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CN-122020831-A - Moxiqi female puppet Peng Yuzhou airship humerus-based structural material and design method

CN122020831ACN 122020831 ACN122020831 ACN 122020831ACN-122020831-A

Abstract

The invention relates to the technical field of spaceflight, in particular to a motor Welch's Peng Yuzhou model of a spacecraft humerus base structure material and a design method, which are used for carrying out deep research and observation on a humerus base structure of a hui bird, after research data are obtained, applying the humerus base structure of a hui bird to the design of a spacecraft, after the design is completed, making a model of the spacecraft humerus base structure, after the model is made, testing the spacecraft humerus base structure, optimizing and perfecting the spacecraft humerus base structure after the test is finished, and applying the model to an actual spacecraft after the performance and efficiency of the spacecraft humerus base structure reach certain requirements. The skeleton structure of the bionic hui bird has good rigidity and stability, ensures the structural stability and safety of the spacecraft, improves the shock resistance of the spacecraft, can flexibly adapt to various space layouts, can simplify the manufacturing process of the spacecraft, reduces the manufacturing cost and the maintenance cost, and simultaneously improves the production efficiency.

Inventors

  • LI FENG

Assignees

  • 马达西奇飞机发动机厂(湖北)有限公司

Dates

Publication Date
20260512
Application Date
20240130

Claims (7)

  1. 1. A method for designing a motor-zebra-female puppet Peng Yuzhou airship humerus base structure, comprising the steps of: Deep research and observation of the humeral structure of hui birds; After the research data are obtained, applying the humerus base structure of hui birds to the design of the airship; After the design is completed, a model of the airship humerus base structure is manufactured; After the model is manufactured, testing the humerus base structure of the airship; After the test is finished, optimizing and perfecting the structure of the airship humerus base; When the performance and efficiency of the airship humerus base structure meet certain requirements, the method is applied to an actual space craft.
  2. 2. The method of designing a Ma Daxi-Qiyn Peng Yuzhou airship humeral structure according to claim 1, wherein the humeral structure of a hui bird is studied and observed in depth, said steps further comprising: Selecting hui bird samples; observing the appearance form of the humerus base structure of hui birds, including the overall form, size, color and texture of the humerus base structure, and simultaneously observing the connection mode and characteristics of the humerus base structure and surrounding tissues and whether abnormality or pathological change exists; the humeral structure of hui birds was studied in depth by anatomical means; The tissue sample with the humerus base structure is subjected to sheet making treatment, and the tissue structure and the cell composition of the tissue sample are observed through a microscope; performing biomechanical test on the humerus base structure of hui birds to obtain performance of the humerus base structure under different loads; Observing and researching the functional performance of hui birds on the humeral structure during flight; comparing and researching with other birds or living brachial base structures to obtain the uniqueness and advantages of hui bird brachial base structures; the collected data and observations are collated and analyzed, and the structure and function of the hui bird humerus base is interpreted and inferred in combination with biological, anatomical, and biomechanical principles and methods.
  3. 3. The method of designing a Ma Daxi-Qiyn puppet Peng Yuzhou airship humerus structure according to claim 2, wherein the humerus structure of hui bird is applied to the design of the airship after the study data is obtained, the steps further comprising: The obtained research data are arranged and analyzed, and characteristics and rules of morphology, organization, function and biomechanics of the hui bird humerus base structure are extracted; according to the characteristics of hui bird humerus base structure in terms of form, material, connection mode and stability, a humerus base structure suitable for a spacecraft is designed.
  4. 4. The method of designing a Ma Daxi-Qiyn puppet Peng Yuzhou airship base structure according to claim 3, wherein after the design is completed, the step of modeling the airship base structure further comprises: Selecting materials according to design requirements and characteristics of a humerus base structure of the airship; determining a manufacturing process based on the selected materials and the complexity of the airship humerus base structure; and (3) manufacturing a model of the airship humerus base structure according to design drawings and technical requirements.
  5. 5. The method of designing a Ma Daxi-Qiyn puppet Peng Yuzhou airship base structure of claim 4, wherein the test is performed on the airship base structure after the modeling is completed, the steps further comprising: building a test platform and an environment; Applying different loads and stresses to the airship humerus base structure, observing the response and change of the humerus base structure, and evaluating the performance of the airship under various conditions; Simulating actions and postures in the flight process, observing the motion track and change rule of the humerus base structure, and checking whether the fit and connection of the humerus base structure and surrounding parts are normal or not; simulating load and stress under unexpected conditions, and observing stability and reliability of the humerus base structure; stability and durability of the humeral structure were evaluated by long time or repeated tests.
  6. 6. The method of designing a Ma Daxi-Qili puppet Peng Yuzhou airship base structure of claim 5, wherein the steps of optimizing and perfecting the airship base structure after the test is completed further include: Analyzing the data collected in the test process, identifying the problems and the defects, and determining the aspects of improvement and optimization; deep diagnosis and positioning are carried out on the problems in the testing process, and the nature and the influence range of the problems are determined; according to the result of the problem diagnosis, a corresponding optimization scheme is formulated; according to the optimization scheme, the design of the airship humerus base structure is improved; optimizing a process for manufacturing the airship humerus-based structure; Selecting or replacing proper materials according to the requirement of an optimization scheme; According to the improved design and optimization scheme, a model of the airship humerus base structure is manufactured again; And verifying the optimized and perfected airship humerus base structure.
  7. 7. A motor-west female puppet Peng Yuzhou airship-based structural material suitable for use in the method of designing a Ma Daxi-west female puppet Peng Yuzhou airship-based structure according to any one of claims 1 to 6.

