Aero-engine strength design method

A technology of aero-engines and design methods, applied in the direction of calculation, special data processing applications, instruments, etc., to achieve the effect of improving accuracy and efficiency, improving overall design and management level, and promoting development

Active Publication Date: 2019-11-22
AECC SHENYANG ENGINE RES INST
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  • Claims
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Problems solved by technology

[0012] The purpose of this application is to provide an aeroengine strength desig...

Method used

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  • Aero-engine strength design method

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Embodiment Construction

[0038] In order to make the purpose, technical solution and advantages of the application more clear, the technical solution in the embodiment of the application will be described in more detail below in conjunction with the drawings in the embodiment of the application.

[0039] like figure 1 As shown, the aeroengine strength design method of the present application includes the following contents:

[0040] 1. Design input

[0041] Criteria, specifications, guidelines and other relevant specifications for aeroengine strength design activities are specified as design input.

[0042] 2. Sorting out the strength design process

[0043] Strength design is divided into overall load strength design, blade strength design, wheel strength design, main shaft strength design, casing strength design, combustion chamber strength design, composite casing strength design, threaded connection strength design, and machine strength design9 According to the strength design specification, so...

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Abstract

The invention relates to an aero-engine strength design method, which belongs to the field of aero-engine strength design. The method mainly comprises the steps of determining design input of aero-engine strength; carding professional design flows involved in strength design according to related data of aero-engine strength design; determining a design activity of typical intensity according to the carded design flow; designing a whole strength design process, matching strength design factors, judging the engineering adaptability of the strength design method, if the use requirements are met,obtaining a strength design result and process data, and if the use requirements are not met, adjusting typical design activities and iterating until the use requirements are met. According to the aero-engine design method, the strength design precision and efficiency can be improved, the required design process and design elements can be rapidly and accurately obtained, and unification of strength design standardization and flexibility is achieved.

Description

technical field [0001] The application belongs to the technical field of aero-engine strength design, in particular to an aero-engine strength design method. Background technique [0002] In recent years, with the rapid development of the aviation industry, the task of aeroengine design has become increasingly heavy, and the workload of simulation analysis of the structural strength design of the whole machine and components has also increased. With the development of strength specialty and the deepening of research, a relatively complete design system has been established, including strength design process, normative design elements, software tools and process database. To apply the design system to model strength design better, and at the same time improve the design system with the help of model development experience, the following problems need to be solved: [0003] 1) Improve the binding and operability of the process; [0004] 2) The strength design process needs t...

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Application Information

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IPC IPC(8): G06F17/50
Inventor 王威耿瑞宋洋王相平曹航赵娜葛长闯
Owner AECC SHENYANG ENGINE RES INST
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