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Towards Operationally Robust Fuel Cell Systems for Aeronautical Applications

机译:对航空应用的操作鲁棒燃料电池系统

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Fuel cell technology will play a decisive role in the process of achieving the ambitious ecological goals of the aviation industry. However, apart from its obvious environmental advantages, the integration of fuel cell technology into commercial aircraft represents a challenging task in terms of operational and economical aspects. Since fuel cell systems are currently exposed to an intense competition with well-established power sources onboard an aircraft, engineers are in pursuit of highly efficient and particularly lightweight fuel cell systems. Supported by model-based design in conjunction with elaborate optimization techniques this pursuit has led to highly specialized systems. These systems tend to use their components to full capacity, which typically implies marginal system robustness. In consequence, preliminary design studies propose fuel cell systems that are sensitive to partial faults, or even to the slightest deviation, or degradation of their components' behavior. Non-functional requirements such as reliability, availability, dispatchability and durability will become key factors for the acceptance of fuel cells as alternative power sources onboard aircraft. These requirements demand the taking of coordinated measures in both Systems Architecting and Sizing, since the potential of measures such as adding redundancy to the system's architecture or making use of modular approaches is directly bound to the reliability of subsystems and their components. A component's reliability, however, strongly depends on its operating point and thus on the operating point of connected components. Hence, an operation envelope-oriented sizing of subsystems and components becomes an important factor. This paper reveals and illustrates the crucial issue of highly sensitive, high-performance fuel cell systems and proposes and discusses measures regarding Systems Architecting and Sizing in order to enhance the system's operational robustness while still keeping track of key performance indicators such as weight and efficiency.
机译:燃料电池技术将在实现航空业的雄心勃勃的生态目标方面发挥决定性作用。然而,除了其明显的环境优势之外,燃料电池技术将燃料电池技术集成到商业飞机上,在运营和经济方面方面是一个具有挑战性的任务。由于燃料电池系统目前暴露于飞机上造成良好的电源的激烈竞争,因此工程师正在追求高效且特别轻巧的燃料电池系统。通过基于模型的设计支持,与精心设计的优化技术相结合,这种追踪导致了高度专业化的系统。这些系统倾向于使用它们的组件来满足,这通常意味着边际系统的鲁棒性。结果,初步设计研究提出了对部分断层敏感的燃料电池系统,甚至是最轻微的偏差,或者组件行为的劣化。非功能性要求,如可靠性,可用性,调度性和耐用性,将成为接受燃料电池作为替代电源的替代电源的关键因素。这些要求需要在系统架构和规模中采取协调措施,因为诸如向系统架构添加冗余或利用模块化方法等措施的可能性直接绑定了子系统及其组件的可靠性。然而,组件的可靠性强烈取决于其操作点,从而依赖于连接组件的操作点。因此,子系统和组件的定向封装尺寸的操作尺寸成为一个重要因素。本文揭示并说明了高度敏感,高性能的燃料电池系统的关键问题,并提出了关于系统架构和尺寸的措施,以提高系统的运行稳健性,同时仍然跟踪重量和效率等关键性能指标。

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