If the gland assembly, shown in the illustration, is located at the forward end of the high pressure turbine, and the vessel is operating at minimum maneuvering speeds, which of the following statements is true? See illustration SE-0006.
• Location and purpose of a forward high-pressure turbine gland (prevents air leaking in or steam leaking out at the shaft penetration) • How pressure relationships change at minimum maneuvering speed (turbine internal pressure vs. atmospheric vs. sealing steam header) • Which side of the gland (spaces "E" and "F") is toward the turbine interior and which is toward the atmosphere/gland exhaust
• First decide the direction of leakage at the forward end of the HP turbine when running at very low power: is the greater pressure inside the turbine or outside? • Based on that leakage direction, would sealing steam need to be admitted closer to the turbine side, the atmospheric side, or both, in order to form the correct pressure ‘barrier’? • Look at the labyrinth group arrangement: how would admitting steam at E versus F change which sets of teeth see sealing steam and which side would still be at vacuum/atmosphere?
• Confirm which cavity (E or F) is bounded by teeth facing the turbine internal pressure and which is bounded by teeth facing the atmosphere/gland exhauster • Verify how a HP forward gland behaves at full power versus minimum maneuvering (when does it become self-sealing, and when is auxiliary sealing steam required?) • Ensure your chosen option matches a realistic flow path: steam should move from higher pressure to lower pressure, forming a gradient from turbine → sealing steam space(s) → atmosphere/vacuum.
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