Metal-ceramic turbine shroud and method of making the same

Rotary kinetic fluid motors or pumps – Working fluid passage or distributing means associated with... – Specific casing or vane material

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291564WL, 264 62, 264 81, 428593, 428598, F01D 2524, B32B 300

Patent

active

042894476

ABSTRACT:
A turbine shroud includes a ceramic sealing layer secured to a metal substrate. In one form, the metal substrate includes a plurality of pegs extending therefrom. Intermediate bonding layers are disposed on the peg-metal substrate structure. A ceramic sealing layer of zirconium oxide with about 20 weight percentage magnesium oxide is disposed, e.g., plasma sprayed, on the intermediate bonding layers. The ceramic sealing layer includes an ordered pattern of very fine cracks therein which reduce the thermal stress in the ceramic sealing layer. A method of constructing a turbine shroud structure is also disclosed.

REFERENCES:
patent: 3053694 (1962-09-01), Daunt et al.
patent: 3126149 (1964-03-01), Bowers, Jr. et al.
patent: 3339933 (1967-09-01), Foster
patent: 3519282 (1970-07-01), Davis
patent: 3843278 (1974-10-01), Torell
patent: 3975165 (1976-08-01), Elbert et al.
patent: 4087199 (1978-05-01), Hemsworth et al.
Shiembob, L. T. Development of a Plasma Sprayed Ceramic Gas Path Seal for High Pressure Turbine Applications, NTIS N77-25534, Apr. 1977, p. (i 1-8, 55).

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