localization of problems that arise during the testing process, and determine the nature and scope of the problems; Based on the results of the problem diagnosis, develop corresponding optimization plans; Based on the optimization scheme, the design of the spacecraft's humeral base structure was improved; Optimize the manufacturing process of the spacecraft's humeral base structure; Select or replace appropriate materials according to the needs of the optimization plan; Based on the improved design and optimization scheme, a new model of the spacecraft's humeral base structure was fabricated. The optimized and improved spacecraft humeral base structure was verified.

7. A humeral base structure material for the Motor Sich-Pulp spacecraft, applicable to the humeral base structure design method of the Motor Sich-Pulp spacecraft as described in any one of claims 1 to 6.

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