Published June 2018 | Version v1
Journal article

Overall performance design of paralleled heat release and compression system for hypersonic aeroengine

  • 1. School of Energy and Power Engineering, Beihang University, Beijing, 100191 (China)

Description

Highlights: • The system is based on paralleled flow path and frequent heat transfer processes. • System working principle, performance, and effects are studied for the first time. • The system can dramatically improve the economy performance of the engine. • The system can considerably reduce the difficulty of turbomachinery design. • Future research directions and potential applications are summarized. The hydrogen powered hypersonic precooled combined cycle engine is an ideal candidate for next generation high speed clean civil aviation propulsion. It utilizes the energy inside the high speed air flow to power the air compression, in order to improve engine performance. Paralleled heat release and compression system, with several separated channels, is proved to be a crucial component to guarantee the favourable performance of the hypersonic precooled combined cycle engine. The system can sharply reduce the fuel consumption and cycle compressor pressure ratio (over 34% reduction in fuel consumption and over 45% reduction in cycle compressor pressure ratio, compared with ordinary single-route flow path design). The system is theoretically and quantitatively analysed. Operation mechanism, parameters design, feasibility and installing effects of the system are discussed. A performance simulation model is built for the paralleled system. The equivalent component method is proposed for measuring its effect on the engine overall performance. Inside the system, higher compression efficiency, lower pressure loss, more branches, higher heat transfer capacity and heat exchanger effectiveness can enhance the performance, while the feasible region, weight and size effects, and technical risks cannot be ignored either. For the engine, the installation of the paralleled system remarkably improves the engine performance and simplifies the compressor design. The paralleled system, with its advantage of coolant flow and compression work reduction, also can be beneficial to other applications in energy and power field.

Availability note (English)

Available from http://dx.doi.org/10.1016/j.apenergy.2018.03.062

Additional details

Identifiers

DOI
10.1016/j.apenergy.2018.03.062;
PII
S0306261918303982;

Publishing Information

Journal Title
Applied Energy
Journal Volume
220
Journal Page Range
p. 36-46
ISSN
0306-2619
CODEN
APENDX

INIS

Country of Publication
United Kingdom
Country of Input or Organization
International Atomic Energy Agency (IAEA)
INIS RN
52106964
Subject category
S42: ENGINEERING;
Descriptors DEI
AIR FLOW; COMBINED CYCLES; COMPRESSION; COMPRESSORS; COOLANTS; ENGINES; FUEL CONSUMPTION; HEAT EXCHANGERS; HEAT TRANSFER; HEATING; HYDROGEN; PERFORMANCE; SIMULATION; TURBOMACHINERY
Descriptors DEC
ELEMENTS; ENERGY CONSUMPTION; ENERGY TRANSFER; EQUIPMENT; FLUID FLOW; GAS FLOW; MACHINERY; NONMETALS; THERMODYNAMIC CYCLES

Optional Information

Copyright
Copyright (c) 2018 Elsevier Ltd. All rights reserved.