离心压气机管式扩压器研究进展及评述
收稿日期: 2016-11-17
修回日期: 2017-06-15
网络出版日期: 2017-06-26
基金资助
国家自然科学基金（51606187）；国防基础科研项目（B1320133025）
A review of studies on pipe diffuser of centrifugal compressor
Received date: 2016-11-17
Revised date: 2017-06-15
Online published: 2017-06-26
Supported by
National Natural Science Foundation of China (51606187);Defense Industry Technology Development Program (B1320133025)
韩戈 , 阳诚武 , 李紫良 , 赵胜丰 , 卢新根 . 离心压气机管式扩压器研究进展及评述[J]. 航空学报, 2017 , 38(9) : 520949 -520949 . DOI: 10.7527/S1000-6893.2017.620949
It is a great challenge to design a diffuser with both high performance and compact size. The compact and high performance design of diffusers has become the main technical limitation for the application of diffusers on high pressure ratio centrifugal compressors. Using pipe diffusers are recognized as an effective method to solve the tough diffuser design problem for high pressure ratio centrifugal compressors. Pipe diffusers have been used for advanced overseas small and medium jet engines. The performance of the centrifugal compressor has been improved evidently by using pipe diffusers. This review mainly introduces the research development of pipe diffusers home and abroad in two perspectives:first, the influences of design parameters of the pipe diffuser on the stage performance of the centrifugal compressor; second, the complex mechanism of the internal flow in pipe diffusers. The influence of the mechanism of internal flow in pipe diffuser on the performance of the centrifugal compressor is discussed, and some recommendations are made for the development of future research on pipe diffusers.
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