New Mathematical and Software Method at Logic and Condition Monitoring System of Helicopter Turboshaft
محل انتشار: کنگره بین المللی علوم مهندسی و توسعه شهری پایدار
سال انتشار: 1397
نوع سند: مقاله کنفرانسی
زبان: انگلیسی
مشاهده: 418
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شناسه ملی سند علمی:
DTUCONF01_098
تاریخ نمایه سازی: 1 دی 1397
چکیده مقاله:
Following a dramatic increase in the use of helicopters and increase in turboshafts to the global market,it isnecessary for these helicopters tobe tested in order toensure their engines arein good working order. Since the engine is its palpitating heart of every aircraft system,the software utilizes a thermodynamic model to assist a helicopter’s engine in stabilize and standby conditions. With the assistance of this software, it is possible to predict the effects of engine defects on the measured performance of the aircraft. A two-step process hasbeen designed to determine the maximum output power of a real turboshaft engine without requiring a motor operating at maximum power. The similar software in this field of engine design, the GSP and GasTurb10 can be named but none of them are specialized in field of turboshaft.
کلیدواژه ها:
نویسندگان
Farshid Bazmi
Aerospace Engineering
Saeid Keshtkar Garousi
Mathematicsand Computer Science
Negin Loghmani
Computer Engineering
Afsaneh Khaghaniazar
Mathematics and Computer Science