United Technologies Corporation

Raytheon Technologies Corporation

Dairus Deylan McDowell

Jeremy Drake

Brian C McLaughlin

Thomas E Clark

Timothy M Davis

Richard K Hayford

Brian Duguay

Michael S Stevens

Peter J Milligan

Jaimie Schweitzer

Ryan M Kohn

Aspects of the disclosure are directed to a seal comprising: a first leg that emanates from a center point of the seal and is configured to contact a first component, a second leg that emanates from the center point and is configured to contact a second component that is operative at a temperature that is within a range of 648 degrees Celsius to 1093 degrees Celsius, and a third leg that emanates from the center point.

Creep resistant axial ring seal

A method of assembling a gas turbine engine is provided that includes locating a consumable assembly tool within the engine. The consumable assembly tool is attached to another component of the gas turbine engine. The engine is run to vaporize the consumable assembly tool.

Consumable assembly tool for a gas turbine engine

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Shapleigh, ME, United States of America

Dairus Deylan McDowell