发明名称 GAS TURBINE COMBUSTOR
摘要 PURPOSE:To provide a high activity at a low temperature, a durability at a high temperature, a long life and to restrict a generation of NOx by a method wherein a catalyst is made in two-stages, the front and rear stage catalyst is of noble metal and an active carrier of the rear stage catalyst is of a lacked perovskite structure. CONSTITUTION:Fuel injected from a combustion nozzle 1 is mixed with combustion air 3, its mixture gas at first flows into a front stage catalyst 8a and then flows into a rear-stage catalyst 8b, thereafter it is discharged to a turbine nozzle 7. A layer of active carrier of the front stage catalyst 8a is a layer which is a mixture of a noble metal an a rare earth metal with an active carrier, for example, alumina. In view of an affinity with noble metal and activity, gamma-alumina is preferable. The noble metal to be used here is a palladium (Pd). The active carrier to be used in rear stage catalyst 8b is of a lacked perovskite structure in which alumina and rare earth are present which a weight ratio (rare earth metal/alumina) of more than 1 and the noble metal is platium (Pt) or platium alloy.
申请公布号 JPS62218728(A) 申请公布日期 1987.09.26
申请号 JP19860059595 申请日期 1986.03.19
申请人 TOKYO ELECTRIC POWER CO INC:THE;TOSHIBA CORP 发明人 ITO MASAMICHI;OGOSHI AKIO;SHIZUKAWA KENJIROU;HAYATA TERUNOBU;FURUYA TOMIAKI;YAMANAKA CHIKAU;HIZUKA JUNJI
分类号 F23R3/40;B01J23/42;B01J23/44;B01J23/78;B01J35/04;F23C13/00 主分类号 F23R3/40
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