Alsthom-atlantique

Societe Anonyme Dite: European Gas Turbines Sa

Jacques Poux

Liberto Gandia

Frederic Rouget

Pierre Belle

The present invention relates to an exhaust diffuser for a gas turbine, the diffuser being designed to be inserted downstream from a last expansion stage constituted by an outlet duct of circular cross-section containing a central bulb. The diffuser includes a flared transition duct having an inlet end of circular cross-section identical to the cross-section of the outlet duct of the last stage, an outlet end of square cross-section, and four fixed fins disposed inside the ducts close to respective corners of the square cross-section for directing the exhaust gases toward the corners of the square cross-section.

Gas turbine exhaust diffuser

An inlet grating (11) is constituted by a thin corrugated sheet having rounded corrugation tops (15) facing incident gas flow (25) arriving at an oblique angle. The corrugations are parallel and regularly spaced with perforations at the bottoms thereof (23). Suitable choice of dimensions, together with optional auxiliary openings (24), can ensure a uniform flow perpendicular to the plane of the trough bottoms at a suitable distance therefrom. This is of particular application to drying apparatus.

Fluid circulation apparatus using fluid flow deflection grating

An electrolyzer cell is made up of a pair of electrodes (1,1') separated by a diaphragm (2). The diaphragm is sandwiched between a pair of frames (3,3') and generally includes its own frame (4). It is difficult to make frames sufficiently accurately for large cells (e.g. up to 2 m.sup.2). using conventional techniques of cutting the frame out from a sheet of material or by one-piece moulding. The present invention uses assembly of elongate frame components. Preferably they are joined together using dovetail joints (31,41), which ensure adequate sealing, and with the dovetails shifted from one frame to the next to ensure a more uniform pressing effect.

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Grenoble, France

Jacques Poux