Gas turbine

Joints and connections – Utilizing thermal characteristic – e.g. – expansion or... – Members having different coefficients of expansion

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Details

403272, 416244A, 416241B, F16C 900, F16D 100

Patent

active

046592458

ABSTRACT:
A gas turbine including a joint structure is disclosed. According to the joint structure, a ceramic shaft is received in a bore formed in an end portion of a metallic shaft. Brazing filler metal made of Ag-Cu alloy is distributed between the closely fitted surfaces of the ceramic shaft and bore wall, and it extends axially toward the open end of the bore up to a predetermined plane where a ring seal groove formed on the end portion of the metallic shaft lies. The open end of the bore is closed to prevent entrance of exhaust gas into the bore.

REFERENCES:
patent: 3801226 (1974-04-01), Bevan et al.
patent: 4424003 (1984-01-01), Brobeck

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