HIGH PRESSURE TURBINE COMPONENT INTERFERENCE FIT UP

13DV-11233 HIGH PRESSURE TURBINE COMPONENT INTERFERENCE FIT UP of the Invention An interference fit up for an HPT hanger is accomplished by machining and casting features into the hanger which create a spring effect when the effect may be accomplished in a variety of ways, including offset radial cu...

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Bibliographische Detailangaben
Hauptverfasser:	PLEMMONS, LARRY W, PROCTOR, ROBERT, ALBERS, ROBERT J
Format:	Patent
Sprache:	eng ; fre
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 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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Beschreibung
Zusammenfassung:	13DV-11233 HIGH PRESSURE TURBINE COMPONENT INTERFERENCE FIT UP of the Invention An interference fit up for an HPT hanger is accomplished by machining and casting features into the hanger which create a spring effect when the effect may be accomplished in a variety of ways, including offset radial cut features on the hanger relative to the support, or offset projection features on the hanger which are concentric with the support. The spring effect is than accomplished by a flex or deflection of the ends of the hanger to conform to the width of the support, and clearance indentations created during the installation.