초록 ▼

A reheat combustion system for a gas turbine comprises a mixing tube adapted to be fed by products of a primary combustion zone of the gas turbine and by fuel injected by a lance; a combustion chamber fed by the said mixing tube; and at least one perforated acoustic screen. The or each said acoustic

A reheat combustion system for a gas turbine comprises a mixing tube adapted to be fed by products of a primary combustion zone of the gas turbine and by fuel injected by a lance; a combustion chamber fed by the said mixing tube; and at least one perforated acoustic screen. The or each said acoustic screen is provided inside the mixing tube or the combustion chamber, at a position where it faces, but is spaced from, a perforated wall thereof. In use, the perforated wall experiences impingement cooling as it admits air into the combustion system for onward passage through the perforations of the said acoustic screen, and the acoustic screen damps acoustic pulsations in the mixing tube and combustion chamber.

대표청구항 ▼

What is claimed is: 1. A reheat combustion system for a gas turbine, the system comprising: a mixing tube adapted to be fed by products of a primary combustion zone of the gas turbine and by fuel injected by a lance; a combustion chamber fed by the mixing tube, at least one of the mixing tube and

What is claimed is: 1. A reheat combustion system for a gas turbine, the system comprising: a mixing tube adapted to be fed by products of a primary combustion zone of the gas turbine and by fuel injected by a lance; a combustion chamber fed by the mixing tube, at least one of the mixing tube and the combustion chamber having a perforated wall; and at least one perforated acoustic screen; wherein the at least one acoustic screen is provided inside the mixing tube or the combustion chamber, at a position where it faces, but is spaced from, the perforated wall thereof; such that, in use, the perforated wall experiences impingement cooling as it admits air into the combustion system for onward passage through the perforations of the acoustic screen, and the acoustic screen damps acoustic pulsations in the mixing tube and combustion chamber; and wherein the mixing tube includes a wall that defines the perforated wall and one of the at least one acoustic screen faces the mixing tube. 2. A gas turbine comprising a reheat combustion system according to claim 1. 3. A reheat combustion system for a gas turbine, the system comprising: a mixing tube adapted to be fed by products of a primary combustion zone of the gas turbine and by fuel injected by a lance; a combustion chamber fed by the mixing tube, at least one of the mixing tube and the combustion chamber having perforated wall; and at least one perforated acoustic screen; wherein the at least one acoustic screen is provided inside the mixing tube or the combustion chamber, at a position where it faces, but is spaced from, the perforated wall thereof; such that, in use, the perforated wall experiences impingement cooling as it admits air into the combustion system for onward passage through the perforations of the acoustic screen, and the acoustic screen damps acoustic pulsations in the mixing tube and combustion chamber; and wherein the mixing tube includes a wall that defines one of the at least one acoustic screen and the perforated wall faces the mixing tube. 4. A gas turbine comprising a reheat combustion system according to claim 3. 5. A reheat combustion system for a gas turbine, the system comprising: a mixing tube adapted to be fed by products of a primary combustion zone of the gas turbine and by fuel injected by a lance; a combustion chamber fed by the mixing tube, at least one of the mixing tube and the combustion chamber having a perforated wall; and at least one perforated acoustic screen; wherein the at least one acoustic screen is provided inside the mixing tube or the combustion chamber, at a position where it faces, but is spaced from, the perforated wall thereof; such that, in use, the perforated wall experiences impingement cooling as it admits air into the combustion system for onward passage through the perforations of the acoustic screen, and the acoustic screen damps acoustic pulsations in the mixing tube and combustion chamber; and wherein the combustion chamber comprises an outer wall which defines one of the at least one acoustic screen and the perforated wall faces the outer wall of the combustion chamber. 6. A gas turbine comprising a reheat combustion system according to claim 5.