A multi-shaft reheat turbine mechnism includes multiple turbines mounted on respective compressor shafts, and catalytic reactors feeding respective ones of the turbines. Fuel is introduced into a low pressure compressor, whereby there is no need to pressurize the fuel. The compressor side of the mechanism emits a compressed air/fuel flow, portions of which are combusted in respective ones of the catalytic reactors. The air/fuel flow traveling from the compressor side to the turbine side passes through a regenerator in heat exchanging relationship with exhaust gas from a low pressure turbine.
申请公布号
WO9945251(A1)
申请公布日期
1999.09.10
申请号
WO1999US04784
申请日期
1999.03.04
申请人
SOLO ENERGY CORPORATION;MONGIA, RAJIV, K.;BUCKLEY, STEVEN, G.;TOUCHTON, GEORGE, L.;DIBBLE, ROBERT, W.;NEUHAUS, PETER, D.