Patent
Multistage axial flow compressor
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TLDR
In this paper, a multistage axial flow compressor with stacked stages in an axial direction is described, each stage including a rotor and a stator, and the rotor and vane heights decrease from stage to stage in the direction of exiting fluid flow from the compressor.Abstract:
A multistage axial flow compressor with stacked stages in an axial direction, each stage including a rotor and a stator. The stages include vanes of identical vane geometry throughout the stator stages and the blades are of identical blade geometry throughout the several rotor stages. The blade and vane heights decrease from stage to stage in the direction of exiting fluid flow from the compressor. A constant hub diameter is maintained throughout the several rotor stages.read more
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