TURBINE ROTOR COMPRISING VENTILATION SPACER

The invention relates to a rotor (3) of a member (7) of a turbomachine (1), for example a rotor of a turbine (7), said rotor (3) comprising: a first element (30), a second element (20) defining with the first element a ventilation cavity (9), the rotor (3) being characterized in that it further comp...

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Bibliographische Detailangaben
Hauptverfasser:	OUDIN BENJAMIN CYRILLE JACQUES, CASALIGGI PASCAL, CAPOLUNGO THIERRY LAURENT, PASQUIET DIDIER DESIRE RENE
Format:	Patent
Sprache:	chi ; eng
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:	The invention relates to a rotor (3) of a member (7) of a turbomachine (1), for example a rotor of a turbine (7), said rotor (3) comprising: a first element (30), a second element (20) defining with the first element a ventilation cavity (9), the rotor (3) being characterized in that it further comprises a spacer (40) that is introduced and secured between the first element (30) and the second element (20) and that comprises a row of through-passages (42) that are configured to permit injection of cooling fluid (F) into the ventilation cavity (9). 本发明涉及涡轮机(1)的构件(7)的转子(3)，例如涡轮(7)的转子，所述转子(3)包括：-第元件(30)，-第二元件(20)，所述第二元件与所述第元件起限定出通风腔(9)，所述转子(3)的特征在于，所述转子进步包括间隔件(40)，所述间隔件被引到并固定在第元件(30)和第二元件(20)之间，并且包括排贯通通道(42)，所述贯通通道被构造成允许冷却流体(F)注入到所述通风腔(9)中。