Diffuser part for a gas turbine
AssigneeRolls-Royce Deutschland Ltd & Co KG
InventorsCarsten CLEMEN, Ivo SZARVASY
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Abstract
A diffuser component for a gas turbine is provided, where a fluid flow in the direction of a combustion chamber of the gas turbine can be slowed down by the diffuser component, and a flow cross-section of the diffuser component, which is defined by a diffuser wall is widened to do so. The diffuser wall is at least locally braced, in that at least one stiffening element with a lattice-type structure is provided on the diffuser wall.
Claims15
A diffuser component for a gas turbine, where a fluid flow in the direction of a combustion chamber of the gas turbine can be slowed down by the diffuser component, and a flow cross-section of the diffuser component, which is defined by a diffuser wall is widened to do so, wherein at least one stiffening element with a lattice-type structure is provided on the diffuser wall, said stiffening element bracing the diffuser wall in at least one section.
Dependencies are inferred from the claim text.