Damping device for a gas turbine combustor

摘要

The invention relates to a damping device for a gas turbine combustor with significantly reduced cooling air mass flow requirements. The damping device includes a wall with a first inner wall and a second outer wall, arranged in a distance to each other. The inner wall is subjected to high temperatures on a side with a hot gas flow. A plurality of cooling channels extend essentially parallel between the first inner wall and the second outer wall, and at least one damping volume bordered by cooling channels. Furthermore, the damping device includes a first passage for supplying a cooling medium from a cooling channel into the damping volume and a second passage for connecting the damping volume to the combustion chamber. An end plate, fixed to the inner wall, separates the damping volume from the combustion chamber.

主权项

1. A damping device for a gas turbine combustor, comprising:
a first inner wall on a side with a hot gas flow and arranged to be subjected to high temperatures; a second outer wall, arranged at a distance from the first inner wall; a plurality of cooling channels extending parallel between the first inner wall and the second outer wall; at least one damping volume between the inner wall and the outer wall; a first passage for supplying a cooling medium from a cooling channel of the plurality of cooling channels into the damping volume; a neck passage configured to connect the at least one damping volume to a combustion chamber; and an end plate fixed to the first inner wall, separating the damping volume from the combustion chamber, wherein said end plate is provided with the neck passage and includes at least one feed plenum for the cooling medium, at least one exit plenum for the cooling medium and cooling passages enabling a flow of cooling medium from the at least one feed plenum to a second plenum and to the at least one exit plenum in a cooling medium flow path direction, wherein the feed plenum, exit plenum, second plenum, and the cooling passages are formed within the end plate and are in serial flow communication to circulate cooling medium through the end plate, and the exit plenum exhaust cooling medium to the damping volume or combustion chamber.