AXIAL RETENTION ASSEMBLY FOR COMBUSTOR COMPONENTS OF A GAS TURBINE ENGINE

The present subject matter is directed to an axial retention assembly for combustor components of a gas turbine engine. The axial retention assembly may include a combustor having a liner (38) defining a liner aperture (114) extending therethrough. Additionally, the combustor may further include a s...

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Bibliographische Detailangaben
Hauptverfasser:	MOGLE II, Thomas Alan, HANSON, Stuart Craig
Format:	Patent
Sprache:	eng ; fre
Schlagworte:	BLASTING COMBUSTION APPARATUS COMBUSTION PROCESSES ENGINE PLANTS IN GENERAL GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS HAND TOOLS HEATING LIGHTING MACHINES OR ENGINES IN GENERAL MANIPULATORS MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES PERFORMING OPERATIONS PORTABLE POWER-DRIVEN TOOLS STEAM ENGINES TOOLS OR BENCH DEVICES NOT OTHERWISE PROVIDED FOR, FORFASTENING, CONNECTING, DISENGAGING OR HOLDING TRANSPORTING WEAPONS
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