A Fuel Supply System for Supplying Fuel to a Combustion Section of a Gas Turbine

A fuel supply system supplies fuel to a plurality of combustion sectors (70,74) of a combustion section of a gas turbine. Each of the combustion sectors includes at least two combustors. The fuel supply system generally includes a fuel distribution manifold (60) that is in fluid communication with a fuel supply. A first flow path (68) is defined between the fuel distribution manifold (60) and a first combustion sector (60). A second flow path (72) is defined between the fuel distribution manifold (60) and a second combustion sector (74).