Invention Grant
US09279369B2 Turbomachine with transition piece having dilution holes and fuel injection system coupled to transition piece 有权
具有过渡件的涡轮机具有稀释孔和连接到过渡件的燃料喷射系统

Turbomachine with transition piece having dilution holes and fuel injection system coupled to transition piece
Abstract:
A turbomachine is provided and includes a combustor in which fuel and air are combusted, a turbine disposed for reception of products of combustion from the combustor, a transition piece fluidly interposed between the combustor and the turbine and including a body formed to define dilution holes configured to allow air to enter the combustor and for enabling steam injection toward a main flow of the products of the combustion proceeding from the combustor to the turbine and a fuel injection system supportively coupled to the transition piece and configured to inject fuel toward the main flow of the products of the combustion to thereby restore a flame temperature of the main flow of the products of the combustion reduced by steam injection enabled by the dilution holes.
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