SEGMENTED RIM SEAL SPACER FOR A GAS TURBINE ENGINE

A seal segment (102) for a gas turbine engine (20) includes a first axial span (134) that extends between a first radial span (130) and a second radial span (132). A second axial span (136) extends between the first radial span (130) and the second radial span (132), the first radial span (130), the...

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Bibliographische Detailangaben

Hauptverfasser:	MERRY, Brian D, SUCIU, Gabriel L, HILL, James D, PARTYKA, Julian, PACK, David R, DOLANSKY, Gregory M
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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