Gas turbine combustor barrier structures for spring clips

A barrier structure ( 302 ) blocks exit of spring clip fragments ( 317 ) that may break off from a spring clip assembly disposed between a gas turbine engine combustor ( 300 ) and a transition piece component ( 360 ). The barrier structure ( 302 ) may additionally comprise an aspect ( 326 ) effectiv...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	PARKER DAVID MARCHANT, WETZL KRISTIAN I
Format:	Patent
Sprache:	eng
Schlagworte:	BLASTING COMBUSTION APPARATUS COMBUSTION PROCESSES ENGINE PLANTS IN GENERAL GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS HEATING INDEXING SCHEME FOR ASPECTS RELATING TONON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES ORJET-PROPULSION PLANTS INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUSSUBCLASSES OF CLASSES F01-F04 LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES WEAPONS
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