Turbomachine blade, turbomachine and method for manufacturing the blade
AssigneeSafran Helicopter Engines
InventorsDamien Laberny, Loïs Pierre Denis Vive, Alexandre Hervé René Montpellaz, Fabrice Iparaguirre
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AssigneeSafran Helicopter Engines
InventorsDamien Laberny, Loïs Pierre Denis Vive, Alexandre Hervé René Montpellaz, Fabrice Iparaguirre
Estimating the term…
Turbomachine blade including an external shell including a pressure-side wall and a suction-side wall delimiting between them an interior volume, an insert arranged in the interior volume so as to form an air passage between the insert and the external shell; and at least one breakable joining portion, connected on the one hand to the insert and on the other hand to the external shell; wherein one at least of the mechanical breaking resistance of the breakable joining portion, the mechanical breaking resistance between the breakable joining portion and the external shell and the mechanical breaking resistance between the breakable joining portion and the insert is less than the mechanical breaking resistance of the external shell and the mechanical breaking resistance of the insert.
A turbomachine blade comprising:
Dependencies are inferred from the claim text.