AERONAUTICAL PROPULSION SYSTEM WITH IMPROVED PROPULSION EFFICIENCY

An aeronautical propulsion system (1) comprises a ducted fan rotor (9) having an aerodynamic load parameter kaero greater than or equal to 0.10 and less than or equal to 0.18 and a mechanical load parameter kmeca greater than or equal to 20.0 × 106 rpm2.min-1 and less than or equal to 32.0 × 106 rpm...

Ausführliche Beschreibung

Bibliographische Detailangaben

1. Verfasser:	ESCURE, Didier
Format:	Patent
Sprache:	eng ; fre
Schlagworte:	BLASTING COMBUSTION ENGINES ENGINE PLANTS IN GENERAL HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS JET-PROPULSION PLANTS LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES WEAPONS
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!