Abstract
In view of the problems of the traditional aero engine development, such as the design elements are difficult to reuse, the traceability of requirements is not good and lack of top-level logic verification, the model based systems engineering (MBSE) method is introduced. Apply the Harmony for Systems Engineering to the top-down design flow of aero-engine turbine system. The system requirement model is established through the creation and classification of turbine system requirements and the definition of system use cases. To establish the function model, the functional, expressive, interface, and other requirements are transformed into a clear description of the system function. The system architecture is analyzed and designed on the basis of the system function, then the function of each use case is decomposed and allocated into the subsystems and components of turbine system. Based on the system model, the requirements of the system are refined, traced and verified. The results show that the MBSE method can perfect the requirement definition, complete the mapping of the requirements to the system elements, realize the function logic verification, and support requirements verification at all stages, which provides an effective practical approach for the development of aero-engine.
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References
Engineering ICOS (2015) INCOSE Systems Engineering Handbook: A Guide for System Life Cycle Processes and Activities
Cordova L, Kovich C, Sargusingh M (2012) An MBSE Approach to Space Suit Development
Vipavetz K, Shull TA, Infeld S, Price J (2016) Interface management for a NASA flight project using model-based systems engineering (MBSE). Incose Int Symp 26(1):1129–1144
Spangelo SC, Kaslow D, Delp C, Cole B (eds) (2012) Applying Model Based Systems Engineering (MBSE) to a standard CubeSat. In: Aerospace Conference
Spangelo SC, Cutler J, Anderson L, Fosse E, Cheng L, Yntema R et al (eds) (2013) Model based systems engineering (MBSE) applied to Radio Aurora Explorer (RAX) CubeSat mission operational scenarios. In: Aerospace Conference
Parthasarathi H, Ramachandra S, Srinivasamurthy PN (2016) Model-based systems engineering for aero gas turbine engine subsystems. Incose Int Symp 26(s1):70–82
Delligatti L (2013) SysML Distilled: A Brief Guide to the Systems Modeling Language. Addison-Wesley Professional
Hans-PeterHoffmann (2014)
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Chen, Z., Wang, Y., Zhang, Y., Li, T. (2019). MBSE Approach to Aero-Engine Turbine System Design and Requirements Management. In: Zhang, X. (eds) The Proceedings of the 2018 Asia-Pacific International Symposium on Aerospace Technology (APISAT 2018). APISAT 2018. Lecture Notes in Electrical Engineering, vol 459. Springer, Singapore. https://doi.org/10.1007/978-981-13-3305-7_139
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DOI: https://doi.org/10.1007/978-981-13-3305-7_139
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