TURBOMACHINE ROTOR BLADE WITH AN AIRFOIL HAVING A VARIABLE ELLIPTICAL TRAILING EDGE

A rotor blade 100 of a turbomachine 10 includes an airfoil 114. The airfoil includes a root 118 and a tip 115 which define a span 128 of the airfoil therebetween. The airfoil also includes a leading edge 124 and a trailing edge 126 downstream of the leading edge along a flow direction. The leading e...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	KARAKASIS MARIOS, FREDMONSKI ADAM JOHN, BUJNICKI ROBERT PIOTR
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 STEAM ENGINES WEAPONS
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