优化SGT-A35 (GT61),在整个负载范围内改善排放和提高效率

Deepak Thirumurthy, B. Ruggiero, Gautam Chhibber, Jaskirat Singh
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引用次数: 1

摘要

RT61是一种三级工业动力涡轮机,与SGT-A35航空衍生气体发生器(以前命名为工业RB211)耦合。它的设计是为了提高效率和模块化结构,便于维护。航空衍生产品SGT-A35 (GT61)服务于油气和发电市场,机队规模超过90台。近年来,清洁能源得到了越来越多的重视,只有监管变化和市场条件才能加以补充。发电和油气客户(上游、中游和下游)一直在寻找通过提高燃气轮机循环效率来减少温室气体排放和降低燃料消耗的机会。SGT-A35 (GT61)动力涡轮机具有> 93%的等熵效率和100,000小时的工业标准大修计划。然而,通过将动力涡轮机的容量优化到特定的负载范围,存在进一步提高循环效率和减少排放的潜力。这是这项技术工作的主要动机。本文讨论了在实施上述改进和进一步优化产品以减少排放方面所做的工程努力。在产品层面和TransCanada pipeline车队层面讨论了这些改进。在客户项目的要求下,开发了一种新的动力涡轮机变体。我们进行了详细的开发项目,以建立新的操作点、空气动力学设计和新的几何形状。它针对客户项目特定的负载范围进行了优化。在制造阶段,采用了新颖的快速成型方法来实现所需的交货期。流动路径的改变被限制在第一级叶片,以尽量减少引入新的风险和不确定性。
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Optimized SGT-A35 (GT61) for Improved Emissions and Enhanced Efficiency Across the Load Range
The RT61 is a three-stage industrial power turbine which couples with the SGT-A35 aeroderivative gas generator (formerly named Industrial RB211). It was designed for improved efficiency and modular construction for ease in maintainability. The aeroderivative SGT-A35 (GT61) product serves both oil & gas and power generation market with a fleet size of greater than 90 units. In recent years, there has been increased emphasis on clean energy, only complemented by the regulatory changes and market conditions. The power generation and oil & gas customers (upstream, midstream, and downstream) are continuously looking for opportunities to decrease their greenhouse gas emissions and reduce fuel consumption by improving the gas turbine cycle efficiency. The SGT-A35 (GT61) power turbine has > 93% isentropic efficiency and industry standard overhaul schedule of 100,000 hours. However the potential for further cycle efficiency improvements and reduction in emissions exist by optimizing the power turbine capacity to a specific load range. This served as the main motivation for this technical work. This paper discusses the engineering efforts taken in implementing the above stated improvement and further optimizing the product for reduced emissions. The improvements are discussed on the product level and on the TransCanada Pipelines fleet level. A new power turbine variant was developed on a demanding timeline driven by the customer project. A detailed development project was undertaken to establish the new operating point, aerodynamic design, and the new geometry. It was optimized to the customer project-specific load range. During the manufacturing phase, novel rapid prototyping methods were used to achieve desired lead times. Flow path change was limited to the first stage vane to minimize the introduction of new risks and uncertainties.
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