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Integrative energy-systems design: System structure from thermodynamic optimization.

机译:一体化能源系统设计:热力学优化的系统结构。

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This thesis deals with the application of thermodynamic optimization to find optimal structure and operation conditions of energy systems. Chapter 1 outlines the thermodynamic optimization of a combined power and refrigeration system subject to constraints. It is shown that the thermodynamic optimum is reached by distributing optimally the heat exchanger inventory. Chapter 2 considers the maximization of power extraction from a hot stream in the presence of phase change. It shows that when the receiving (cold) stream boils in a counterflow heat exchanger, the thermodynamic optimization consists of locating the optimal capacity rate of the cold stream. Chapter 3 shows that the main architectural features of a counterflow heat exchanger can be determined based on thermodynamic optimization subject to volume constraint. Chapter 4 addresses two basic issues in the thermodynamic optimization of environmental control systems (ECS) for aircraft: realistic limits for the minimal power requirement, and design features that facilitate operation at minimal power consumption. Several models of the ECS-Cabin interaction are considered and it is shown that in all the models the temperature of the air stream that the ECS delivers to the cabin can be optimized for operation at minimal power. In chapter 5 it is shown that the sizes (weights) of heat and fluid flow systems that function on board vehicles such as aircraft can be derived from the maximization of overall (system level) performance. Chapter 6 develops analytically the optimal sizes (hydraulic diameters) of parallel channels that penetrate and cool a volume with uniformly distributed internal heat generation and Chapter 7 shows analytically and numerically how an originally uniform flow structure transforms itself into a nonuniform one when the objective is to minimize global flow losses. It is shown that flow maldistribution and the abandonment of symmetry are necessary for the development of flow structures with minimal resistance. In the second part of the chapter, the flow medium is continuous and permeated by Darcy flow. As flow systems become smaller and more compact, the flow systems themselves become “designed porous media”.
机译:本文研究了热力学优化方法在寻找能源系统的最佳结构和运行条件方面的应用。第1章概述了受约束的电力和制冷系统的热力学优化。结果表明,通过优化分配热交换器库存可以达到热力学最优。第2章考虑了在存在相变的情况下从热流中提取功率的最大化。它表明,当接收(冷)流在逆流换热器中沸腾时,热力学优化包括确定冷流的最佳容量率。第三章表明,逆流热交换器的主要结构特征可以基于受体积约束的热力学优化来确定。第4章讨论了飞机环境控制系统(ECS)的热力学优化中的两个基本问题:最小功率要求的实际限制,以及有助于以最小功率运行的设计功能。考虑了多种ECS-机舱相互作用模型,结果表明,在所有模型中,ECS输送至机舱的气流温度都可以优化,以最小的功率运行。在第5章中,可以从整体(系统级)性能的最大化中得出在飞机等飞机上运行的热量和流体流动系统的大小(重量)。第6章通过分析得出在内部热量产生均匀分布的情况下渗透并冷却一定体积的平行通道的最佳尺寸(液压直径),而第7章则通过分析和数值分析得出了当目标是将原始均匀的流动结构转变为不均匀的流动结构时的方法。最大程度地减少总体流量损失。结果表明,流动的不均匀分布和对称性的放弃是发展阻力最小的流动结构所必需的。在本章的第二部分,流动介质是连续的,并被达西流渗透。随着流量系统变得越来越小,越来越紧凑,流量系统本身也变成了“设计的多孔介质”。

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