Ansaldo Energia Switzerland Ag

Stephan Strueken

Adnan Eroglu

Stephen Wilder Jorgensen

Thomas Zierer

Frank Graf

Joshua R McNally

Cyrille Bricaud

Carl Berger

Marcos Escudero Olano

Afzal Pasha Mohammed

Cyrille Jerome Bricaud

Stephen W Jorgensen

A sealing arrangement at an interface between a combustor and a turbine of a gas turbine. The turbine can include deflecting vanes at its inlet, which deflecting vanes are each mounted within the turbine so as to define an inner or outer diameter platform and are in sealing engagement via an inner or outer diameter vane tooth with a seal arranged at the corresponding inner or outer diameter part of the outlet of the combustor. The seal is movable and is pressed on the inner or outer diameter vane tooth by a differential pressure such that the pressure of the mainstream hot gas flow is a lower pressure.

Sealing device arrangement at the interface between a combustor and a turbine of a gas turbine and gas turbine with such a sealing arrangement

A heat exchanger is disclosed which includes a pressure vessel with an inlet for air, an outlet for air, and a bundle of pipes housed within the pressure vessel for a thermo-vector fluid. A gas/solid separator is provided within the pressure vessel for separating particles drawn by the air.

Heat exchanger for a gas turbine engine

Growing community of inventors

Zurich, Switzerland

Stephan Strueken