Rotor

Rotor for a gas-turbine engine, the rotor comprising a first (1 a) and a second (1 b) rotor disc, the rotor discs (1 a, 1 b) being suitable to be joined directly, each rotor disc (1a, 1 b) is symmetric with respect to an axis of rotation common to the two rotor discs (1a, 1 b), characterized in that...

Ausführliche Beschreibung

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Bibliographische Detailangaben
1. Verfasser:	Safari Zadeh, Hossein
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:	Rotor for a gas-turbine engine, the rotor comprising a first (1 a) and a second (1 b) rotor disc, the rotor discs (1 a, 1 b) being suitable to be joined directly, each rotor disc (1a, 1 b) is symmetric with respect to an axis of rotation common to the two rotor discs (1a, 1 b), characterized in that the first rotor disc (1 a) provides an interrupted screw on one side (4), the second rotor disc (1 b) provides an interrupted screw on another side (5), said interrupted screw of the second rotor disc (1 b) reciprocates the interrupted screw of the first rotor disc (1 a).