Transition between a combustion chamber and a turbine

The turbine has a combustion chamber surrounded by an external wall, and a turbine unit that downstreams the chamber visible in the flow direction of working medium. The turbine unit has wall units (32) limiting the flow path of the medium. The wall units form a balancing gap in a transition area, w...

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Bibliographische Detailangaben
Hauptverfasser:	HERZ, MARGARETE, LERNER, CHRISTIAN, HEILOS, ANDREAS, LENZE, MARTIN, WOLFF, MARIANO CANO
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	BLASTING COMBUSTION APPARATUS COMBUSTION PROCESSES CYLINDERS ENGINE PLANTS IN GENERAL ENGINEERING ELEMENTS AND UNITS GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS HEATING LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES PISTONS SEALINGS STEAM ENGINES THERMAL INSULATION IN GENERAL WEAPONS
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Beschreibung
Zusammenfassung:	The turbine has a combustion chamber surrounded by an external wall, and a turbine unit that downstreams the chamber visible in the flow direction of working medium. The turbine unit has wall units (32) limiting the flow path of the medium. The wall units form a balancing gap in a transition area, where the gap is closed by a number of separate closing components. The closing components are fixed at the wall unit of the turbine unit.