AERONAUTICAL THRUSTER

An aeronautical thruster having a longitudinal axis and having a hub, an upstream annular row and a downstream annular row which are spaced apart from each another along the longitudinal axis, the upstream annular row being rotatable around the longitudinal axis, and the downstream annular row havin...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser:	JODET, Norman Bruno André, LEBEAULT, Eva Julie, GEA AGUILERA,, Fernando, DUBOIS, Adrien Clément Marcel, LAFITTE, Anthony Bernard Germain, REGNARD, Josselin David Florian, BINDER, Anthony
Format:	Patent
Sprache:	eng
Schlagworte:	AEROPLANES AIRCRAFT AVIATION BLASTING COSMONAUTICS ENGINE PLANTS IN GENERAL HEATING HELICOPTERS LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES PERFORMING OPERATIONS STEAM ENGINES TRANSPORTING WEAPONS
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Beschreibung
Zusammenfassung:	An aeronautical thruster having a longitudinal axis and having a hub, an upstream annular row and a downstream annular row which are spaced apart from each another along the longitudinal axis, the upstream annular row being rotatable around the longitudinal axis, and the downstream annular row having a first blade and a second blade each extending in a radial direction to define a radial dimension between the hub and a radially outer end of the corresponding blade. When observed angularly around the longitudinal axis, the second blade can be positioned closer to an angular position at 3 o'clock or an angular position at 9 o'clock than the first blade, and the radial dimension of the first blade can be greater than the radial dimension of the second blade.