Combustor of gas turbine

Abstract

A combustor of a gas turbine according to one aspect of the present disclosure includes: an outside wall surrounding a combustion chamber; a liner located inside the outside wall and facing the combustion chamber; a spacer at least part of which is located between the outside wall and the liner; a fastener at least part of which is located outside the outside wall; and a fixture by which the liner is attached to the outside wall and which includes a head supporting the liner and a shaft portion penetrating the outside wall and fastened to the fastener. The fastener includes a fastener groove extending along the fixture, a first air passage being located at the fastener groove. The spacer includes a spacer groove extending along the fixture, a second air passage through which air having flowed through the first air passage flows being located at the spacer groove.

Dependencies are inferred from the claim text.