The Latest Development of Turboshaft Engines
DOI:
https://doi.org/10.54097/hset.v71i.12709Keywords:
Turboshaft engines, compressor, performance, surge, efficiency.Abstract
As the main power of rotor aircraft, the turboshaft engine has always been the focus of scientific and engineering research and has achieved rich research results. This paper reviews and summarizes the research results at home and abroad in the past 10 years from the aspects of control systems, oil-electric mixing, pollutant emission and compressor internal flow field optimization. High altitude and low temperature is the best condition for turboshaft engine operation. Pre-mission fuel estimation is good for low emissions. Oil-electric mixing engines can effectively improve efficiency, but reducing weight and cost is a problem that needs to be solved. The interaction between the leakage vortex and the excitation wave in the compressor increases the total pressure loss in the vortex core downstream of the excitation wave. The modes associated with wheezing can be stabilised by feeding back small-amplitude perturbations. The universality of the surge suppression of transonic centrifugal compressors and the stability of most of the compressor surges by small disturbance feedback are the next research focus.
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Mehrdad Pakmehr,Nathan Fitzgerald,Eric M. Feron,Jeff S. Shamma,Alireza Behbahani, “Gain Scheduled Control of Gas Turbine Engines: Stability and Verification,”Journal of Engineering for Gas Turbines and Power,MARCH 2014, Vol. 136 / 031201.
Jesus Ortiz-Carretero,Alejandro Castillo Pardo,Ioannis Goulos,Vassilios Pachidis, “Impact of Adverse Environmental Conditions on Rotorcraft Operational Performance and Pollutant Emissions,”Journal of Engineering for Gas Turbines and Power,FEBRUARY 2018, Vol. 140 / 021201.
Ioannis Goulos,Fakhre Ali,Konstantinos Tzanidakis,Vassilios Pachidis Roberto d’Ippolito, “A Multidisciplinary Approach for the Comprehensive Assessment of Integrated Rotorcraft–Powerplant Systems at Mission Level,” Journal of Engineering for Gas Turbines and Power,JANUARY 2015, Vol. 137 / 012603.
Fakhre Ali, Ioannis Goulos, Vassilios Pachidis, “A Preliminary Design Tradeoff Study for an Advanced Propulsion Technology Rotorcraft at Mission Level,”Journal of Engineering for Gas Turbines and Power,JANUARY 2016, Vol. 138 / 012602.
Chana Anna Saias,Ioannis Roumeliotis,Ioannis Goulos,Vassilios Pachidis,Marko Bacic, “Design Exploration and Performance Assessment of Advanced Recuperated Hybrid-Electric Urban Air Mobility Rotorcraft,”Journal of Engineering for Gas Turbines and Power,MARCH 2022, Vol. 144 / 031023.
Seiichi Ibaraki, Tetsuya Matsuo,Hiroshi Kuma,Kunio Sumida,Toru Suita, “Aerodynamics of a Transonic Centrifugal Compressor Impeller,”Transactions of the ASME,Vol. 125, APRIL 2003.
Nicolas Poujol,Isabelle Trébinjac,Pierre Duquesne, “Effects of Inlet Guide Vanes on the Performance and Stability of an Aeronautical Centrifugal Compressor,”Journal of Turbomachinery,OCTOBER 2021, Vol. 143 / 101010.
Fangyuan Lou,Herbert M. Harrison,Nicole L. Key, “Investigation of Surge in a Transonic Centrifugal Compressor With Vaned Diffuser—Part I: Surge Signature,”Journal of Turbomachinery,MAY 2023, Vol. 145 / 051003.
E. B. Nelson,J. D. Paduano,A. H. Epstein, “Active Stabilization of Surge in an Axicentrifugal Turboshaft Engine,”Journal of Turbomachinery, JULY 2000, Vol. 122.
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