VARIABLE STATOR VANE ASSEMBLY

PROBLEM TO BE SOLVED: To provide a modified variable stator vane assembly and a modified bushing thereof. SOLUTION: A variable stator vane assembly 10. The assembly includes a rotatable trunnion 12 and a first metal bushing 14. The trunnion is capable of being located in a through hole extending bet...

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
Hauptverfasser:	BRUCE ROBERT W, BOWEN WAYNE RAY, CORNELL JAY L, GUTKNECHT JAMES EDWARD, SLAVIK DONALD CHARLES, DINGWELL WILLIAM TERENCE
Format:	Patent
Sprache:	eng
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BEARINGS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ELEMENTS OR CRANKSHAFT MECHANISMS ENGINE PLANTS IN GENERAL ENGINEERING ELEMENTS AND UNITS FLEXIBLE SHAFTS GAS-TURBINE PLANTS GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS INDEXING SCHEME FOR ASPECTS RELATING TONON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES ORJET-PROPULSION PLANTS INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUSSUBCLASSES OF CLASSES F01-F04 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 ROTARY BODIES OTHER THAN GEARING ELEMENTS SHAFTS STEAM ENGINES THERMAL INSULATION IN GENERAL WEAPONS
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!

Beschreibung
Zusammenfassung:	PROBLEM TO BE SOLVED: To provide a modified variable stator vane assembly and a modified bushing thereof. SOLUTION: A variable stator vane assembly 10. The assembly includes a rotatable trunnion 12 and a first metal bushing 14. The trunnion is capable of being located in a through hole extending between outer and inner surfaces 18 and 20 of a compressor casing 22 of a gas turbine engine 24. The first metal bushing is capable of being located in the through hole proximate the outer surface to surround a first portion 26 of the trunnion when the trunnion is located in the through hole. The first metal bushing and the first portion have wear-resistant coatings which are in mutual contact, apart from any intervening lubricant, when the trunnion and the first metal bushing are located in the through hole and the trunnion is rotating with respect to the first metal bushing. COPYRIGHT: (C)2007,JPO&INPIT