西北工业大学动力与能源学院,西安,710072
Published:2009
移动端阅览
SU San-mai, ZHANG Lei, CAI Yuan-hu, et al. Microturbo engine development and key technology analysis[J]. 2009, 24(11).
DOI:
SU San-mai, ZHANG Lei, CAI Yuan-hu, et al. Microturbo engine development and key technology analysis[J]. 2009, 24(11). DOI:
对国内外4 000 N推力级以下的导弹与无人机用典型系列微型涡轮发动机进行综述
主要包括发动机研制背景、发动机结构、性能参数、应用对象等内容.详细介绍了目前技术水平较先进的TJ100和推质比超过10的AT-1500系列发动机
总结了该类发动机的技术特点.最后
结合工程经验提出并分析了发动机研制的关键技术.
As powerplant of unmanned aerial vehicales(UAV) and cruise missile
microturbo engine has been developing quickly in recent years.In this paper
worldwide typical series microturbo engines with thrust below 4 000 N were summarized
covering the engine development background
structure
performance parameter and equipment/weapon object
etc.The newest developed TJ100 and AT-1 500 series of turbojets with thrust weight ratio over 10 were specially introduced.Based on above
common characteristics of this type of engine were discussed
and finally
seven key technologies during engine design
testing and manufacturing were proposed and analyzed by integrating real project engineering experience.
0
Views
680
下载量
CSCD
Publicity Resources
Related Articles
Related Author
Related Institution