Draining and cooling system for gas turbine bearings

F - Mech Eng,Light,Heat,Weapons – 01 – D

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Details

F01D 9/06 (2006.01) F01D 25/12 (2006.01) F01D 25/16 (2006.01) F01D 25/32 (2006.01) F02C 7/06 (2006.01)

Patent

CA 2676235

A draining and cooling system for gas turbine cushions where the above-mentioned gas turbine has its own drain unit (11), which consists of two essentially concentric rings connected to each other by means of a number of spokes (12, 13). In the draining system described, the lubricating and cooling oil is fed into the gas turbine's drain unit (11) by means of at least a first pipe (14), located inside one of the spokes (12) and is drained by means of at least a second pipe (20), located inside one of the spokes (13).

L'invention concerne un système d'évacuation et de refroidissement destiné aux amortisseurs d'une turbine à gaz comportant sa propre unité d'évacuation (11). Ce système est constitué par deux anneaux sensiblement concentriques reliés l'un à l'autre par des ailettes (12, 13). Dans ce système d'évacuation, l'huile de lubrification et de refroidissement est acheminée dans l'unité d'évacuation (11) de la turbine à gaz par l'intermédiaire d'au moins un conduit (14) situé dans l'une des ailettes (12), puis évacuée via au moins un second conduit (20) situé dans l'une desdites ailettes (13).

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