MECHANICAL FLANGE JOINT FOR A GAS TURBINE ENGINE

A joint for a gas turbine engine to reduce thermal gradients across the joints component parts includes, an annular component such as an inner nozzle support (66) having an annular, radially-extending flange 68; an annular second component such as a diffuser having an annular, radially-extending sec...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	SASIKUMAR MUTHUSAMY, PAUL ALEXANDER INTEMANN, RYAN MICHAEL JASKO, JARMO TAPANI MONTTINEN, KENNETH EDWARD SEITZER
Format:	Patent
Sprache:	eng
Schlagworte:	BLASTING DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS ORMACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS,CLIPS, WEDGES, JOINTS OR JOINTING ENGINE PLANTS IN GENERAL ENGINEERING ELEMENTS AND UNITS GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS HEATING LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES THERMAL INSULATION IN GENERAL WEAPONS
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