Raytheon Technologies Corporation

Salvatore D'Alessandro

Gary J Dillard

A combustor liner assembly includes a first liner panel that has a first forward end and a first aft end. A second liner panel has a second forward end and a second aft end. A support band has a plurality of circumferentially spaced holes. The support band is arranged between the first liner panel and the second liner panel. The support band has a protrusion with a first angled surface and a second angled surface. The first angled surface is in engagement with the first aft end and the second angled surface in engagement with the second forward end.

Growing community of inventors

Jupiter, FL, United States of America

Salvatore D'Alessandro