CIVILICA We Respect the Science
(ناشر تخصصی کنفرانسهای کشور / شماره مجوز انتشارات از وزارت فرهنگ و ارشاد اسلامی: ۸۹۷۱)

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

عنوان مقاله: Design of high-pressure piston pump for the application of aerospace
شناسه ملی مقاله: CARSE04_002
منتشر شده در چهارمین کنفرانس بین المللی پژوهش های کاربردی در علوم و مهندسی در سال 1398
مشخصات نویسندگان مقاله:

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

خلاصه مقاله:
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.

کلمات کلیدی:
Piston Pump, Propeller, Hydrogen Peroxide, Low pressure tanks, signal valve

صفحه اختصاصی مقاله و دریافت فایل کامل: https://civilica.com/doc/1000526/