The scramjet engine usually employs a fuel regeneration cooling system to cool the walls. As a highly efficient thermal engine, the supercritical carbon dioxide (S-CO2) cycle system can recover and utilize heat energy to generate electricity to power equipment while reducing the amount of fuel needed for cooling and effectively enhancing the engine's overall performance. An overall parametric analysis of the cooling system for the scramjet engine is conducted based on the supercritical CO2 cycle power generation system, obtaining a system-generated power output of 65kW and a cycle efficiency of 11.75%. Additionally, the impact of various parameters is evaluated such as compressor pressure ratio, turbine inlet temperature, engine heat input, compressor inlet temperature, compressor isentropic efficiency, and turbine isentropic efficiency on system power generation and efficiency. Using a multi-objective genetic algorithm, the maximum power output and efficiency of the system are assessed, and preliminary designs for key components including the precooler and compressor are conducted.
| 科 Family | 属数 Number of genus | 种数 Number of species | 占总种数比例 Percentage of total species (%) | 属 Genus | 种数 Number of species | 占总种数比例 Percentage of total species (%) |
|---|---|---|---|---|---|---|
| 鹅膏菌科Amanitaceae | 2 | 11 | 5.26 | 鹅膏菌属 Amanita | 10 | 4.78 |
| 小菇科 Mycenaceae | 2 | 12 | 5.74 | 丝盖伞属 Inocybe | 5 | 2.39 |
| 多孔菌科 Polyporaceae | 8 | 14 | 6.70 | 蜡蘑属 Laccaria | 5 | 2.39 |
| 红菇科 Russulaceae | 3 | 23 | 11.00 | 小皮伞属 Marasmius | 6 | 2.87 |
| 小菇属 Mycena | 11 | 5.26 | ||||
| 光柄菇属 Pluteus | 5 | 2.39 | ||||
| 红菇属 Russula | 17 | 8.13 | ||||
| 栓菌属 Trametes | 5 | 2.39 |