气压站机械驱动用ORC轴流涡轮膨胀机的设计

L. Branchini, Cesar Celis, Sebastián Ruiz, R. Aguilar, A. D. Pascale, F. Melino
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引用次数: 0

摘要

本文研究了利用有机朗肯循环(ORC)提高天然气压缩站容量的可行性。在建议的配置中,ORC回收天然气压缩机驱动器的废热并将其转化为机械能。因此,作为创新的方法,ORC产生的机械动力将用于拖动额外的气体压缩机。并以某中型陆上设施为例进行了研究。机械驱动装置由4台pgt5r型回收式gt(3台连续运行,1台作为备用)和2台较小的太阳土星20型发动机组成。假设该站实际运行,增加一个ORC作为底部循环,用于回收三个pgt5r运行机组的废热。根据作者的初步调查和目前mw尺寸参数的现状,选择了再生亚临界ORC循环。分别选择热敏醇66和六甲基二硅氧烷(MM)作为中间体和工质。确定了设计ORC关键循环参数:可以增加约2700 hp (2 MW)的容量来驱动压缩机。为了进行综合研究,在假设三分之一的顶循环机组停止使用的情况下,还探讨了ORC非设计运行范围。由于预期ORC驱动器和气体压缩机直接耦合,因此不使用齿轮箱以避免损失,因此设计了基于ORC轴向涡轮的膨胀器,以适应变速操作。所述设计包括在设计和非设计点条件下的平均值线计算和基于三维计算流体力学(CFD)的数值模拟。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
On the Design of an ORC Axial Turbine Based Expander Working As a Mechanical Driver in Gas Compressor Stations
In this work, the feasibility of increasing the capacity of a natural gas compressor station by means of an Organic Rankine Cycle (ORC) is studied. In the proposed configuration, the ORC recovers natural gas compressor drivers’ wasted heat and converts it into mechanical energy. Thus, as innovative approach, the ORC generated mechanical power will be used to drag an additional gas compressor. A case study representative of a medium-size on-shore facility is taken as reference. The mechanical drivers’ arrangement is composed of four recuperated GTs of PGT5 R type (three units continuously operating and one used as back-up) and two smaller engines of Solar Saturn 20 type. Assuming the actual operation of the station, the addition of an ORC, as bottomer cycle, is designed to recover the exhaust heat from the three PGT5 R running units. According to the Authors’ preliminary investigations and state of the art MW-size parameters, a regenerative sub-critical ORC cycle is selected. Therminol 66 and Hexamethyldisiloxane (MM) are chosen as intermediate and working fluids, respectively. The design ORC key cycle parameters are identified: about 2700 hp (2 MW) of capacity could be added to drive a compressor. For a comprehensive investigation, ORC off-design operating range is explored too assuming one out of three topper cycle units out of service. Since a direct coupling of the ORC driver and the gas compressor is expected, thus excluding the use of gearboxes to avoid losses, an ORC axial turbine based expander is designed that accommodates variable speed operation. The referred design includes mean-line calculations and three-dimensional computational fluid dynamics (CFD) based numerical simulations at design and off design point conditions.
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