Design of high-pressure piston pump for the application of aerospace

Publish Year: 1398
نوع سند: مقاله کنفرانسی
زبان: English
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شناسه ملی سند علمی:

CARSE04_002

تاریخ نمایه سازی: 17 اسفند 1398

Abstract:

In this study, the performance and how to build a high-pressure pump as a feeding system for pressurizing fuel and an oxidizing to convey the flow and pressure in the combustion chamber and labor conditions will be used. This system will be active until the engine has finished working. The use of this pump in jet engines is suitable for high environmental pressure and high ambient temperature as well as fuel injection pressure in various conditions. In this approach, the first step is to explain how the pump works and performs, also, using MATLAB and FLUENT software, we perform various tests and check the performance of the pump. In the end, the results are analyzed, and the function that is expected from the pump is checked.

Authors

abbasali saboktakin

Assistant Professor of Mechanical Engineering, sistan and blochestan university, zahedan, iran

mohammad monjezi

mechanical engeneering, sistan and blochestan university, zahedan, iran

sadeq qiassi

mechanical engeneering, sistan and blochestan university, zahedan, iran