The customer, one of the world’s leading HVAC manufacturers, required the design of a new range of chillers using R1234ze(E) refrigerant. The chiller uses a 2-stage in-line compressor. Both compressors and the return channel need to be designed.
This webinar presents the redesign of an electrically driven mixed flow transonic compressor by using a 3D inverse design methodology. The compressor will be used for an active high-lift system application that aims to delay the onset of stall and thus contributing to the reduction of both the aircraft noise footprint and the impact of aviation emission on local air quality.
This paper presents the redesign of an electrically driven mixed flow transonic compressor by using a 3D Inverse Design methodology. The compressor will be used for an active high-lift system application that aims to delay the onset of stall.
The aim for this project was to design a refrigeration compressor stage using R134a to improve performance of the entire stage (impeller, vaneless diffuser and volute) and to meet various flow rates and pressure ratio requirements by trimming the impeller.
In this paper on designing turbomachinery components for supercritical CO2 using 3D Inverse Design you can learn about the development of supercritical CO2 and the challenges it presents.
In the present paper, the redesign of a transonic rotor was performed by means of a three-dimensional viscous inverse design method. The inverse approach used in this work is one where the pressure loading, blade thickness distribution and stacking axis are specified and the camber surface is calculated accordingly