GAS TURBINE WITH AXIALLY DISPLACEABLE ROTOR

The device has an axially movable rotor (3) and an annular channel (24) in a housing with inner and outer guide surfaces (21,22) forming a flow channel (24) narrowing in the axial direction, at least one fixed rim (15) in the annular channel and at least one rim (17) of profiles on the rotor, whereb...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser:	STOECKER, BERND, REICHERT, ARND
Format:	Patent
Sprache:	eng ; fre ; ger
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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Beschreibung
Zusammenfassung:	The device has an axially movable rotor (3) and an annular channel (24) in a housing with inner and outer guide surfaces (21,22) forming a flow channel (24) narrowing in the axial direction, at least one fixed rim (15) in the annular channel and at least one rim (17) of profiles on the rotor, whereby the end of each rotor blade (14) and/or guide vane (16) is opposite an axial section of one of the two bounding surfaces to form a radial gap (23). The size of each radial gap between the end of each blade and the opposing axial section of the bounding surface is constant at least over the displacement distance of the rotor and the radial gap is parallel to the rotation axis of the rotor.