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Experimental study of a controlled variable double-baffle distortion generator engine test rig
Authors:Aiguo XIA  Xudong HUANG  Wei TUO  Ming ZHOU
Institution:1. School of Aerospace Engineering, Tsinghua University, Beijing 100084, China;2. Beijing Aeronautical Technology Research Center, Beijing 100076, China
Abstract: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.
Keywords:Distortion generator  Engine stability  Inlet flow  Inlet total-pressure distortion  Turbofan engines
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