BUCKLE JOINT FOR SPLIT FAIRING OF A GAS TURBINE ENGINE

A gas turbine engine strut fairing (10, 110) includes: inner and outer bands; a hollow, airfoil-shaped vane (12, 112) extending between the bands; wherein the fairing (10, 110) is split along a transverse plane passing through the bands and vane (12, 112), defining a nose piece (24, 124) and a tail...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	DREISCHARF, DEREK THOMAS, RYCZEK, SCOTT PATRICK
Format:	Patent
Sprache:	eng ; fre
Schlagworte:	BLASTING ENGINE PLANTS IN GENERAL HEATING 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 STEAM ENGINES WEAPONS
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!