SPRING LOADED AND SEALED CERAMIC MATRIX COMPOSITE COMBUSTOR LINER

A combustor liner assembly of a gas turbine engine comprises a dome (42) having a central axis aligned with an engine axis, the dome arranged at an inlet end (32) of a combustor (16), a first spring (70) disposed at a radially outward position of the dome, an outer liner retainer engaging a radially...

Ausführliche Beschreibung

Bibliographische Detailangaben

1. Verfasser:	DERY, BRYAN ROBERT
Format:	Patent
Sprache:	eng ; fre
Schlagworte:	BLASTING COMBUSTION APPARATUS COMBUSTION PROCESSES GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS HEATING LIGHTING MECHANICAL ENGINEERING WEAPONS
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