Essays about: "Siemens Industrial Turbomachinery AB"
Showing result 21 - 25 of 36 essays containing the words Siemens Industrial Turbomachinery AB.
-
21. Flexible Ignition System for a Gas Turbine
University essay from KTH/Kraft- och värmeteknologiAbstract : Siemens Industrial Turbomachinery AB produce five gas turbines models. The SGT-700 can currently only start on gases which contain low amounts of inert gases. It is therefore of interest to widen the fuel range which the SGT-700, as well as other gas turbines, can start on. READ MORE
-
22. Weld Analysis in Combustion Chambers Subjected to Thermo-Mechanical Fatigue Load Conditions
University essay from HållfasthetsläraAbstract : At cyclic operation of gas turbines, components are subjected to thermo-mechanical fatigue (TMF) due to the high temperature gradients that arises. In this thesis life assessment of welds in combustion chambers are at focus. READ MORE
-
23. Preliminary study of a frame for a two module turbine system
University essay from MaskinkonstruktionAbstract : The development of steam turbines is continuously moving forward and the aim is oftento develop configurations with higher power output. Siemens Industrial Turbomachinery AB is currently in the beginning of a development project which replaces a single turbine with two interconnected turbines with higher pressure and temperature of the steam than before. READ MORE
-
24. Calculation of power losses in turbine-driven generator
University essay fromAbstract : Siemens Industrial Turbomachinery AB har köpt en generator från ABB och vill kunna driva denna på olika varvtal, spänning och belastning. Vår uppgift har blivit att med given förlustdata efter utökat generatorprov vid olika varvtal och belastningar, ta fram en metod för att bestämma förluster i godtyckliga punkter inom ett känt intervall. READ MORE
-
25. Alternative Cooling and Mounting Concepts for Transition Duct in Industrial Gas Turbines at Siemens Industrial Turbomachinery AB
University essay from MaskinkonstruktionAbstract : Gas turbine development is constantly moving forward and for higher efficiency hotter turbine inlet temperature is required. Because of that, one of the largest design problems is to find efficient ways to cool the hot parts in the gas turbine. READ MORE