Rotary kinetic fluid motors or pumps – Bearing – seal – or liner between runner portion and static part – Between blade edge and static part
Patent
1998-02-13
2000-05-30
Look, Edward K.
Rotary kinetic fluid motors or pumps
Bearing, seal, or liner between runner portion and static part
Between blade edge and static part
4151731, 4151736, 4151745, 416189, F01D 520
Patent
active
060684437
ABSTRACT:
The invention relates to a cavity constituted by a casing of a gas turbine and a moving blade with a tip shroud, by which a cavity space is made to a necessary minimum size, a main flow gas is prevented from being entrained and a pressure loss is reduced. A tip shroud (6) is mounted on a tip end portion of a moving blade (4), a fin (7) is mounted thereon, a recess-like cavity (15) narrower than the conventional one is formed by portions (12a) and (12b) of a casing (12) and the fin (7), and further a projecting portion (16) is provided to an upstream end portion of the tip shroud (6). The projecting portion (16) is at a position (13a) at a time of a cold start and is at a position (13b) at a time of a hot start run, even if a thermal expansion occurs, thus the projecting portion (16) is not in contact with the recess portion, a main flow gas (1) is less entrained within the cavity (15), and a pressure loss is reduced because of no swirl, so that a performance of the gas turbine is enhanced.
REFERENCES:
patent: 3314651 (1967-04-01), Beale
patent: 4161318 (1979-07-01), Stuart et al.
patent: 5188507 (1993-02-01), Sweeney
patent: 5205706 (1993-04-01), Belcher
Aoki Sunao
Ito Eisaku
Look Edward K.
Mitsubishi Heavy Industries Ltd.
Nguyen Ninh
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