Composite seal for turbomachinery

Rotary kinetic fluid motors or pumps – Bearing – seal – or liner between runner portion and static part – Erodable or permanently deformable

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Details

415196, F01D 1108

Patent

active

042957869

ABSTRACT:
A gas path seal suitable for use with a turbine engine or compressor is provided. A shroud wearable or abradable by the abrasion of the rotor blades of the turbine or compressor shrouds the rotor blades. A compliant backing surrounds the shroud. The backing is a yieldingly deformable porous material covered with a thin ductile layer. A mounting fixture surrounds the backing.

REFERENCES:
patent: 3887299 (1975-06-01), Profant
patent: 4022481 (1977-05-01), Long et al.
patent: 4135851 (1979-01-01), Bill et al.
patent: 4207024 (1980-06-01), Bill et al.

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