文献类型：期刊文献

英文题名：Dynamic thermo-physical characteristics of high temperature gaseous hydrocarbon fuel thermal power generation for regeneratively cooled hypersonic propulsion system

作者：Xu, Qing[1,2];Li, Haowei[1,2];Feng, Yaoxun[1,2];Li, Xiaoning[1,2];Ling, Changming[1,2];Zhou, Chaoying[3];Qin, Jiang[4]

机构：[1]Guangdong Ocean Univ, Sch Mech & Power Engn, Dept Thermal Power & Power Engn, 1 Haida Rd, Zhan Jiang 524088, Peoples R China;[2]Southern Marine Sci & Engn Guangdong Lab Zhanjian, Zhanjiang, Peoples R China;[3]Harbin Inst Technol, Dept Mech Engn & Automat, Shenzhen Sch, Shenzhen 518055, Peoples R China;[4]Harbin Inst Technol, Sch Energy Sci & Engn, Harbin 150001, Peoples R China

年份：2020

卷号：211

外文期刊名：ENERGY

收录：SCI-EXPANDED(收录号：WOS:000589890900011)、、EI(收录号：20203609139002)、Scopus(收录号：2-s2.0-85090167737)、WOS

基金：This research was funded by the Fund of Southern Marine Science and Engineering Guangdong Laboratory (ZJW-2019-01), the General program of Natural Science Foundation of Guangdong Province, China (No. 2019A1515011551) and the Project of Fundamental Research of Shenzhen Science and Technology Plan (No. JCYJ20170307151117299).

语种：英文

外文关键词：Dynamic thermos-physical characteristics; Hydrocarbon fuel; Thermal power generation (TPG); Thermo-mechanical coupling effect; Hypersonic air-breathing propulsion

外文摘要：Power generation is urgent needed by the hypersonic air-breathing propulsion system, but the on-board power generation method is heavily restricted by its special structure. The outlet high temperature hydrocarbon fuel of the cooling channel in the hypersonic propulsion system can be used to generate power. However, the hydrocarbon fuel temperature is highly related with hypersonic propulsion system dynamic working conditions. To analyze the dynamic thermos-physical characteristics of high temperature hydrocarbon fuel thermal power generation (TPG) system, a zero-dimensional dynamic analytical model was developed, dynamic characteristics of the TPG system under different working conditions were conducted. Results show that there is overshoot of outlet fuel temperature under flight Mach number increase conditions and fuel equivalence ratio decrease conditions, which can be more than 10 K. Whilst there are both negative and positive overshoot of the generated power under the above working conditions, the largest magnitude of negative and positive overshoot can be more than 1 kW. Furthermore, the dynamic time of outlet fuel temperature and generated power are about 20-30s. Such complexity of dynamic characteristics brings difficulties in fuel supply for the propulsion system. (C) 2020 Elsevier Ltd. All rights reserved.