Gas Turbine Transition Duct Gap Assessment for Unsymmetrical Thermal Boundary Conditions

Manoharan Sambandam, S. Colantoni
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Abstract

The transition duct (TD) in a gas turbine (GT) twin shaft variant provides an aerodynamic coupling between its high-pressure gas generator module and low-pressure power module. Since the TD defines the flow passage, it interfaces with the high-pressure rotor and shroud at the forward end and the low-pressure rotor and stator at the aft end. Normally, the GT twin shaft variant is equipped with part-load capability. To fulfill this need and to comply with the emission norms, only desired number of burners, adjacent to each other, are used to burn fuel. Using some of the burners during the GT operation is referred to as staging. The GT operation under staging conditions result in non-uniform temperature distribution in the angular locations at any axial position and thus non-uniform thermal growth in the radial and axial directions. This non-uniform thermal growth in radial and axial direction leads to the interface definition very challenging. During the staging operation, the rotor parts experiences uniform radial and axial growth at all the angular locations. Whereas the interfacing stator parts experience temperature distribution like that of the TD and results in non-uniform thermal growth in the radial and axial directions. Appropriate interface definition is vital for efficient operation of the GT. Any interference condition of the TD with rotating parts result in rubbing and with stationary parts result in thermal binding, impacting the GT normal operation. Any generous gap adversely impacts the GT performance due to consumption of more cooling medium. Thus, an assembly gap which results in no interference and consumption of less cooling medium throughout the staging operation is considered as optimum assembly gap. Thorough gapping assessment is performed considering all the transient time points to ensure that the gap values are set optimally. This paper is intended to describe the steps followed in assessing the anticipated interference and gap situations at various interfaces.
非对称热边界条件下燃气轮机过渡管道间隙评估
燃气轮机(GT)双轴变型中的过渡管道(TD)在高压燃气发生器模块和低压动力模块之间提供了气动耦合。由于TD定义了流动通道,因此它与前端的高压转子和叶冠以及尾部的低压转子和定子相连接。通常,GT双轴变型配备了部分负载能力。为了满足这一需求并符合排放标准,只使用所需数量的彼此相邻的燃烧器来燃烧燃料。在GT操作期间使用一些燃烧器被称为分段。分段工况下的GT运行导致轴向任意位置的角度位置温度分布不均匀,从而导致径向和轴向的热增长不均匀。这种径向和轴向的非均匀热生长导致界面定义非常具有挑战性。在分级操作期间,转子部件在所有角位置经历均匀的径向和轴向增长。而接合的定子部件则经历了与TD相似的温度分布,导致径向和轴向的热增长不均匀。适当的界面定义对于GT的有效运行至关重要。TD与旋转部件的任何干扰都会导致摩擦,与静止部件的任何干扰都会导致热结合,从而影响GT的正常运行。由于消耗更多的冷却介质,任何较大的间隙都会对GT性能产生不利影响。因此,在整个分级操作过程中不产生干扰和消耗较少冷却介质的装配间隙被认为是最佳装配间隙。考虑所有暂态时间点,进行全面的间隙评估,以确保间隙值的最优设置。本文旨在描述在评估各种界面的预期干扰和间隙情况时所遵循的步骤。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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