COMPRESSOR AIRFOIL WITH TIP DIHEDRAL

An airfoil for a compressor is described. The airfoil has a root, an airfoil tip, a leading edge, a trailing edge, airfoil pressure and suction sides extending between the leading edge and the trailing edge. The airfoil has an inner span region and an outer span region and the trailing edge has a di...

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Hauptverfasser:	BREEZE-STRINGFELLOW, ANDREW, BEACHER, BRENT, FRANKLIN, CLARK, DAVID, SCOTT
Format:	Patent
Sprache:	eng ; fre
Schlagworte:	BLASTING ENGINE PLANTS IN GENERAL HEATING 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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creator	BREEZE-STRINGFELLOW, ANDREW BEACHER, BRENT, FRANKLIN CLARK, DAVID, SCOTT
description	An airfoil for a compressor is described. The airfoil has a root, an airfoil tip, a leading edge, a trailing edge, airfoil pressure and suction sides extending between the leading edge and the trailing edge. The airfoil has an inner span region and an outer span region and the trailing edge has a dihedral profile such that the trailing edge dihedral angle decreases in at least a portion of the inner span region and the outer span region. La présente invention a trait à une aube qui est destinée à un compresseur. L'aube est dotée d'une origine, d'une pointe d'aube, d'un bord avant, d'un bord arrière, de côtés de pression et d'aspiration d'aube qui s'étendent entre le bord avant et le bord arrière. L'aube est dotée d'une région d'envergure intérieure et d'une région d'envergure extérieure et le bord arrière est pourvu d'un profil dièdre de sorte que l'angle dièdre du bord arrière diminue sur au moins une partie de la région d'envergure intérieure et de la région d'envergure extérieure.
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L'aube est dotée d'une région d'envergure intérieure et d'une région d'envergure extérieure et le bord arrière est pourvu d'un profil dièdre de sorte que l'angle dièdre du bord arrière diminue sur au moins une partie de la région d'envergure intérieure et de la région d'envergure extérieure.</abstract><oa>free_for_read</oa></addata></record>
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language	eng ; fre
recordid	cdi_epo_espacenet_WO2012134835A1
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subjects	BLASTING ENGINE PLANTS IN GENERAL HEATING 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
title	COMPRESSOR AIRFOIL WITH TIP DIHEDRAL
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