Internally cooled gas turbine airfoil and method

Details Internally cooled gas turbine airfoil and method Internally cooled gas turbine airfoil and method

F - Mech Eng,Light,Heat,Weapons

01

D

F01D 5/18 (2006.01) F02C 7/12 (2006.01)

Patent

CA 2528098

An internally cooled airfoil for a gas turbine engine, wherein a plurality of elongated cooling fins are provided inside the concave sidewall between two crossovers.

Il s'agit d'un profil aérodynamique à refroidissement interne pour turbine à gaz dans lequel de multiples ailettes de refroidissement allongées occupent la paroi latérale concave comprise entre deux éléments de jonction doubles.

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