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Inner shell radial pin geometry and mounting arrangement

Patent ·
OSTI ID:874771
Circumferentially spaced arrays of support pins are disposed through access openings in an outer turbine shell and have projections received in recesses in forward and aft sections of an inner turbine shell supported from the outer shell. The projections have arcuate sides in a circumferential direction affording line contacts with the side walls of the recesses and are spaced from end faces of the recesses, enabling radial and axial expansion and contraction of the inner shell relative to the outer shell. All loads are taken up in a tangential direction by the outer shell with the support pins taking no radial loadings.
Research Organization:
General Electric Company (Schenectady, NY)
DOE Contract Number:
FC21-95MC31176
Assignee:
General Electric Company (Schenectady, NY)
Patent Number(s):
US 6457936
OSTI ID:
874771
Country of Publication:
United States
Language:
English

References (2)

Advances in Steam Path Technology journal April 1996
Development Requirements for an Advanced Gas Turbine System journal October 1995