RETAINING RING ASSEMBLY FOR A GAS TURBINE ENGINE

A retaining ring assembly (182) for a gas turbine engine (20) may include a first engine component (140) and a second engine component (160). A retaining ring (180) may be disposed between the first engine component (140) and the second engine component (160). The retaining ring (180) may be circumf...

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Bibliographische Detailangaben
1. Verfasser:	CAPRARIO, Joseph T
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	BLASTING ENGINE PLANTS IN GENERAL HEATING 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:	A retaining ring assembly (182) for a gas turbine engine (20) may include a first engine component (140) and a second engine component (160). A retaining ring (180) may be disposed between the first engine component (140) and the second engine component (160). The retaining ring (180) may be circumferentially discontinuous and may include a first terminal portion (210) having at least one of a tapered or a contoured geometry. A thickness of the retaining ring (180) at the first terminal portion (210) may be less than a thickness of the retaining ring (180) away from the first terminal portion (210).