BELLCRANK FOR A VARIABLE ADJUSTMENT DEVICE FOR A TURBOMACHINE

A bellcrank for a variable adjustment device for an aircraft turbomachine, is articulated respectively to a control housing, to a synchronization bar, to a piston stem of an actuator and to a turnbuckle. The bellcrank includes a part for articulation to the control housing which includes, on the one...

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
Hauptverfasser:	ROBERT, Yann, Thierry, BARBIER-NEVEU, Clélia, Antoinette, BOSTON, Erick, Jacques
Format:	Patent
Sprache:	eng ; fre ; ger
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 NON-POSITIVE DISPLACEMENT PUMPS POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC FLUIDS STEAM ENGINES WEAPONS
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!

Beschreibung
Zusammenfassung:	A bellcrank for a variable adjustment device for an aircraft turbomachine, is articulated respectively to a control housing, to a synchronization bar, to a piston stem of an actuator and to a turnbuckle. The bellcrank includes a part for articulation to the control housing which includes, on the one hand, a tab and, on the other hand, a tubular portion spaced apart from the tab, the tab and the tubular portion including orifices that are aligned and are configured to receive a common axis of articulation of the control housing.