Method for cooling a turbo machine and turbo machine
AssigneeSiemens Aktiengesellschaft
InventorsMichael Diesler, Martin Grosse Duweler, Uwe Hoffstadt, Oliver Myschi, Uwe Zander
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AssigneeSiemens Aktiengesellschaft
InventorsMichael Diesler, Martin Grosse Duweler, Uwe Hoffstadt, Oliver Myschi, Uwe Zander
Estimating the term…
The invention relates to a method and a device for cooling thermally stressed regions in a turbo machine which has a live-steam feed line (9), an inflow region (17), a housing (2) and an exhaust-steam region (7), a flow medium flowing through the turbo machine (1) and leaving in the exhaust-steam region (7) during operation, part of the flow medium from the live-steam feed line (9) being passed to the exhaust-steam region (7) and cooled by means of a heat exchanger (8) before entry into the turbo machine (1) and entering the turbo machine (1) via the inflow region (17), thermally stressed regions that are located in the inflow region (17) being cooled by the flow medium that has been cooled in this way.
A method for cooling thermally stressed regions in a turbo machine (1) which has a live-steam feed line (9), an inflow region (17), a housing (2) and an exhaust-steam region (7), a flow medium flowing through the turbo machine and leaving in the exhaust-steam region (7) during operation, characterized in that part of the flow medium from the live-steam feed line (9) is cooled by means of a heat exchanger (8) before entry into the turbo machine (1) and enters the turbo machine (1) via the inflow region (17), thermally stressed regions that are located in the inflow region (17) being cooled by the flow medium that has been cooled in this way.
A turbo machine (1) which has a live-steam feed line (9) through which a flow medium can flow and which leads to a live-steam inflow region (12), the turbo machine (1) having an exhaust-steam region (7), characterized in that the live-steam feed line (9) has a branch (10) with which part of the flow medium is passed via a line (15) to a heat exchanger (8), and the turbo machine (1) has a feed line (16) downstream of the heat exchanger (8) into an inflow region (17) of the turbo machine (1).
Dependencies are inferred from the claim text.