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contributor authorS. T. Adelman
contributor authorM. A. Hoffman
contributor authorJ. W. Baughn
date accessioned2017-05-08T23:47:15Z
date available2017-05-08T23:47:15Z
date copyrightJanuary, 1995
date issued1995
identifier issn1528-8919
identifier otherJETPEZ-26735#16_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/115330
description abstractSeveral illustrative designs are presented for a methane-steam reformer (MSR) that is used as a chemical recuperator in a Basic Chemically Recuperated Gas Turbine power cycle (a “Basic” CRGT is defined as one without intercooling or reheat). In this cycle, an MSR, heated by the turbine exhaust flow, converts a methane-steam mixture into a hydrogen-rich fuel that powers the gas turbine. A computer code was developed to calculate the size and performance characteristics of counterflow reformers. The code consists of a one-dimensional marching scheme that integrates the chemical, thermodynamic, and geometric variables along the heat exchanger/reformer tubes. The calculated designs were selected to give near-minimum catalyst volumes. These designs show that maintaining a high reformer gas temperature, using combustion-side heat transfer augmentation techniques, and using a catalyst of high reactivity are critical to obtaining a compact reformer design.
publisherThe American Society of Mechanical Engineers (ASME)
titleA Methane-Steam Reformer for a Basic Chemically Recuperated Gas Turbine
typeJournal Paper
journal volume117
journal issue1
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.2812768
journal fristpage16
journal lastpage23
identifier eissn0742-4795
keywordsGas turbines
keywordsMethane
keywordsSteam
keywordsMolten salt reactors
keywordsCatalysts
keywordsCycles
keywordsExhaust systems
keywordsHydrogen
keywordsPerformance characterization
keywordsMixtures
keywordsHeat exchangers
keywordsTurbines
keywordsComputers
keywordsFlow (Dynamics)
keywordsTemperature
keywordsHeat transfer
keywordsCombustion
keywordsFuels AND Design
treeJournal of Engineering for Gas Turbines and Power:;1995:;volume( 117 ):;issue: 001
contenttypeFulltext


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