首页 | 本学科首页   官方微博 | 高级检索  
     检索      

某型发动机外场温度高问题的排故
引用本文:尚义,张保安,陈筱雄.某型发动机外场温度高问题的排故[J].航空动力学报,1992,7(4):317-318,394.
作者姓名:尚义  张保安  陈筱雄
作者单位:南京航空学院210016
摘    要:本文讨论了某型发动机温度高问题,并提出了解决这一故障的措施,包括在修理厂如何严格把关和外场如何合理调整,在可靠工作的前提下,尽量减少对飞机战术性能的影响。 

关 键 词:涡轮喷气发动机    排气温度高    排故
收稿时间:4/1/1991 12:00:00 AM

ELIMINATION OF OVERTEMPERATURE IN TURBOJET
Shang Yi,Zhang Baoan and Chen Xiaoxing.ELIMINATION OF OVERTEMPERATURE IN TURBOJET[J].Journal of Aerospace Power,1992,7(4):317-318,394.
Authors:Shang Yi  Zhang Baoan and Chen Xiaoxing
Institution:Nanjing Aeronautical Institute
Abstract:This paper analyzes the reasons of the overtemperature in a turbojet andprovides the available measures to eliminate it, such as the strict requirements for the engine overhaul at the repair factory and the reasonable engine adjustment in the field maintenance. It is essential for the field maintenance to adjust properly the relationship between the turbine pressure ratio and the exhaust nozzle area, so that the turbine gas temperature comes down without afterburning temperature drop. In this way, the influence of the above problem on the operational performance of the engine can be minimized on condition that the engine reliability is guaranteed.
Keywords:
本文献已被 CNKI 等数据库收录!
点击此处可从《航空动力学报》浏览原始摘要信息
点击此处可从《航空动力学报》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号