某发动机最大状态控制计划试飞方法研究

摘要

A predication model of an engine inlet total temperature is gained through analyzing flight test data of an aircraft which equipped with the engine.According the engine inlet total temperature predication model,the flight test method of the engine maximum condition control scheme is designed and planned.The test result shows that the engine inlet total temperature predication model provides an effective guidance on the engine maximum condition control scheme flight test,and improves the flight test efficiency and saves the resource.Besides,the test result also shows that the engine maximum condition control scheme works effectively,and guarantees the flight test safety.%首先对某飞机飞行数据进行总结，得到某发动机入口总温的预测模型。根据得到的发动机入口总温预测模型，对发动机最大状态控制计划试飞方法进行设计规划。试飞结果显示：发动机入口总温预测模型有效指导了发动机最大状态控制计划试飞，提高了试验效率，节省了试验资源；该发动机最大状态控制计划控制有效，保证了发动机最大状态工作可靠。