Computer-aided Design of Axial Flow Turbine Structure of Aviation GTE
- 10.2991/itids-19.2019.6How to use a DOI?
- expert system, choice of material, gas turbine engine, strength calculations, computer-aided design, node mass estimation
The article discusses the issues of modeling the design of axial turbines of aircraft engines. Modeling is carried out using the developed expert decision-making system "AM". The advantage of using this system in the early stages of engine design is shown. This advantage is achieved by selecting the most optimal material for the main assembly units of an aircraft engine based on various calculations that represent the mathematical model of the expert system. It is shown that the expert system in addition to the selection of material also carries out the selection of measures to improve the resistance of the material to the external environment, and the recommended modes of surface treatment. As an example, the results of computer-aided design of the elements of the flow channel of high and low pressure turbine assemblies of a two spool turbojet engine with afterburner and mixed flow for a 4th generation military highly mobile aircraft are given. The results of the design simulation are compared with the actual design of the prototype engine. Comparison of the results is carried out both in terms of geometrical parameters (diametrical dimensions of the flow part and the dimensions of the chords of the nozzle assembly and blades), and in terms of mass characteristics.
- © 2019, the Authors. Published by Atlantis Press.
- Open Access
- This is an open access article distributed under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).
Cite this article
TY - CONF AU - Igor Krivosheev AU - Alexander Kishalov AU - Vadim Lipatov PY - 2019/05 DA - 2019/05 TI - Computer-aided Design of Axial Flow Turbine Structure of Aviation GTE BT - Proceedings of the 7th Scientific Conference on Information Technologies for Intelligent Decision Making Support (ITIDS 2019) PB - Atlantis Press SP - 34 EP - 39 SN - 1951-6851 UR - https://doi.org/10.2991/itids-19.2019.6 DO - 10.2991/itids-19.2019.6 ID - Krivosheev2019/05 ER -