CAPOTAGE POUR BORD D'ATTAQUE D'AUBE DE SOUFFLANTE DE TURBOREACTEUR

A fairing formed from a dihedron of which the faces, disposed in the extension of the intrados and extrados surfaces follow the aerodynamic profile of the blade. Such rejoin the blade at a small radius portion constituting a leading edge. The fairing imparts a characteristic enabling the optimum eff...

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
1. Verfasser:	JEAN MARIE LOUIS GELY, MARIUS JEAN MARIE GOUTINES ET GEORGES MEAUZE
Format:	Patent
Sprache:	fre
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
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!

Beschreibung
Zusammenfassung:	A fairing formed from a dihedron of which the faces, disposed in the extension of the intrados and extrados surfaces follow the aerodynamic profile of the blade. Such rejoin the blade at a small radius portion constituting a leading edge. The fairing imparts a characteristic enabling the optimum efficiency of the fan to be approached. The useful height of the dihedron is at least 5% of the height of the blade.