Honeywell International Inc.

Jeffrey Aitchison

Jason Smoke

Harry Lester Kington

Shawn Alstad

Andrew Appleby

Timothy Darling

Courtney Murphy

William Weiss

Laurence Liston

A shroud system for a gas turbine engine. The shroud system includes a support structure defining two stages. One shroud is disposed at one stage and another shroud is disposed at the other stage. A retention and positioning assembly is disposed on the support structure and positions and holds both shrouds relative to the support structure. A load transfer pin is located radially outward from each of the shrouds. A spring is coupled to the support structure and engages both load transfer pins. The spring applies forces on the load transfer pins toward their respective shroud. A retainer is coupled with the support structure and extends over both stages.

Shroud system with two-stage spring and retainer system for gas turbine engine shroud

Growing community of inventors

Phoenix, AZ, United States of America

Jeffrey Aitchison