METHOD AND DEVICE FOR ASSEMBLING GAS TURBINE ENGINE

PROBLEM TO BE SOLVED: To assemble a gas turbine engine (10). SOLUTION: A method comprises a step for forming at least one substantially elliptically-shaped opening (80) within a flange (72) extending from a fan disk (40), a step for at least partially inserting a fastener (120) including a first bod...

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Bibliographische Detailangaben
Hauptverfasser:	TAKEHARA JOANN MARI, DIX BRIAN EDWARD, GARRISON MICHAEL RAY
Format:	Patent
Sprache:	eng
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS 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 GAS-TURBINE PLANTS GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS JET-PROPULSION 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 THERMAL INSULATION IN GENERAL WEAPONS
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Beschreibung
Zusammenfassung:	PROBLEM TO BE SOLVED: To assemble a gas turbine engine (10). SOLUTION: A method comprises a step for forming at least one substantially elliptically-shaped opening (80) within a flange (72) extending from a fan disk (40), a step for at least partially inserting a fastener (120) including a first body portion (122), a second body portion (124), and an anti-rotation stop (126) extending therebetween through at least one flange opening, and a step for coupling the fastener to the flange such that the fastener stop is positioned within at least one flange opening. COPYRIGHT: (C)2005,JPO&NCIPI