摘要
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。
Analysis specific measures of firing weapons and fighters to preventing engine surge in flight,The prevention of anti-surge controller on the engine size of the structure of the impact of anti-surge and anti-surge devices are given specific advice to improve the design,study Boost limiter system structural parameters relationship with anti-surge process of the cutting oil.
出处
《装备制造技术》
2011年第2期19-20,共2页
Equipment Manufacturing Technology
关键词
飞机
发动机
喘振
防喘
aircraft
engine
surge
anti-surge
