BLADE/DISK DOVETAIL BACKCUT FOR BLADE/DISK STRESS REDUCTION (6FA AND 6FA+e, STAGE 1)

Blade load path on a gas turbine disk can be diverted to provide a significant disk fatigue life benefit. A plurality of gas turbine blades are attachable to a gas turbine disk, where each of the gas turbine blades includes a blade dovetail engageable in a correspondingly-shaped dovetail slot in the...

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Bibliographische Detailangaben

Hauptverfasser:	GOPALAKRISHNAN, BABU, SANTHANA, ZEMITIS, WILLIAM, SCOTT, CHAN, SZE BUN, BRIAN
Format:	Patent
Sprache:	eng ; fre
Schlagworte:	MARINE PROPULSION OR STEERING MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVINGMATERIAL PERFORMING OPERATIONS PUNCHING METAL RELATED EQUIPMENT SHIPS OR OTHER WATERBORNE VESSELS TRANSPORTING WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS ORPROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL
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