通过对燃气轮机增压站压缩机性能曲线的分析，对压缩机防喘振控制逻辑进行了分析及改进。
The control logic preventing the compressor from surge was analyzed and improved after the performance curve of compressor in gas turbine booster station was analyzed.
最终给出了一台40公斤推力级、低增压比为3.0的单叶轮微涡扇发动机的丰富数据和特性曲线。
Eventually given a 40 kg thrust class, low-pressurized than 3.0 single-turbofan engine micro-impeller rich data and characteristic curves.
应用推荐