期刊名称:International Journal of Advances in Engineering and Management
电子版ISSN:2395-5252
出版年度:2021
卷号:3
期号:6
页码:97-103
DOI:10.35629/5252-030625092512
语种:English
出版社:IJAEM JOURNAL
摘要:In the modern world’s aviation system and transport system gas internal combustion engines plays a main role because of its excellent advantages and applications mainly the speed which provides to the vehicle. This paper gives the deep introduction to the turbo jet engine as this mainly works on the Newton’s 3rd rule. For this work a simple turbo jet engine is designed by referring some other sources, this design consists of inlet vanes. Compressor vanes, centre rotating shaft where the vanes are located, inner walls of combustion chamber. Here we also mention the objectives of the turbo jet engine based on their applications. This work is concentrated on the structural static analysis work and the modal analysis of the designed turbo jet engine. The main objective of this work is to find out the stresses, strains, strain energy, and fatigue life of the designed model by structural static analysis when we use structural steel as a material and we also tend to find out the structural vibrations through modal analysis in which the structure deform in particular shapes when excited in their natural frequencies.