| 摘要 |
<p>PROBLEM TO BE SOLVED: To reduce or avoid limitations in design of downstream components, such as combustion chamber and turbine components, when utilizing a limited burner exit area.SOLUTION: A reheat burner arrangement includes a center body, an annular duct with a prescribed cross-section area, and an intermediate fuel injection plane located along the center body and actively connected to the cross section area of the annular duct. The center body is located upstream of a combustion chamber. The structure of the reheat burner arrangement is defined by various different parameters, and the structure of the reheat burner arrangement is defined by various interrelations.</p> |
