面向高超声速民机的多通道双涡轮引射冲压组合动力

doi:10.7527/S1000-6893.2022.27181

Abstract

Abstract:

The reusable turbine-based combined cycle engine for wide-space/speed range aircraft is a revolutionary technology attracting global attention. Firstly， this paper briefly describes the state-of-the-art of turbine-based combined cycle engines， and then focusing on the technical characteristics and research progress of the presented Multi-ducted Twin-Turbines Ejector-Ramjet/scramjet （MUTTER） combined cycle engine for hypersonic civil aircraft. Different from conventional turbine-based combined cycle engines，MUTTER uses the distinctive symmetrical configuration of four engine ducts. An ejector engine is placed in the ramjet duct to bridge the thrust gap between the twin turbine engines and the ramjet/scramjet engine. A scaled and staged research and verification plan is introduced， and the study on the core sub-systems shows that the inlet and nozzle sub-systems can work stably and efficiently in the wide-space/speed range， and the ejector ramjet engine sub-system can effectively match with other sub-systems. In addition， the aircraft/engine integration features of the present combine cycle engine are discussed. Finally， some conclusions are drawn from our previous work.

Key words: turbine based combined cycle engine, multi-ducts inlet and nozzle, twin-turbines, ejector ramjet, aircraft/engine integration

CLC Number:

V211.1

Zeyong YIN, Yancheng YOU, Chengxiang ZHU, Jianfeng ZHU, Liaoni WU, Yue HUANG. Multi-ducted twin-turbines ejector-ramjet/scramjet combined cycle engine for hypersonic civil vehicles[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(2): 627181-627181.

Figures/Tables 19

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Multi-ducted twin-turbines ejector-ramjet/scramjet combined cycle engine for hypersonic civil vehicles

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