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Investigation of measures improvement of turbine constructive element gas turbine engine cooling for middle range aircrafts

Репозитарій Національного Авіаційного Університету

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Title Investigation of measures improvement of turbine constructive element gas turbine engine cooling for middle range aircrafts
 
Creator Bakalo, Evhenii Mykolayovich
 
Subject durability
NDT
diagnostics
engines
thermal-mechanical design
thermodynamic cycle
 
Description Робота публікується згідно наказу ректора від 29.12.2020 р. №580/од "Про розміщення кваліфікаційних робіт вищої освіти в репозиторії НАУ" . Керівник проекту: доцент, к. т. н. Хімко Андрій Миколайович.
Advanced heat transfer and cooling techniques form one of the major pillars supporting the continuing development of high efficiency, high power output gas turbine engines. Conventional gas turbine thermal management technology is composed of five main elements including internal convective cooling, external surface fi lm cooling, materials selection, thermal-mechanical design at the component and system levels, and selection and/or pre-treatment of the coolant fluid.
The technology of cooling gas turbine components, primarily via internal convective flows of single-phase gases and external surface fi lm cooling with air, has developed over the years into very complex geometries involving many differing surfaces, architectures, and fluid-surface interactions. The fundamental aim of this technology area is to obtain the highest overall cooling effectiveness with the lowest possible penalty on the thermodynamic cycle performance. As a thermodynamic Brayton cycle, the efficiency of the gas turbine engine can be raised substantially by increasing the fi ring temperature of the turbine. Modern gas turbine systems are fired at temperatures far in excess of the material melting temperature limits.
 
Date 2021-02-24T13:12:26Z
2021-02-24T13:12:26Z
2020-12
 
Type Learning Object
 
Identifier https://er.nau.edu.ua/handle/NAU/47741
 
Language en
 
Format application/pdf
 
Publisher National Aviation University
 

Технічна підтримка: НДІІТТ НАУ