AIR ACCELERATOR ON TIE ROD WITHIN TURBINE DISK BORE

Gas turbine engine high pressure rotor (12) first and second high pressure turbine stages (55, 56) include first and second stage disks (60, 62) having first and second stage disk bores (164, 166) and a single tie rod (170) therethrough. First and second bore annular flowpaths (184, 186) are radiall...

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Bibliographische Detailangaben
Hauptverfasser: PEPI, JASON FRANCIS, NORCOTT, KEVIN PATRICK, VON DER ESCH, ROBERT CLAYTON
Format: Patent
Sprache:eng ; fre
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