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Thermal Management Solutions for Network File Server Used in Avionics Applications

机译:航空电子应用程序中使用的网络文件服务器的热管理解决方案

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In the modern era of commercial aviation there is an increasing need for establishing on-aircraft networks that interconnect legacy avionics systems for the purpose of data collection, health monitoring, and software management. At the heart of these networks are flight worthy file servers that perform similar functions to servers used in ground-based IT infrastructures. However, the size, weight, and power constraints for airborne servers are significantly more challenging than the constraints placed on ground-based equipment. As a result, the critical goals in the development of aircraft network systems are reducing the size and weight, maximizing the performance and reliability, and reducing cost. One of the main challenges includes dissipating high power in small packages within a confined space. This makes thermal management a critical component of the overall LRU (Line-Replaceable Unit) design. In addition, passive cooling systems are often required in place of internal fans in order to improve long-term reliability of the system. This presents another set of challenges, such as optimizing the airflow provided by the aircraft in the electronics compartment. This paper will present some of the critical elements of thermal management such as heat sinking, component placement, thermal interface materials, thermal vias, thermal links, heat spreader, packaging approaches and cooling strategies. The design and optimization of this system are based on analytical solutions, conjugated heat transfer and experimental results. Thermal management solutions must enable reliable operation under various environmental conditions: ground operation, flight operation, high operating temperature and loss of cooling air. Each environmental condition has different parameters for coolant airflow rate, effect of the surroundings, and ambient and coolant air temperature. Cooling airflow analyses were performed using CFD (Computational Fluid Dynamics). We have identified multiple approaches to remove heat from the critical components through optimization of the components and subsystems. These same approaches also serve to increase the system's performance and reliability.
机译:在商业航空的现代社会人们越来越需要建立在飞机网络,进行数据采集,健康监测,以及软件管理的目的互连传统的航空电子系统。在这些网络的心脏是执行类似的功能在使用的服务器飞行值得文件服务器基于地面的IT基础架构。然而,尺寸,重量,功率和机载服务器约束显著多于放置在地面设备的约束挑战。其结果是,在飞机网络系统发展的关键目标是减少体积和重量,最大限度地提高性能和可靠性,并降低成本。其中一个主要的挑战包括在密闭空间内小包装耗散高功率。这使得热管理整体LRU(现场可更换单元)设计的一个重要组成部分。此外,被动冷却系统通常需要在适当位置的内部风扇,以提高系统的长期可靠性。这带来了另外的挑战,如优化在电子室的飞机提供的气流。本文将介绍一些热管理的诸如散热,元件放置,热界面材料,热通孔,热链接中,散热器,封装方法和冷却策略关键元件。该系统的设计和优化是基于解析解,共轭传热和实验结果。热管理解决方案必须能够在各种环境条件下可靠工作:地面操作,飞行操作,高工作温度和冷却空气的损失。每个环境条件具有用于冷却剂气流速率,周围环境的影响,以及环境温度和冷却剂空气温度不同的参数。冷却气流分析使用CFD(计算流体动力学)进行。我们已经确定了多种方法来通过部件和子系统的优化从关键部件带走热量。这些相同的方法也有助于提高系统的性能和可靠性。

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