Genetic Algorithm Optimization for Primary Surfaces Recuperator of MicroturbineSource: Journal of Engineering for Gas Turbines and Power:;2007:;volume( 129 ):;issue: 002::page 436DOI: 10.1115/1.2436550Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: In recent years, the genetic algorithm (GA) technique has gotten much attention in solving real-world problems. This technique has a strong ability for global searching and optimization based on various objectives for their optimal parameters. The technique may be applied to complicated heat exchangers and is particularly useful for new types. It is important to optimize the heat exchanger, for minimum volume/weight, to save fabrication cost or for improved effectiveness to save energy consumption, under the requirement of allowable pressure drop; simultaneously it is mandatory to optimize geometry parameters of heating plate from technical and economic standpoints. In this paper, GA is used to optimize the cross wavy primary surface (CWPS) and cross corrugated primary surface (CCPS) geometry characteristic of recuperator in a 100kW microturbine, in order to get more compactness and minimum volume and weight. Two kinds of fitness assignment methods are considered. Furthermore, GA parameters are set optimally to yield smoother and faster fitness convergence. The comparison shows the superiority of GA and confirms its potential to solve the objective problem. When the rectangular recuperator core size and corrugated geometries are evaluated, in the CWPS the weight of the recuperator decreases by 12% or more; the coefficient of compactness increases by up to 19%, with an increase of total pressure drop by 0.84% compared to the original design data; and the total pressure drop versus the operating pressure is controlled to be less than 3%. In the CCPS area compactness is increased to 70% of the initial data by decreasing pitch and relatively high height of the passage, the weight decreases by 17–36%, depending on the inclination angle (θ). Comparatively the CCPS shows superior performance for use in compact recuperators in the future. The GA technique chooses from a variety of geometry characters, optimizes them and picks out the one which provides the closest fit to the recuperator for microturbine.
keyword(s): Weight (Mass) , Microturbines , Optimization , Genetic algorithms , Design , Pressure drop , Geometry , Heat exchangers , Flow (Dynamics) , Pressure , Manufacturing AND Heat transfer ,
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contributor author | Wang Qiuwang | |
contributor author | Liang Hongxia | |
contributor author | Xie Gongnan | |
contributor author | Zeng Min | |
contributor author | Luo Laiqin | |
contributor author | Feng ZhenPing | |
date accessioned | 2017-05-09T00:23:44Z | |
date available | 2017-05-09T00:23:44Z | |
date copyright | April, 2007 | |
date issued | 2007 | |
identifier issn | 1528-8919 | |
identifier other | JETPEZ-26949#436_1.pdf | |
identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/135741 | |
description abstract | In recent years, the genetic algorithm (GA) technique has gotten much attention in solving real-world problems. This technique has a strong ability for global searching and optimization based on various objectives for their optimal parameters. The technique may be applied to complicated heat exchangers and is particularly useful for new types. It is important to optimize the heat exchanger, for minimum volume/weight, to save fabrication cost or for improved effectiveness to save energy consumption, under the requirement of allowable pressure drop; simultaneously it is mandatory to optimize geometry parameters of heating plate from technical and economic standpoints. In this paper, GA is used to optimize the cross wavy primary surface (CWPS) and cross corrugated primary surface (CCPS) geometry characteristic of recuperator in a 100kW microturbine, in order to get more compactness and minimum volume and weight. Two kinds of fitness assignment methods are considered. Furthermore, GA parameters are set optimally to yield smoother and faster fitness convergence. The comparison shows the superiority of GA and confirms its potential to solve the objective problem. When the rectangular recuperator core size and corrugated geometries are evaluated, in the CWPS the weight of the recuperator decreases by 12% or more; the coefficient of compactness increases by up to 19%, with an increase of total pressure drop by 0.84% compared to the original design data; and the total pressure drop versus the operating pressure is controlled to be less than 3%. In the CCPS area compactness is increased to 70% of the initial data by decreasing pitch and relatively high height of the passage, the weight decreases by 17–36%, depending on the inclination angle (θ). Comparatively the CCPS shows superior performance for use in compact recuperators in the future. The GA technique chooses from a variety of geometry characters, optimizes them and picks out the one which provides the closest fit to the recuperator for microturbine. | |
publisher | The American Society of Mechanical Engineers (ASME) | |
title | Genetic Algorithm Optimization for Primary Surfaces Recuperator of Microturbine | |
type | Journal Paper | |
journal volume | 129 | |
journal issue | 2 | |
journal title | Journal of Engineering for Gas Turbines and Power | |
identifier doi | 10.1115/1.2436550 | |
journal fristpage | 436 | |
journal lastpage | 442 | |
identifier eissn | 0742-4795 | |
keywords | Weight (Mass) | |
keywords | Microturbines | |
keywords | Optimization | |
keywords | Genetic algorithms | |
keywords | Design | |
keywords | Pressure drop | |
keywords | Geometry | |
keywords | Heat exchangers | |
keywords | Flow (Dynamics) | |
keywords | Pressure | |
keywords | Manufacturing AND Heat transfer | |
tree | Journal of Engineering for Gas Turbines and Power:;2007:;volume( 129 ):;issue: 002 | |
contenttype | Fulltext |