F - Mech Eng,Light,Heat,Weapons – 01 – D
Patent
F - Mech Eng,Light,Heat,Weapons
01
D
F01D 9/04 (2006.01) F01D 11/18 (2006.01)
Patent
CA 2515175
In the gas turbine split ring, on an outer peripheral surface 1b between two cabin attachment flanges, a circumferential rib which extends in the circumferential direction and an axial rib which extends in the axial direction and has a height taller than that of the circumferential rib are, respectively, formed in plural lines, so that it is possible to suppress heat deformation in the axial direction which largely contributes to reduction of the tip clearance compared to head deformation in the circumferential direction more efficiently.
Fujikawa Tatsuaki
Inoue Shinichi
Kuwabara Masamitsu
Magoshi Ryotaro
Tomita Yasuoki
Fetherstonhaugh & Co.
Mitsubishi Heavy Industries Ltd.
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