Seal plate with concentrate annular segments for a gas turbine e

Power plants – Combustion products used as motive fluid – Plural combustion products generators in ring coaxial with...

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60 3932, F02C 728, F02C 308

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active

050741110

ABSTRACT:
The clearance between a seal assembly 46 and a turbine wheel 14 in a turbine engine of the type having a radial outflow compressor 24 and a radial inflow turbine wheel 14 may be minimized by utilizing a diaphragm assembly 76 as part of the seal assembly 46 and which is formed of multiple pieces in the form of concentric rings 78, 80. In addition, the thermal stress in the rings 78 and 80 will be considerably less than in a single ring as used in existing designs. This greatly extends the useful life of the seal plate assembly before the onset of cracking and other kinds of mechanical failure.

REFERENCES:
patent: 2911138 (1959-11-01), Birmann
patent: 2946192 (1960-07-01), Hambing
patent: 3116908 (1964-01-01), Wosika
patent: 3266250 (1966-08-01), Freeman et al.
patent: 3613360 (1971-10-01), Howes
patent: 3623318 (1971-10-01), Shank
patent: 4009568 (1977-03-01), King et al.
patent: 4439871 (1984-04-01), Weiler et al.
patent: 4446693 (1984-05-01), Pidcock et al.
patent: 4932207 (1990-06-01), Harris et al.

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