Inter-vane platform with lateral deflection for a vane support of a turbine engine

An inter-vane platform ( 3 ), for a vane support disk ( 1 ) of a turbine engine fan, comprises a central part ( 5 ) of one piece with the support disk ( 1 ) between two adjacent vanes ( 2 ), and two lateral parts ( 8,9 ), forming extensions to two lateral edges ( 6,7 ) of the central part ( 5 ), and...

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Bibliographische Detailangaben
Hauptverfasser:	LEJARS CLAUDE, QUERIAULT MICHELE
Format:	Patent
Sprache:	eng
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ENGINE PLANTS IN GENERAL GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES NON-POSITIVE DISPLACEMENT PUMPS POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC FLUIDS STEAM ENGINES WEAPONS
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Beschreibung
Zusammenfassung:	An inter-vane platform ( 3 ), for a vane support disk ( 1 ) of a turbine engine fan, comprises a central part ( 5 ) of one piece with the support disk ( 1 ) between two adjacent vanes ( 2 ), and two lateral parts ( 8,9 ), forming extensions to two lateral edges ( 6,7 ) of the central part ( 5 ), and each designed in such a way as to deflect under the impact of the vane ( 2 ) opposite which it is located.