Porous abradable shroud with transverse partitions

Rotary kinetic fluid motors or pumps – With diversely oriented inlet or additional inlet for...

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415174, F01D 1108

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active

042227062

ABSTRACT:
A turbine housing for a jet engine is provided with a ring of an abradable orous material. A supporting and mounting device consisting of a cylindricoconical monoblock having a conical internal jacket provides for the convection cooling of the external surface and a cylindrical jacket for cooling air is held over the abradable ring by means of a perforated ferrule integral with the rest of the device. The abradable ring carries transverse partitions to prevent axial leakage.

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patent: 3365172 (1968-01-01), McDonough et al.
patent: 3656862 (1972-04-01), Rahaim et al.
patent: 3728039 (1973-04-01), Plemmons et al.
patent: 3825364 (1974-07-01), Halila et al.
patent: 3825365 (1974-07-01), Peng
patent: 3834001 (1974-09-01), Carroll et al.

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