发明名称 PERFEZIONATO STADIO DI TURBINA A VAPORE.
摘要 A stage of an axial flow turbine includes a plurality of spaced apart buckets and a plurality of spaced apart nozzle partitions, each plurality respectively circumferentially aligned about and axially spaced from each other along a rotor of the turbine. The nozzle partitions are circumferentially spaced such that a minimum throat extends a predetermined radial distance from the root, thereby forming a converging-diverging flow passageway between nozzle partitions. The trailing edge of the nozzle partitions are disposed to include axial and tangential lean with respect to the rotor. Buckets include a plurality of covers respectively connecting the tips and having a single outward radially extending sealing rib on the radially outer surface of each cover, wherein each rib is tangentially aligned with respective adjacent ribs. Buckets are overtwisted to compensate for untwist at operational speed to achieve optimum efficiency. Buckets are circumferentially spaced to provide a converging-diverging channel therebetween and include lashing for providing mechanical coupling at operational speed.
申请公布号 IT8521318(D0) 申请公布日期 1985.06.27
申请号 IT19850021318 申请日期 1985.06.27
申请人 GENERAL ELECTRIC CO. 发明人 KENNETH ELMER ROBBINS;STEPHEN GARRISON RUGGLES;DAN DUNCAN;JOHN CLIFTON WILLIAMS;STEPHEN KIN-KEUNG TUNG;WILLIAM JAMES SUMNER;COUNG VAN DINH
分类号 F01D5/22;F01D5/02;F01D5/14;F01D9/02;F01D9/04;F01D11/08 主分类号 F01D5/22
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