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An Improved Methodology for Gas Turbine Technology Portfolio Planning, Including Technology Synergy Matrices and Real Options Analysis

机译:一种改进的燃气轮机技术组合计划方法,包括技术协同矩阵和实物期权分析

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The management of technologies remains a challenging and risky constituent of gas turbine component design. The performance impact of a single new technology on a gas turbine component is often uncertain, requiring statistical methods to fully quantify. The inclusion of multiple new technologies further complicates gas turbine component performance prediction because there may be significant non-linear technology interactions. When designing gas turbine components to operate within the context of a fully specified gas turbine engine, each component introduces its own mix of new technologies. Because gas turbine components are linked thermodynamically, a new technology in one component may induce secondary impacts in other engine components. Thus, technology portfolio analysis for gas turbines is further complicated by the dynamics of component interaction. In this paper, a new technology portfolio planning methodology is presented that directly addresses these three inherent complexities of gas turbine component design. This methodology includes Technology Impact Matrices to quantify component level technology impacts as well as Technology Compatibility Matrices and Technology Synergy Matrices to account for non-linear component level technology interactions. Through surrogate modeling, a physics-based dynamic engine model is formed that quickly translates component technology impacts into total-system thermodynamic performance. Real Options analysis is used to translate engine performance metrics to net engine economic performance. Finally, a probabilistic multi-objective genetic algorithm is used to discover a robust Pareto front of optimal technology combinations with respect to system level thermodynamic and economic performance metrics. This paper first describes the proposed methodology in detail. Next, a benchmark gas turbine technology portfolio problem is outlined. Finally, a baseline technology portfolio planning methodology and the newly proposed methodology are both executed upon the benchmark problem, allowing for the benefits of the new methodology to be quantified.
机译:技术管理仍然是燃气轮机组件设计中具有挑战性和风险性的组成部分。单一新技术对燃气轮机部件的性能影响通常是不确定的,因此需要统计方法才能完全量化。由于可能存在重大的非线性技术交互作用,因此包含多种新技术会使燃气轮机部件性能的预测更加复杂。当设计燃气轮机部件以在完全指定的燃气轮机发动机内运行时,每个部件都会引入自己的新技术组合。因为燃气轮机组件是热力学链接的,所以一个组件中的一项新技术可能会在其他发动机组件中引起二次冲击。因此,由于部件相互作用的动力学,使得燃气轮机的技术组合分析更加复杂。在本文中,提出了一种新的技术组合计划方法,可以直接解决燃气轮机组件设计的这三个固有的复杂性。该方法包括用于量化组件级技术影响的技术影响矩阵,以及用于说明非线性组件级技术交互的技术兼容性矩阵和技术协同矩阵。通过代理建模,形成了基于物理的动态引擎模型,该模型可快速将组件技术的影响转化为整个系统的热力学性能。实物期权分析用于将发动机性能指标转换为发动机净经济性能。最后,使用概率多目标遗传算法来发现关于系统级热力学和经济绩效指标的最优技术组合的鲁棒帕累托前沿。本文首先详细介绍了所提出的方法。接下来,概述了基准燃气轮机技术组合问题。最后,基准技术组合计划方法和新提出的方法均在基准问题上执行,从而可以量化新方法的收益。

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