Mathematical Analysis for Off-Design Performance of Cryogenic Turboexpander

Author:

Ghosh Subrata K.1,Sahoo R. K.2,Sarangi Sunil K.2

Affiliation:

1. Department of ME and MME, ISM, Dhanbad, Jharkhand 826004, India

2. NIT Rourkela, Orissa 769008, India

Abstract

A study has been conducted to determine the off-design performance of cryogenic turboexpander. A theoretical model to predict the losses in the components of the turboexpander along the fluid flow path has been developed. The model uses a one-dimensional solution of flow conditions through the turbine along the mean streamline. In this analysis, the changes of fluid and flow properties between different components of turboexpander have been considered. Overall, turbine geometry, pressure ratio, and mass flow rate are input information. The output includes performance and velocity diagram parameters for any number of given speeds over a range of turbine pressure ratio. The procedure allows any arbitrary combination of fluid species, inlet conditions, and expansion ratio since the fluid properties are properly taken care of in the relevant equations. The computational process is illustrated with an example.

Publisher

ASME International

Subject

Mechanical Engineering

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4. Modeling of Twin-Entry Radial Turbine Performance Characteristics Based on Experimental Investigation Under Full and Partial Admission Conditions;Hajilouy;Transaction B: Mechanical Engineering, Scientia Iranica

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