Turbomachine vane provided with a structure reducing the risk of cracks

A vane 54, suitable for a turbomachine, comprising an aerodynamic profile 61, having a leading edge and formed from a body 70 and an add-on part 74. The add-on part is inserted in a recess in a median part of an end part 73 of the body, said end part forming the bodys leading edge 62. The insert is...

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Bibliographische Detailangaben
Hauptverfasser:	Didier Noel Durand, Olivier Jean Daniel Baumas, Nicolas Daniel Delaporte
Format:	Patent
Sprache:	eng
Schlagworte:	BLASTING COMBINED OPERATIONS ENGINE PLANTS IN GENERAL HEATING LIGHTING MACHINE TOOLS MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING METAL-WORKING NOT OTHERWISE PROVIDED FOR NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES OTHER WORKING OF METAL PERFORMING OPERATIONS STEAM ENGINES TRANSPORTING UNIVERSAL MACHINE TOOLS WEAPONS
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