Counterstagger compressor airfoil

A compressor airfoil (20) includes opposite pressure and suction sides (26,28) joined together at leading and trailing edges (30,32) and extending in span between a root (34) and tip (36). The airfoil (20) includes stagger increasing above the root (34) and decreasing above a midspan pitch section (...

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Bibliographische Detailangaben
Hauptverfasser:	WOOD PETER JOHN, DOLORESCO BRYAN KEITH
Format:	Patent
Sprache:	chi ; 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:	A compressor airfoil (20) includes opposite pressure and suction sides (26,28) joined together at leading and trailing edges (30,32) and extending in span between a root (34) and tip (36). The airfoil (20) includes stagger increasing above the root (34) and decreasing above a midspan pitch section (40) thereof.