Compressor diaphragm assembly

Rotary kinetic fluid motors or pumps – Working fluid passage or distributing means associated with... – Vane or deflector

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Details

415189, 4152092, F04D 2954

Patent

active

050228188

ABSTRACT:
A compressor diaphragm assembly for combustion turbines includes a plurality of vane airfoils, each of which is formed with an integral inner shroud and an integral outer shroud, joined together by connecting bars which transfer loads between the vane airfoils and the casing slots of the turbine within which the vane airfoils are suspended.

REFERENCES:
patent: 2683583 (1954-07-01), Huebner, Jr. et al.
patent: 2917276 (1959-12-01), Klompas et al.
patent: 3326523 (1967-06-01), Bobo
patent: 3338508 (1967-08-01), Castle et al.
patent: 3393436 (1968-07-01), Blackhurst et al.
patent: 3997280 (1976-12-01), Germain
patent: 4014627 (1977-03-01), Heurteux
patent: 4889470 (1989-12-01), Scalzo

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