Louver construction for liner of gas turbine engine combustor

Claim 1

A louver constructed combustor for a gas turbine power plant that has a hot wall portion and a cooler wall portion, the hot wall portion subjected to gases of combustion, the opposing cool wall portion subjected to cooling air flow including a lip on the downstream end of the louver overlying and spaced from the adjacent downstream louver, cooling air holes in a bent portion of the louver upstream of the lip to flow a film of cool air on the inner wall of the cooler wall portion of the louver, a plurality of laterally spaced posts for limiting the deflection of the lip extending in the cool film between the lip and the adjacent cool wall portion and terminating short of the opposing wall, said posts being disposed within said overlying portion of said lip a sufficient distance from the end thereof and being dimensioned relative to the axial extent of said lip such that its axial dimension is sufficiently small and sufficiently axially spaced from said holes such that the flow egressing from said holes has sufficient mixing distance to form a substantially circumferentially uniform film of air and the distance said posts is spaced from the discharge end of the lip is sufficiently long to allow the air film flowing therepass to coalesce providing a substantially circumferentially uniform air film, the relationship of said diameter of said posts, the space of said overlying louver and the distance of said posts from its center line to the end of said lip is at substantially a 1:1:1 ratio.