分析了战斗机在发射武器和飞行过程中,预防发动机喘振的具体措施,探讨了预防喘调节器各结构尺寸对发动机防喘的影响,并给出了防喘装置改进设计的具体意见,研究了升压限制器的结构参数与系统防喘切油过程的关系。 The specific measures to prevent engine surge in the process of launching weapons and flight were analyzed. The effects of preventing various structural sizes of asthma regulators on engine anti-asthma were also discussed. Specific suggestions for improving the design of anti-asthma devices were given. Relationship between structural parameters of boost limiters and anti-skid oil cutting process of the system.