摘要：In order to investigate the design method for a micro centrifugal compressor,which is the most important component of an ultra micro gas turbine,two types of centrifugal impeller with 2-dimensional blade were designed,manufactured and *** impellers have different shapes of hub on the meridional plane with each ***,these types of impeller were made for the 5 times and the 6 times size of the final target centrifugal impeller with the outer diameter of 4mm in order to assess the similitude for the *** comparison among the performance characteristics of the impellers revealed the influence of the meridional configuration on the performance and the similitude of the compressors.

摘要：以便建立设计一台极端微离心的压缩机的方法论，是一个极端微煤气的汽轮机单位的最重要的部件，最后的目标压缩机的 10 次尺寸(impeller 外部直径 40 公里，改正的旋转速度 220,000 r/min ) 被设计。为精简要解决的问题被检验，当第一由于它的生产率当模特儿， 2-dimensional impeller 被选择。常规 1D 预言方法和 CFD 被使用。建原型的压缩机被以 110,000 r/min 的减少的速度使用冷空气测试。对 10 次模型，后面期末考试的 5 次尺寸充分让 3-dimensional 塑造的目标模型(impeller 外部直径 20mm，改正的旋转速度 500,000 r/min ) 被以 250,000 r/min 的减少的速度使用热气体设计并且测试。关键词离心的压缩机 - 表演特征 - 3-dimensional impeller CLC 数字 TK474.

摘要：In order to establish the design methodology of ultra micro centrifugal compressor,wich is the most important component of ultra micro gas turbine unit,a 10 times of the final target size model was designed,prototyped and *** problems to be solved for downsizing were examined and 2-dimensional impeller was chosen as the first model due to its *** conventional 1D prediction *** and the inverse design were *** prototyped compressor was driven by using a turbocharger and the performance characteristics were measured.