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第四代发动机不加力超声巡航性能的研究
引用本文:屠秋野,唐狄毅.第四代发动机不加力超声巡航性能的研究[J].航空动力学报,2001,16(3):300-304.
作者姓名:屠秋野  唐狄毅
作者单位:1. 中国船舶科学研究中心,
2. 西北工业大学七系,
摘    要:本文基于改善第四代发动机不加力超声巡航性能这一目标 ,提出了合理配置发动机地面设计点高压物理转速和节流比的设计思想 ,并结合冷超转和燃气储备利用技术进行性能寻优 ,大大提高了发动机的高空速度特性。

关 键 词:发动机  超音速  巡航飞行
文章编号:1000-8055(2001)03-0300-05
收稿时间:2000/8/30 0:00:00
修稿时间:2000年8月30日

Study on Non-Augmented Supersonic Cruise of the 4th Generation Engines
TU Qiu-ye and TANG Di-yi.Study on Non-Augmented Supersonic Cruise of the 4th Generation Engines[J].Journal of Aerospace Power,2001,16(3):300-304.
Authors:TU Qiu-ye and TANG Di-yi
Institution:TU Qiu-ye~1,TANG Di-yi~2 1.China Ship Science Research Center,Wuxi214082,China, 2.7th Dept.,Northwest Polytechnic University,Xi'an710072,China
Abstract:In order to improve the non augmented supersonic cruise performance of the 4th generation engine,an idea for designing is proposed,which consists in rational matching of the high pressure rotor physical speed to the throttle ratio at ground design point and utilization of the "cold overrun" and "gas temperature storage" techniques for performance optimization.A realization of the ides is carried out.It is proven that the velocity characteristics of the engine is improved to a great extent and the optimal thrust characteristics of the engine are provided in a broad range of the flight Mach numbers.
Keywords:engine  supersonic  cruing flight  performance
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