Third stage turbine airfoil

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

Patent

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Details

F01D 5/14 (2006.01)

Patent

CA 2633323

The present invention provides an airfoil for a third stage blade (138) having an external surface with first and second sides. The external surface extends spanwise between a hub (352) and a tip (354) and streamwise between a leading edge (140) and a trailing edge (142) of the airfoil. The external surface includes a contour substantially defined by Table 1 as listed in the s specification.

La présente invention concerne un profil aérodynamique destiné à une aube de troisième étage et disposant d'une surface extérieure présentant un premier et un deuxième côtés. La surface extérieure s'étend radialement entre un moyeu et une extrémité et dans le sens du flux entre un bord d'attaque et un bord de fuite de ce profil aérodynamique. La surface extérieure possède un contour qui est sensiblement défini par le tableau 1 figurant dans la description.

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