Vane actuation system

Rotary kinetic fluid motors or pumps – Including thermal expansion joint

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Details

415149R, 415162, F01D 1716

Patent

active

044001355

ABSTRACT:
An improved vane actuation system for a gas turbine engine having adjustable stator vanes in stages between which the engine casing exhibits relative axial and radial thermal growth, the improved system including a pair of platforms on the casing forming therewith three bar link arrangements which automatically compensate for radial and axial thermal growth, rollers on each platform supporting vane actuation rings in centered relationship on the axis of the engine, connectors between the rings and the vane arms which locate the vanes but which permit radial expansion of the arms to accommodate radial thermal growth, a pair of bell cranks on each platform operated remotely and simultaneously, and links between each bell crank and corresponding ones of the rings operative to rotate the rings and, in combination with the rollers, to foreclose translation of the rings in their respective planes.

REFERENCES:
patent: 2817475 (1957-12-01), Moody
patent: 2858062 (1958-10-01), Allen
patent: 2999630 (1961-09-01), Warren et al.
patent: 3356288 (1967-12-01), Corsmeier
patent: 3458118 (1969-07-01), Burge et al.
patent: 3487992 (1970-01-01), Pineda
patent: 3841788 (1974-10-01), Sljusarev et al.
patent: 3873230 (1975-03-01), Norris et al.

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