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Title: A parametric analysis microcomputer model for evaluating the thermodynamic performance of a reciprocating Brayton cycle engine

Journal Article · · Journal of Engineering for Gas Turbines and Power; (USA)
DOI:https://doi.org/10.1115/1.3240294· OSTI ID:7002261
 [1];  [2]
  1. Mechanical Engineering Dept, Portland State Univ, Portland, OR (US)
  2. Bonneville Power Administration, Portland, OR (US)

A Brayton open-cycle engine is under development. It operates similarly to a gas turbine engine, but uses reciprocating piston compressor and expander components. The design appears to have a number of advantages, including multifuel capability, the potential for lower cost, and the ability to be scaled to small sizes without significant loss in efficiency. An interactive microcomputer model has been developed that analyzes the thermodynamic performance of the engine. The model incorporates all the important irreversibilities found in piston devices, including heat transfer, mechanical friction, pressure losses, and mass loss and recirculation. There are 38 input parameters to the model. Key independent operating parameters are maximum temperature, compressor rpm, and pressure ratio. The development of the model and its assumptions are outlined in this paper. The emphasis is on model applications.

OSTI ID:
7002261
Journal Information:
Journal of Engineering for Gas Turbines and Power; (USA), Vol. 111:1; ISSN 0742-4795
Country of Publication:
United States
Language:
English