AIR ACCELERATOR ON TIE ROD WITHIN TURBINE DISK BORE

A gas turbine engine high pressure rotor with first and second high pressure turbine stages include first and second stage disks having first and second stage disk bores and a single tie rod therethrough. First and second bore annular flowpaths are radially located between first and second stage dis...

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Bibliographische Detailangaben

Hauptverfasser:	VON DER ESCH, ROBERT, CLAYTON, PEPI, JASON, FRANCIS, NORCOTT, KEVIN, PATRICK
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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