Modeling and mode transition simulation of over-under turbine based combined cycle (TBCC) propulsion system based on inlet/engine matching

被引：8

作者：

Gao, Yuan ^{[1
]}

Xi, Zhihua ^{[1
]}

Hu, Chenxu ^{[1
]}

Zhang, Haibo ^{[1
]}

机构：

[1] Nanjing Univ Aeronaut & Astronaut, JiangSu Prov Key Lab Aerosp Power Syst, 29 Yudao St, Nanjing 210016, Peoples R China

来源：

INTERNATIONAL JOURNAL OF TURBO & JET-ENGINES | 2023年 / 40卷 / 02期

关键词：

inlet; engine matching; mode transition; modeling; simulation;

D O I：

10.1515/tjj-2020-0038

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

The over-under turbine based combined cycle (TBCC) propulsion system dynamic model is established, including the engine model and inlet model. A dual-channel inlet is designed to match the engine and the inlet performance parameters are obtained by computational fluid dynamics (CFD) calculation, which provides original data for the integrated Inlet/Engine matching model. Control plan is designed to ensure that the engine is not over-temperature, over-rotation or surging based on correlation analysis. The simulation results show that the designed control plan can keep the TBCC propulsion system continuous in thrust during the mode transition, and the thrust fluctuation is about 10%.

引用

页码：171 / 181

页数：11

共 50 条

[41] A rocket-based combined-cycle engine prototype demonstrating comprehensive component compatibility and effective mode transition
Shi, Lei
He, Guoqiang
Liu, Peijin
Qin, Fei
Wei, Xianggeng
Liu, Jie
Wu, Lele
ACTA ASTRONAUTICA, 2016, 128 : 350 - 362
[42] Process Modeling System of a Combined Cycle Plant for Steady State Simulation with Model Based Approach
Kim, Shin Hyuk
Hwang, Lee Si
Joo, Yong Jin
Lee, Sang Uk
Shon, Byung Mo
Oh, Min
KOREAN CHEMICAL ENGINEERING RESEARCH, 2015, 53 (05): : 545 - 552
[43] Experimental study of rocket plume expansion in the rocket-based combined-cycle engine under the ejector mode
Yao, Yizhi
Sun, Mingbo
Huang, Yuhui
Li, Peibo
An, Bin
Zhang, Dongdong
Gu, Rui
Li, Menglei
Wang, Taiyu
Chen, Jikai
Wang, Jiaoru
AEROSPACE SCIENCE AND TECHNOLOGY, 2023, 138
[44] Performance analysis and dynamic optimization of integrated cooling and power generation system based on supercritical CO2 cycle for turbine-based combined cycle engine
Ma, Xiaofeng
Jiang, Peixue
Zhu, Yinhai
APPLIED THERMAL ENGINEERING, 2022, 215
[45] Effect of the heat release on ejector-to-ramjet dynamic mode transition process in the rocket-based combined cycle engine
Hu, Yu-Peng
Liu, Yuan-Shu
Wang, Yi-Jun
Zhou, Ben-Quan
Zheng, Xing
Xue, Rui
INTERNATIONAL COMMUNICATIONS IN HEAT AND MASS TRANSFER, 2023, 140
[46] Modeling and Simulation of a PMSG-based Marine Current Turbine System under Faulty Rectifier Conditions
Toumi, Sana
Benelghali, Seifeddine
Trabelsi, Mohamed
Elbouchikhi, Elhoussin
Amirat, Yassine
Benbouzid, Mohamed
Mimouni, Mohamed Faouzi
ELECTRIC POWER COMPONENTS AND SYSTEMS, 2017, 45 (07) : 715 - 725
[47] Numerical simulations on a rocket-based combined cycle engine in ejector mode under sea-level static conditions
Shi, Lei
He, Guo-Qiang
Qin, Fei
Guti Huojian Jishu/Journal of Solid Rocket Technology, 2013, 36 (03): : 310 - 317
[48] Modeling and performance analysis of a pre-cooling and power generation system based on the supercritical CO2 Brayton cycle on turbine-based combined cycle engines
Ma, Xiaofeng
Jiang, Peixue
Zhu, Yinhai
ENERGY, 2023, 284
[49] Adaptive Robust Unit Commitment of Combined-Cycle Gas-Turbine Considering Mode-Based Modeling of Carbon Capture Plant
Wang, Luyu
Jiang, Boyou
Shi, Yunhui
Chen, Zhe
IEEE ACCESS, 2023, 11 : 34510 - 34528
[50] Finite-time control for polynomial parameter-varying systems and its application in mode transition of turbine-based combined cycle engines
Yu, Lianchen
Yang, Chenlong
Sun, Hongfei
Zeng, Jianping
TRANSACTIONS OF THE INSTITUTE OF MEASUREMENT AND CONTROL, 2025,

← 1 2 3 4 5 →