| 摘要 |
A pressurized gas turbine engine(74) is disclosed which utilizes a new turbi ne design. Pressurized gas is supplied by nozzle gas ways(6) in the turbine(3) to gas nozzles(5) affixed to the perimeter of the turbine. The gas nozzles(5) m ay be recessed in the turbine perimeter or extend from the turbine perimeter. T he gas nozzles(5) may be equipped with gas exit cones(106) to enhance the efficiency of the nozzles(5). The axis of the nozzles has an obliqu e angle with the direction of rotation of the turbine. Pressurized gas is supplied t o the nozzle gas ways(6) through one or more shaft gas ways(8) in the turbine shaft(2), or is supplied through engine gas ports(75) in the front wall(10) of the turbine engine to gas supply zones(77) which are hydraulically separated by seal rings(76) on the front face(11) of the turbine, each gas supply zone(77) being hydraulically connected to one or more nozzle gas ways(6).</S DOAB>
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