微型涡喷发动机装配关键技术
Key Techniques of Micro Turbojet Engine Assembly
Received date: 2017-10-31
Online published: 2025-05-29
王航洲 , 胡智玺 , 刘建国 , 李永生 . 微型涡喷发动机装配关键技术[J]. 弹箭与制导学报, 2018 , 38(5) : 82 -84 . DOI: 10.15892/j.cnki.djzdxb.2018.05.020
Assembly technique is an important link to ensure the product performance, reliability and life The micro turbojet engine assembly procedure is complex; the assembly precision should be very high and it is hard to ensure the assembly quality. To solve the problems above, combing the practical application, this paper puts forward and analyzes the key technologies of the micro turbojet engine assembly. The results show that the techniques can guide the assembly of the micro turbojet engine.
Key words: micro turbojet engine; assembly technique
| [1] | 《航空发动机设计手册》总编委会. 航空发动机设计手册[M]. 北京: 航空工业出版社, 2000: 153-462. |
| [2] | 刘长福. 航空发动机构造[M]. 北京: 国防工业出版社, 1989: 81-88. |
| [3] | 程进杰, 孙郁, 孙立佳, 等. 高速透平转子的动平衡试验研究[J]. 低温与超导, 2014, 42(6): 6-9. |
| [4] | 腾瑞静, 张余斌, 周晓军, 等. 圆柱面过盈连接的力学特性及设计方法[J]. 机械工程学报, 2012, 48(13): 160-166. |
| [5] | 张敬佩, 李初晔. 过盈配合产生的接触压力和拔出力计算[J]. 机械工程与自动化, 2011(1): 195-198. |
| [6] | 王大磊, 朴英. 叶尖间隙高度对某高压涡轮级损失分布的影响[J]. 航空动力学报, 2012, 27(1): 169-475. |
/
| 〈 |
|
〉 |