Gas turbine with exhaust gas casing and also method for producing such gas turbine

The turbine (10) has an annular exhaust gas casing (16) arranged at a turbine outlet at a distance from a supporting foundation (22) and comprising an outer shell (20a). Supporting devices (26-28) are arranged with a predetermined supporting direction for absorbing deformations of the casing, where...

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Bibliographische Detailangaben
Hauptverfasser:	ORESTES JESUS MAURELL, KEVIN CARPENTER, JOSE RUIZ, KEVIN BRADY POWELL, HAROLD SIEGERT
Format:	Patent
Sprache:	eng
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS
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Beschreibung
Zusammenfassung:	The turbine (10) has an annular exhaust gas casing (16) arranged at a turbine outlet at a distance from a supporting foundation (22) and comprising an outer shell (20a). Supporting devices (26-28) are arranged with a predetermined supporting direction for absorbing deformations of the casing, where the supporting devices are arranged between the foundation and the outer shell. Each supporting device has an end fastened on the outer shell and another end supported on the foundation. Each supporting device exhibits a pre-loaded spring support that acts in the supporting direction. An independent claim is also included for a method for manufacturing a gas turbine.