Exit guide vanes

The invention relates to a stator vane (1) for a turbine engine, characterised by being made up of a set of vane portions (3a, 3b, 3c) arranged relative to one another in order to define passages (5a, 5b) for the air flow to circulate between the vane portions, and by comprising a means (2) for circ...

Ausführliche Beschreibung

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Bibliographische Detailangaben
1. Verfasser:	NILS BORDONI
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 JET-PROPULSION PLANTS 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 stator vane (1) for a turbine engine, characterised by being made up of a set of vane portions (3a, 3b, 3c) arranged relative to one another in order to define passages (5a, 5b) for the air flow to circulate between the vane portions, and by comprising a means (2) for circulating a fluid to be cooled by said air flow.