Raytheon Technologies Corporation

Matthew B DeGostin

Jeffrey Michael Jacques

Hoyt Y Chang

John E Paul

Mohamed Hassan

Charles Thistle

Carlos Calixtro

Vladimir Skidelsky

David A Burdette

A self-contained computerized system includes a processor and a memory. The memory stores instructions for causing the self-contained computerized system to perform the process of morphing a finite element mesh of a legacy design to the finite element mesh of a component design and applying measurement variations from the legacy design to the finite element mesh of the component design.

Process for gas turbine engine component design

A damper seal for a turbine blade of a gas turbine engine, the damper seal having: an upper portion; a first downwardly curved portion; and a second downwardly curved portion, the first downwardly curved portion and the second downwardly curved portion extend from opposing end regions of the upper portion, the upper portion having a length extending between the opposing end regions of the upper portion and a width transverse to the length, wherein the upper portion is curved along the entire width as it extends along the length.

Pre-formed faceted turbine blade damper seal

Growing community of inventors

Eastford, CT, United States of America

Matthew B DeGostin