Aspirating system for the compressor of a gas turbine

摘要

Aspirating system for the compressor of a gas turbine disposed next to a power-producing plant on the same shaft. The system has two separated suction canals extending laterally next to the powder producing plant. A transition part conveys the air from the suction canals to an axial intake opening in the compressor. The transition part has an inner shell of a truncated cone and outer shell of the truncated cone and two vertical baffles inclined toward each other, disposed between the inner shell and outer cone shell with the baffles touching each other in front of the intake opening of the compressor and terminating there. A transfer canal part adapts the cross section of each such canal facing the transition part to the entrance cross section of the transition part.