Siemens Aktiengesellschaft

Reinhard Mönig

Peter Tiemann

Christian Cornelius

Iris Oltmanns, Legal Representative

Ulf Koeller

Ulf Köller

A gas turbine engine having an axial flow compressor, an annular combustion chamber, a turbine, and a diffuser. The diffuser includes a flow-dividing element formed by an inner deflecting flank and an outer deflecting flank that divides a compressed gas flow into two partial flows at a branching point. The two deflecting flanks define: an angle of less than 90&#xb0; along at least a portion of the deflecting flanks, and an angle between 15&#xb0; and 90&#xb0; between the deflecting flank angle bisector and the turbine longitudinal axis. The deflector also includes a main deflecting region arranged upstream of the branching point and directed at an acute angle from the turbine longitudinal axis toward an inner combustion chamber shell.

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Königswinter, Germany

Reinhard Mönig