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THE EFFECTS OF WET COMPRESSION WITH FUEL INJECTION AT THE GEOMETRY AND THE DESIGN POINT PERFORMANCE OF AN AXIAL COMPRESSOR

机译:湿润压缩与轴向压缩机的燃料喷射的影响和轴向压缩机的设计点性能

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Over the past few years, an intensive effort has been put forth to reduce gas turbine engine generated pollutants, as well as fuel consumption. The current research team understanding the motives behind this effort, suggests an alternative method of wet compression that of using fuel as a cooling medium. Fundamentally, the method of wet compression with fuel injection is based on the same principles of wet compression incorporating water injection. However, there are some considerable differences between the two approaches. A thorough comparison has been carried out revealing each method's advantages and disadvantages. Following the initial comparison of the two methods, the study goes a step further by investigating the applicability of wet compression incorporating fuel. The investigation has taken into account the characteristics of the axial flow compressor where a typical aviation fuel was injected. However, in order to acquire all the necessary information before putting method's applicability into context, the differences between dry compression and wet compression with fuel injection were examined. In this new approach, the compressor is the engine component where the fuel is injected first, thus a preliminary design study was carried out along an axial compressor's mean radius line. Finally the computation has been carried out for both dry and wet compression techniques. Compressor's specifications were similar to J85's compressor whereas fuel's specifications were based on JP-8's properties. Compressor's geometry and design point performance, were computed using a mean line analysis domestic code. A brief analysis of the code will be given, including both the initial version that was used for the dry compression calculations, as well as the modified one that was used for the wet compression calculations. After that, the presentation of the results follows. Finally, the paper will be concluded with a discussion of the findings and wet compression's with fuel injection perspectives.
机译:在过去的几年里,已经提出了一种密集的努力来减少燃气轮机发动机产生的污染物,以及燃料消耗。目前的研究团队了解这项努力背后的动机,建议使用燃料作为冷却介质的替代方法。从根本上说,燃料喷射的湿式压缩方法基于包含注水的湿压缩原理。然而,两种方法之间存在相当大的差异。已经进行了彻底的比较,揭示了每种方法的优点和缺点。在两种方法的初始比较之后,通过研究诸如燃料的湿压缩的适用性进一步进一步进一步逐步。调查考虑了轴流压缩机的特性,其中注入典型的航空燃料。然而,为了在将方法适用于上下文之前获取所有必要的信息,检查干压缩与燃料喷射湿压缩之间的差异。在这种新方法中,压缩机是首先注入燃料的发动机部件,因此沿轴向压缩机的平均半径线进行初步设计研究。最后,已经为干燥和湿式压缩技术进行了计算。压缩机的规格类似于J85的压缩机,而燃料的规格则基于JP-8的特性。压缩机的几何形状和设计点性能,使用均值分析国内代码计算。将给出对代码的简要分析,包括用于干压缩计算的初始版本,以及用于湿式压缩计算的修改后的版本。之后,遵循结果的呈现。最后,将通过讨论燃料喷射观点的研究结果和湿润压缩的讨论结束。

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