TURBINE ASSEMBLY AND METHOD FOR SUPPORTING TURBINE COMPONENT

PROBLEM TO BE SOLVED: To provide a turbine assembly and a method for supporting turbine components.SOLUTION: The turbine assembly includes a first static structure and a second static structure outward in the radial direction of the first static structure. The assembly also includes a support member...

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Bibliographische Detailangaben
1. Verfasser:	KLINGLER BRETT DARRICK
Format:	Patent
Sprache:	eng
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ENGINE PLANTS IN GENERAL GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES WEAPONS
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Beschreibung
Zusammenfassung:	PROBLEM TO BE SOLVED: To provide a turbine assembly and a method for supporting turbine components.SOLUTION: The turbine assembly includes a first static structure and a second static structure outward in the radial direction of the first static structure. The assembly also includes a support member placed in the recess part of the second static structure, wherein the support member includes first and second curved surfaces which come into contact with the first and second static structures respectively, and the support member includes a biasing structure which retains the support member in the recessed part.