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TRANSITION IN GAS TURBINE CONTROL SYSTEM ARCHITECTURE: MODULAR, DISTRIBUTED AND EMBEDDED

机译:燃气轮机控制系统架构中的过渡:模块化,分布式和嵌入式

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摘要

Controls systems are an increasingly important component of turbine-engine system technology. However, as engines become more capable, the control system itself becomes ever more constrained by the inherent environmental conditions of the engine; a relationship forced by the continued reliance on commercial electronics technology. A revolutionary change in the architecture of turbine-engine control systems will change this paradigm and result in fully distributed engine control systems. Initially, the revolution will begin with the physical decoupling of the control law processor from the hostile engine environment using a digital communications network and engine-mounted high temperature electronics requiring little or no thermal control. The vision for the evolution of distributed control capability from this initial implementation to fully distributed and embedded control is described in a roadmap and implementation plan. The development of this plan is the result of discussions with government and industry stakeholders.
机译:控制系统是涡轮发动机系统技术的越来越重要的组成部分。然而,由于发动机变得更大,因此控制系统本身因发动机固有的环境条件而变得更加约束;继续依赖商业电子技术的关系。涡轮发动机控制系统架构的革命性变化将改变该范例并导致完全分布式的发动机控制系统。最初,革命将从敌对的发动机环境中使用数字通信网络和发动机安装的高温电子设备开始对控制法处理器的物理解耦,需要很少或没有热控制。从该初始实施方式到完全分布和嵌入式控制的分布式控制能力的演变的愿景描述于路线图和实施计划中。该计划的发展是与政府和行业利益攸关方进行讨论的结果。

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