Transition piece seal spring for a gas turbine

Rotary kinetic fluid motors or pumps – Bearing – seal – or liner between runner portion and static part – Resilient – flexible – or resiliently biased

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Details

4151701, 415135, 277 97, 277236, 277206A, 277DIG9, F01D 1100

Patent

active

051257963

ABSTRACT:
The transition piece seal spring includes a pair of integrally formed spring clips folded at one end to define a support slot, the spring clips being disposed in back-to-back relation one to the other. Each spring clip includes a pair of elongated, arcuately disposed spring segments spaced one from the other defining a slot for receiving the outwardly directed flange of the transition piece edge. A flat leaf spring is received in the support slot and mounts the spring clip to the first-stage turbine outer nozzle support ring such that the spring clips depend radially between the flanges of adjacent edges of the transition pieces. The spring clips enable radial, circumferential and axial vibratory movement of the adjacent transition pieces whereby motion is taken up in high cycle fatigue rather than wear.

REFERENCES:
patent: 3817654 (1974-06-01), Sohma
patent: 4067585 (1978-01-01), Rode
patent: 4303249 (1981-12-01), Illy
patent: 4379560 (1983-04-01), Bakken
patent: 4410163 (1983-10-01), Scobie et al.
patent: 4465284 (1984-08-01), Szema
patent: 4759555 (1988-07-01), Halling
patent: 4850521 (1989-07-01), Servant
patent: 5002288 (1991-03-01), Morrison et al.

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