کد مقاله کد نشریه سال انتشار مقاله انگلیسی نسخه تمام متن
10226387 1701267 2018 14 صفحه PDF دانلود رایگان
عنوان انگلیسی مقاله ISI
Experimental study of a controlled variable double-baffle distortion generator engine test rig
ترجمه فارسی عنوان
آزمایش تجربی یک متغیر کنترل متغیر کنترل دیفرانسیل دیفرانسیل دیفرانسیل موتور تست
کلمات کلیدی
ژنراتور تحریف ثبات موتور، جریان ورودی، اعوجاج فشار ورودی کامل موتور توربو فن،
موضوعات مرتبط
مهندسی و علوم پایه سایر رشته های مهندسی مهندسی هوافضا
چکیده انگلیسی
In order to explore the total-pressure distortion test assessment method for a turbofan engine, a Controlled Variable Double-Baffle Distortion Generator (CVDBDG) with a horizontal symmetry moving form was developed, which can adjust the steady-state and time-variant distortion separately in real time. The inlet total-pressure distortion test was conducted on an afterburner turbofan engine. The distortion parameters of CVDBDG and the instability characteristics of the engine were measured. The experimental data were modeled and analyzed by using back propagation artificial neural networks, and the work envelope of CVDBDG was obtained. Based on the analysis of the data on the engine's instability, the properties of CVDBDG used for the stability assessment were preliminarily evaluated. The results show that CVDBDG can simulate both steady-state and time-variant distortions simultaneously in a range determined by three envelopes. Under the condition of symmetric double baffles, a critical depth of insertion exists, beyond which the symmetric baffles will generate an asymmetric flow field. In the case of double baffles, compared to a single baffle, the engine exhibited different instability characteristics. Based on CVDBDG, it is expected that more efficient engine stability and durability assessment methods can be developed.
ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: Chinese Journal of Aeronautics - Volume 31, Issue 9, September 2018, Pages 1880-1893
نویسندگان
, , , ,