Evaluation of the relationship between the aerothermodynamic process and operational parameters in the high-pressure turbine of an aircraft engine
Autor: | Phuong Tri Nguyen, Trung Hieu Nguyen, François Garnier |
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Rok vydání: | 2019 |
Předmět: |
0209 industrial biotechnology
business.industry Rotor (electric) Flow (psychology) Process (computing) Aerospace Engineering 02 engineering and technology 01 natural sciences Turbine 010305 fluids & plasmas law.invention 020901 industrial engineering & automation Flow velocity law 0103 physical sciences Turbomachinery Water cooling Environmental science Takeoff Aerospace engineering business |
Zdroj: | Aerospace Science and Technology. 86:93-105 |
ISSN: | 1270-9638 |
DOI: | 10.1016/j.ast.2019.01.011 |
Popis: | Gaining a full understanding of the aerothermodynamic (AT) process in the high-pressure turbine of an aircraft engine is a complex task. The data in the literature on this topic are very limited, particularly that on tridimensional simulation. We report herein, for the first time, the designs, computer simulations, tridimensional calculations of the interactions of AT parameters under various operation conditions (takeoff, cruise) of an aircraft engine by using a refined mesh system containing approximately 6 million polyhedrons and more than 1 million interactions to solve equations in a high-pressure turbine (HPT). Our research provides, for the first time, an overview of high-resolution topographic images of the distribution of AT parameters in multi-row turbomachinery. Our calculations indicate that the relationship between these parameters was convoluted and depended on each operating condition. For example, our findings show that the thermal boundary conditions and rotor speeds strongly affected the flow temperatures (14%) and flow velocity (31%). On the other hand, the cooling system appeared not to affect AT parameters. The temperature nonuniformities in the turbine in the axial and radial directions were also observed. |
Databáze: | OpenAIRE |
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