AIRFOIL SUPPORT AND COOLING SCHEME

摘要

In various embodiments, an airfoil used as a turbine blade for a turbine wheel in a gas turbine engine is provided. The airfoil may comprise a root, a tip, and a body. The root may have a first area. The tip may have a second area. The body may have a chord bounded by the root and the tip. The body may also define a cooling chamber. The cooling chamber may have a first rib substantially perpendicular to the chord. The cooling chamber may also have a second rib extending partially between the root and the tip.

主权项

1. An airfoil, comprising:
a root having a first area; a tip having a second area; a body having a chord bounded by the root and the tip, the body defining a cooling chamber, the body having a first rib substantially perpendicular to the chord and a second rib extending from the tip region toward the root, the second rib terminating at a point in the cooling chamber between the root and the tip.