| 摘要 |
<p>The present invention relates to a burner device for a gas turbine. The burner device comprises a burner body (120), wherein the burner body (120) comprises an axial end face (123). The burner body (120) further comprises a first supply channel (121) which has a first opening in the axial end face (123). The burner device further comprises a burner end element (100) which is arranged at the axial end face (123). The burner end element (100) comprises a first plenum chamber (101) which is coupled to the first opening of the first supply channel (121), such that a first fluid is feedable from the first supply channel (121) to the first plenum chamber (101). The burner end element (100) further comprises a lattice structure (103) with a plurality of interconnected pores, wherein the first plenum chamber (101) is coupled to the lattice structure (103) for feeding the first fluid into the lattice structure (103). The lattice structure (103) forms a part of a burner surface (104) which points to a burning chamber (140) of the gas turbine such that a fluid connection between the burning chamber (140) and the lattice structure (103) is formed.</p> |
