Gas turbine components for cooling purposes including other unique and complex three-dimensional designs could be made explicitly possible through additive manufacturing using SLM technology in contrary to the conventional machining processes. Nevertheless, the surface roughness and subsequently the friction factor governs thepressure drop in these components implicitly, thus, influencing the secondary air flow system of a gas turbine. Research studies to understand and predict flow behaviours through especially AM parts are still in a budding stage, and thus, in this scope of thesis, the same has been attempted through experimentation to quantifypressure losses in additively manufactured rectangular orices. With the purpose of a brief analogy, a set of aluminium circular samples were also tested which were manufactured by the conventional process of machining. A total of 9 rectangular MA247 samples of different lengths and hydraulic diameters were tested as continuation to the ongoing research at Siemens Industrial Turbomachinery AB and further on to that, 5 Aluminium Alloy- AW-6082 T6 material samples of circular geometry with varying lengths were tested. The on-going research focuses on the additively manufactured geometries for both rectangular and circular, and hence, the data for circular orifices were used to draw a comparison with its Aluminium counterpart. Pressure losses here were described using the coefficient of discharge and the investigations on roughness were by calculating Darcy frictional factor and Colebrooks equation. Classical theories such as the boundary layer theory, Hagen's power law, Ward-Smith's theory for vena contracta and other works by previous researchers were used to validate the results. The coefficient of discharge could be deployed to restrict and measure the mass flow in the secondary air systems, whereas the results from the calculated frictional factors could be held to simulate the flow distribution in cooling geometries. / <p>E-presentation via Zoom due to the pandemic.</p> / Part of the on-going research on pressure loss study for Gas Turbine cooling purposes by Siemens Energy

Bei eigengekühlten Elektromaschinen in Außenläuferbauweise resultiert aus der schwierigeren Abführung der Statorverluste üblicherweise eine Reduktion der elektromagnetischen Ausnutzung. Im Beitrag wird am Beispiel eines permanentmagnetisch erregten Synchrongenerators für eine Kleinwindenergieanlage das Verfahren der intensivierten Statorrohrinnenkühlung unter Nutzung der Windströmung durch einen im Statorrohr angeordneten Kühlkörper diskutiert. Neben der elektromagnetischen und strömungsmechanischen bzw. thermischen Modellierung wird die experimentelle Trennung der Einzelverluste vorgestellt. Es wird gezeigt, dass die Ausnutzung der Maschine durch die intensivierten Statorrohrinnenkühlung um ca. 40 % gesteigert werden kann. / For self-ventilated electrical machines in outer rotor design, the difficult dissipation of stator losses usually results in a reduction of the electromagnetic utilization. Based on an example of a permanent magnet synchronous generator for a small wind turbine, the method of intensified inner stator tube cooling using the wind flow through a heat sink arranged in the stator tube is discussed in the article. In addition to the electromagnetic and fluid mechanical as well as thermal modeling, the experimental separation of the losses is presented. It is shown that the utilization of the machine can be increased by approx. 40 % by means of the intensified internal cooling of the stator tube.

This study focused on experimentally determining the cooling performance of a fully cooled, scaled-up model of a C3X turbine vane. The primary objective was to determine the differences in overall effectiveness in the presence and absence of a hot mainstream flowing over the vane. Overall effectiveness was measured using a thermally scaled matched Biot number vane with an impingement plate providing the internal cooling. This is the first study focused on investigating the effect of removing the mainstream flow and comparing the contour and laterally-averaged effectiveness data in support of the development of an assembly line thermal testing method. It was found that the proposed method of factory floor testing of turbine component cooling performance did not provide comparable information to traditional overall effectiveness test methods. A second experiment was performed in which the effect of altering the angle of attack of a flow into a passive turbulence generator was investigated. Measurements in the approach flow were taken using a single wire hot-wire anemometer. This study was the first to investigate the effects such a setup would have on fluctuating flow quantitates such as turbulence intensity and integral length scale rather than simply the mean quantities. It was found that both the downstream turbulence intensity and the turbulence integral length scale increase monotonically with approach flow incidence angle at a specified distance downstream of the turbulence generator. / text

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