INLET GUIDE WHEEL FOR A TURBO ENGINE

An embodiment of the invention relates to an inlet guide wheel for a turbo engine with a plurality of guide vanes that radially extend inside a flow channel of the turbo engine, and that respectively comprise: a first, radially outer aerofoil that comprises a radially inner end, and a second, radial...

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Bibliographische Detailangaben
1. Verfasser:	HEINICHEN, Frank
Format:	Patent
Sprache:	eng
Schlagworte:	BLASTING ENGINE PLANTS IN GENERAL HEATING 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:	An embodiment of the invention relates to an inlet guide wheel for a turbo engine with a plurality of guide vanes that radially extend inside a flow channel of the turbo engine, and that respectively comprise: a first, radially outer aerofoil that comprises a radially inner end, and a second, radially inner aerofoil that comprises a radially outer end, wherein the first aerofoil and/or the second aerofoil is embodied in a rotatable manner. It is provided that the first aerofoil and the second aerofoil are separated by a tip shroud which at least partially covers both the radially inner end of the first aerofoil and the radially outer end of the second aerofoil.