A Numerical Study for Flow Excitation and Performance of Rampressor Inlet considering Rotor Motion

Abstract

A unique supersonic compressor rotor with high pressure ratio, termed the Rampressor, is presented by Ramgen Power Systems, Inc. (RPS). In order to obtain the excitation characteristic and performance of Rampressor inlet flow field under external excitation, compression inlet flow of Rampressor is studied with considering Rampressor rotor whirling. Flow excitation characteristics and performance of Rampressor inlet are analyzed under different frequency and amplitude of Rampressor rotor whirling. The results indicate that the rotor whirling has a significant effect for flow excitation characteristics and performance of Rampressor inlet. The effect of rotor whirling on the different inlet location excitation has a definite phase difference. Inlet excitation becomes more complex along with the inlet flow path. More frequency components appear in the excitation spectrum of Rampressor inlet with considering Rampressor rotor whirling. The main frequency component is the fundamental frequency, which is caused by the rotor whirling. Besides the fundamental frequency, the double frequency components are generated due to the coupling between inlet compression flow of Rampressor rotor and rotor whirling, especially in the subsonic diffuser of Rampressor rotor inlet. With the increment of rotor whirling frequency and whirling amplitude, the complexity of Rampressor inlet excitation increases, and the stability of Rampressor inlet performance deteriorates.

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“…Corresponding author, Dr.Sc., E-mail: a.kuzmin@spbu.ru Supersonic flow in curved channels is also of interest for the design of rampressors, which are compressors operating at high peripheral speeds necessary to achieve supersonic effect in a stationary environment. Han et al (2009) and Kang et al (2014) investigated the performance of rampressors and flow excitation characteristics under different frequencies and amplitudes of rampressor rotor whirling. Feng et al (2017a, b) performed a numerical and experimental study of supersonic flow in a bent channel which models a variable geometry dual mode combustor.…”