General Electric Company
Turbine engine with airfoil having high acceleration and low blade turning

Last updated:

Abstract:

A turbine engine with at least a compressor section, combustor section, turbine section and a set of airfoils. The airfoils include geometric characteristics to create a high contraction ratio (CR), a low blade turning (BT) at a radially inward location the airfoil, a low solidity, or a low aspect ratio (AR).

Status:
Grant
Type:

Utility

Filling date:

14 Jan 2021

Issue date:

6 Sep 2022