ROTOR, NOTAMMENT POUR COMPRESSEURS OU TURBINES DE GROUPES MOTOPROPULSEURS A TURBINE A GAZ

A compressor or turbine rotor, particularly for gas turbine propulsion units in which individual blades 1. 2 of a compressor or turbine stage are disposed in slotted-wing fashion in respect of adjacent outlet and inlet edges 3, 4. The rotor comprises a plurality of portions A, B, each of which compr...

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
1. Verfasser:	WOLFGANG WEILER
Format:	Patent
Sprache:	fre
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
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!

Beschreibung
Zusammenfassung:	A compressor or turbine rotor, particularly for gas turbine propulsion units in which individual blades 1. 2 of a compressor or turbine stage are disposed in slotted-wing fashion in respect of adjacent outlet and inlet edges 3, 4. The rotor comprises a plurality of portions A, B, each of which comprises a row of profile members or blades 1, 2 the portions A, B having on adjacent end faces 3, 4 thereof interengaging complementary profiles 7, 8 thereon to prevent relative rotation. Coaxial centering action when the portions A, B are pushed together may be provided by a peripheral stepped portion (9), Fig 1. The rotor portions A, B may be fastened together by welding or by bolts (16), Fig 1.