Turbine blade with recessed tip

F - Mech Eng,Light,Heat,Weapons – 01 – D

Patent

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Details

F01D 5/20 (2006.01)

Patent

CA 2675151

A turbine blade (1) with a side surface (7) having an aerodynamic profile. The turbine blade (1) further comprises an end surface (6) and is mounted in a turbine, whereby the end surface (6) is delimited by a gap from a casing (8) of the turbine. The end surface (6) comprises a recess (2) which is shaped such that it acts as an improved aerodynamic seal.

La présente invention concerne une pale de turbine (1) dont une surface latérale (7) possède un profil aérodynamique. La pale de turbine (1) comprend en outre une surface d~extrémité (6) et est montée dans une turbine, la surface d~extrémité (6) étant ainsi délimitée par un espace par rapport à un logement (8) de la turbine. La surface d~extrémité (6) comprend un renfoncement (2) formé de manière à assurer une fonction de joint aérodynamique amélioré.

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