General Electric Company

Mohsin Hasan Khan

Rebinth Jose Robin

Lyle D Dailey

Ravikanth Avancha

Ganesh Seshadri

Aditya Bhakta

Karunamay Pathak

Sarasija Sudharsan

A turbine rear frame for a gas turbine engine comprises a plurality of struts disposed between an outer ring and an inner ring. The struts can be mounted adjacent to one or more mount surfaces defined within the outer ring. The mount surface can comprise a recess in the outer ring having a maximum radial distance upstream of engine mounts inserted therein. The struts can further comprise a pitch angle offset from a centerline of the mount surface and a tangentially curved trailing edge at a tip to improve aerodynamic performance of the turbine rear frame.

Turbine rear frame for a turbine engine

Systems, computer-implemented methods and/or computer program products that facilitate aviation engine inspection are provided. In one embodiment, a computer-implemented method comprises: generating, by a system operatively coupled to a processor, a digital grid and visual layer overlay on a raw video feed from borescope inspections; analyzing, by the system, the video feed and identifying frames that capture information of part damage and defects; and classifying, by the system, type of part defect, determining location of defect and learning the digital grid.

Best image grab from video with digital grid assistance for aviation engine borescope inspection

Growing community of inventors

Sirohi, India

Mohsin Hasan Khan