军用中型涡桨运输机高温高原性能设计的分析

Analysis on High Temperature Plateau Performance Design of Military Medium Turboprop

文章介绍军用中型涡桨运输机高温高原性能的主要设计思路,并从高原典型机场运力的优化设计、动力装置与飞机气动外形一体化设计、起飞襟翼状态的优化设计、高原轮胎与刹车装置的设计等方面入手,阐述飞机高温高原性能优化设计的主要方案内容,并结合试飞试验确定相应优化方案的实效性。

This article introduces the main design ideas for high-temperature plateau performance of military medium-sized turboprops,from the optimization design of the typical plateau airport capacity,the integrated design of the power plant and the aircraft aerodynamic shape,the optimization design of the take-off flap state,the plateau tires and Starting with the design of the brake device,the main program content of the optimization design of the aircraft's high temperature plateau performance is explained,and the actual effect of the corresponding optimization program is determined in combination with the flight test.