Description

Moxiqi female puppet Peng Yuzhou airship humerus-based structural material and design method Technical Field The invention relates to the technical field of aerospace, in particular to a motor Xiqi female puppet Peng Yuzhou airship humerus base structural material and a design method. Background The humeral structure of a spacecraft refers to the support structure of the spacecraft, generally the connection and support structure between the main body portion of the spacecraft and the propulsion system, navigation system, etc. The humerus-based structure is a very important part in the design of spacecraft, and needs to bear various complex environments and loads, so as to ensure the stability and safety of the whole structure of the spacecraft. Meanwhile, the humerus base structure also needs to consider factors in the aspects of propulsion efficiency, mass distribution, heat dissipation performance and the like of the airship, so that various factors need to be comprehensively considered in the design process. Inspired by the evolution of everything in nature, intelligent bionic design has demonstrated many advantages in terms of functional materials and complex optimized structures, but a humeral base structure of a spacecraft with hui birds as the bionic design is not disclosed at present. Disclosure of Invention The invention aims to provide a motor Welch female puppet Peng Yuzhou airship humerus base structural material and a design method, which solve the problem that a humerus base structure of a spacecraft with hui birds as a bionic design is not disclosed at present. In order to achieve the above object, the present invention provides a design method of a motor Xiqi female puppet Peng Yuzhou airship humerus base structure, comprising the steps of: Deep research and observation of the humeral structure of hui birds; After the research data are obtained, applying the humerus base structure of hui birds to the design of the airship; After the design is completed, a model of the airship humerus base structure is manufactured; After the model is manufactured, testing the humerus base structure of the airship; After the test is finished, optimizing and perfecting the structure of the airship humerus base; When the performance and efficiency of the airship humerus base structure meet certain requirements, the method is applied to an actual space craft. Wherein, the humerus base structure of hui birds is deeply studied and observed, and the steps further comprise: Selecting hui bird samples; observing the appearance form of the humerus base structure of hui birds, including the overall form, size, color and texture of the humerus base structure, and simultaneously observing the connection mode and characteristics of the humerus base structure and surrounding tissues and whether abnormality or pathological change exists; the humeral structure of hui birds was studied in depth by anatomical means; The tissue sample with the humerus base structure is subjected to sheet making treatment, and the tissue structure and the cell composition of the tissue sample are observed through a microscope; performing biomechanical test on the humerus base structure of hui birds to obtain performance of the humerus base structure under different loads; Observing and researching the functional performance of hui birds on the humeral structure during flight; comparing and researching with other birds or living brachial base structures to obtain the uniqueness and advantages of hui bird brachial base structures; the collected data and observations are collated and analyzed, and the structure and function of the hui bird humerus base is interpreted and inferred in combination with biological, anatomical, and biomechanical principles and methods. Wherein, after obtaining the study data, the hui bird's humeral structure is applied to the design of the airship, the steps further include: The obtained research data are arranged and analyzed, and characteristics and rules of morphology, organization, function and biomechanics of the hui bird humerus base structure are extracted; according to the characteristics of hui bird humerus base structure in terms of form, material, connection mode and stability, a humerus base structure suitable for a spacecraft is designed. After the design is completed, a model of the airship humerus base structure is manufactured, and the method further comprises the following steps: Selecting materials according to design requirements and characteristics of a humerus base structure of the airship; determining a manufacturing process based on the selected materials and the complexity of the airship humerus base structure; and (3) manufacturing a model of the airship humerus base structure according to design drawings and technical requirements. After the model is manufactured, the airship humerus base structure is tested, and the method further comprises the following steps: building a test platform and an