一种用于稳态和瞬态评估的先进空气路径试验台的设计

R. Vijayakumar, R. Burke, Yang Liu, J. Turner
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引用次数: 0

摘要

不同的空气系统,如涡轮增压器(TC)、混合动力增压、涡轮增压和废气再循环(EGR),越来越多地用于提高内燃机(ICE)的热效率。一维(1D)气体动态代码通过对发动机和空气系统进行建模并减少测试时间,支持其开发和集成。然而,这种方法目前依赖于稳态流动特性图,这对于模拟瞬态发动机条件是不准确的。这是在发动机模拟中使用气站测量图的一个关键弱点。在发动机上进行TC映射原则上可以解决这个问题,但是基于发动机的映射受到发动机工作范围的限制,在这些设备上,高精度测量具有挑战性。此外,简单的涡轮增压不再局限于单个TC向发动机提供增压空气。相反,现代小型化发动机需要使用多种组件的气路系统,包括tc、机械增压器、电动压缩机(EDCs)、EGR路径和控制阀。因此,研究多个空气系统需要一个实验测试设施,以了解他们如何协同工作。这在开发经验模型以最小化测试时间方面也很有用。因此,本文的目的是提出一种新颖的实验装置,该装置设计灵活,既可以单独评估空气系统,也可以在系统层面上评估稳定和瞬态状态下复杂的空气路径。这台先进的测试设备围绕一台2.2升柴油发动机而建,用于测试上述空气系统,这些空气系统可以隔离发动机脉动流中的热瞬态和负载瞬态。消除流动脉动可以在稳定状态下研究系统特性。讨论了几个组件和系统级测试的例子,包括由VGT(可变几何涡轮)TC和48V EDC组成的两级空气路径,具有典型的工作条件(由1D建模提供)。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Design of an Advanced Air Path Test Stand for Steady and Transient Evaluation
Different air systems such as turbochargers (TC), hybrid boosting, turbo compounding and exhaust gas recirculation (EGR) are increasingly used to improve the thermal efficiency of internal combustion engines (ICE). One dimensional (1D) gas dynamic codes supports their development and integration by modelling the engine and air systems and reducing testing time. However, this approach currently relies on steady flow characteristic maps which are inaccurate for simulating transient engine conditions. This is a key weakness of using gas-stand measured maps in engine simulations. Performing TC mapping on an engine would in principle solve this problem, however engine-based mapping is limited by the engine operating range and on these facilities, high-precision measurements are challenging. In addition, simple turbocharging can no longer be constrained to an individual TC supplying boost air to an engine. Instead, modern downsized engines require air-path system making use of multiple components including TCs, mechanical superchargers, electrically driven compressors (EDCs), EGR paths and control valves. Thus studying multiple air systems requires an experimental test facility to understand how they work in synergy. This is also useful in developing empirical models to minimize test time. Therefore the aim of this paper is to present a novel experimental facility that is flexibly designed for evaluating air systems individually and also at the system level representing a complicated air path both in steady and transient condition. The advanced test facility is built around a 2.2 l diesel engine to test the above air systems which can isolate the thermal and load transients from engine pulsating flows. Removing the flow pulsation allows study of the system characteristics in a steady state. Several examples of component and system level tests including a two-stage air path comprising of a VGT (variable geometry turbine) TC and a 48V EDC with typical operating condition (provided by 1D modeling) are discussed.
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