United Technologies Corporation

Raytheon Technologies Corporation

Rtx Corporation

Eric Beach

Jorge I Farah

Javier Nebero Johnson

Chris Bates

Caleb N Cross

Jeffery A Lovett

Jeffrey A Lovett

Robert Ken Hon

Caleb Cross

Michel E Nackoul

A system for limiting deflection of an exhaust sidewall liner on a variable geometry exhaust duct uses a spacer and a T-bolt. The system connects the exhaust sidewall liner to the static structure on a variable geometry exhaust duct. The spacer includes a chimney having a first side and a second side opposite of the first side, an aperture extending from the first side to the second side, a flange disposed on the first side, and at least one anti-rotation tab disposed on the second side near an edge of the second side. The T-bolt includes an elongated shaft that extends along an axis and having a diameter, and a head having at least one straight edge connected to an end of the shaft. The at least one straight edge engages with the anti-ration tab, thereby preventing rotation of the stud T-bolt about the axis.

Exhaust liner deflection limiter

An augmentor vane assembly of a gas turbine engine with an additively manufactured augmentor vane, the additively manufactured augmentor vane having a vane wall with integral longitudinal wall passages formed therein, at least one of the integral longitudinal wall passages including at least one entrance aperture and at least one exit aperture, the at least one exit aperture transverse to the integral longitudinal wall passage.

Augmentor vane assembly of a gas turbine engine with an additively manufactured augmentor vane

A gaspath component includes a flowpath body. A cooling plenum is disposed within the flowpath body. The cooling plenum includes a first region configured to receive a cooling flow and a second region configured to expel the cooling flow from the flowpath body. A metering obstruction is positioned between the first region and the second region and is configured to meter a flow of coolant through the cooling plenum.

Cooling system for a gaspath component of a gas powered turbine

An augmentor vane assembly includes an additively manufactured augmentor vane and a fuel line additively manufactured within the augmentor vane. A method of manufacture including additively manufacturing an augmentor vane having a wall that forms an internal volume therein; and additively manufacturing a fuel line within the augmentor vane that extends through the internal volume.

Additively manufactured augmentor vane of a gas turbine engine with additively manufactured fuel line extending therethrough

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Coventry, CT, United States of America

Eric Beach