Thermal isolation device for liquid fuel components
AssigneeGeneral Electric Company
InventorsKeith Cletus Belsom, Michael Damian Seal
Life of this patent
Estimating the term…
Abstract
A thermal isolation device for a gas turbine combustor assembly includes a plurality of substantially flat plates secured in spaced relationship by a plurality of columns, at least one column incorporating a bolt hole for use in securing the device between a pair of combustor components.
Claims14
A gas turbine combustor assembly comprising a thermal isolation device having a plurality of substantially flat plates secured in spaced relationship to a plurality of columns, at least one column incorporating a bolt hole, and a bolt extending through the bolt hole and securing the device between a pair of combustor components.
A thermal isolation device for a gas turbine combustor assembly comprising at least three dicrete substantially flat and substantially triangular-shaped plates secured in spaced, substantially parallel relationship to at least three columns, that pass through said plated, each column formed with a through hole adapted to receive a bolt.
Dependencies are inferred from the claim text.