Turbine vane mounting arrangement

Details Turbine vane mounting arrangement Turbine vane mounting arrangement

1998-12-22

2000-12-26

Verdier, Christopher

Rotary kinetic fluid motors or pumps

Including thermal expansion joint

Resilient

415138, 415189, 415200, 4152092, 4152094, 4152093, F01D 904, F01D 2526

Patent

active

061649031

ABSTRACT:
A ceramic turbine inlet vane(s) is resiliently mounted to stator portions (10) and (15) of a gas turbine engine by outer and inner resilient mounts (20) and (25). The resilient mounts each include springs, which accommodate varying rates of radial and axial thermal expansion between the vane and adjacent metallic stator structure.

REFERENCES:
patent: 2914300 (1959-11-01), Sayre
patent: 3394919 (1968-07-01), Catterfeld
patent: 5630700 (1997-05-01), Olsen et al.
patent: 5634767 (1997-06-01), Dawson
patent: 6000906 (1999-12-01), Draskovich

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