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