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US 2014/0112769 A1Published application
Gas turbine
AssigneeMTU Aero Engines AG
InventorHarald Schoenenborn
Life of this patent
Estimating the term…
Abstract
A gas turbine having a system of stages including at least one stage having first and second airfoils arranged alternately in the circumferential direction. The first airfoils each have a first array of cavities and the second airfoils each have a second array of cavities different from the first array of cavities.
Claims15
A gas turbine having a system of stages comprising:
- at least one stage having first and second airfoils arranged alternately in the circumferential direction, wherein the first airfoils each have a first array of cavities and the second airfoils each have a second array of cavities different from said first array of cavities.
Dependencies are inferred from the claim text.