To provide an improved closure turbine bucket capable of supporting aerofoil without generating excessive stress.
A closure bucket group 100 is installed on a dovetail 140 of a turbine wheel 150. The closure bucket group 100 may include a leading bucket 110 with a leading bucket rear side, a closure bucket 120 with a closure bucket front side and a closure bucket rear side, and a trailing bucket 130 with a trailing bucket front side. The leading bucket rear side and the closure bucket front side define a pair of first enclosed keyway 390, and the closure bucket rear side and the trailing bucket front side define a pair of second enclosed keyway 400. A plurality of keys 410 and 420 may be arranged in the first enclosed keyway 390 and the second enclosed keyway 400.
COPYRIGHT: (C)2008,JPO&INPIT
LAVASH JOHN CLELAND
JPS62111102A | 1987-05-22 | |||
JPS623102A | 1987-01-09 | |||
JP2000220405A | 2000-08-08 |
US1415266A | 1922-05-09 | |||
US2220918A | 1940-11-12 | |||
US2844355A | 1958-07-22 | |||
US4165949A | 1979-08-28 | |||
GB2006884A | 1979-05-10 | |||
EP0369926A1 | 1990-05-23 |
Hirokazu Ogura
Toshihisa Kurokawa
Arakawa Satoshi
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