TOROID-SHAPED GAS TURBINE OF BOUNDARY LAYER Russian patent published in 2015 - IPC F01D1/36 

Abstract RU 2551469 C2

FIELD: power industry.

SUBSTANCE: combustion housing includes a toroid-shaped combustion chamber receiving centrifugal forces caused by combustion, which occur at ignition of vortex of combustion fluid medium along the whole above said toroid-shaped combustion chamber; and an outlet hole of the above said toroid-shaped combustion chamber. The combustion turbine includes a shaft, several discs distributed in space and radially connected to the above shaft in the centre of the above said several discs; and a combustion chamber. The combustion chamber contains fluid medium subject to combustion and has at least one wall that partially envelopes the above said several discs. The fluid medium subject to combustion flows from the above said combustion chamber and is redirected for its tangential flow above adjacent surfaces of the above said several discs, thus making the above said several discs rotate.

EFFECT: achievement of a simple design and increase of energy output due to more effective fuel consumption in larger amount, as well as by transmission of higher rotation to combustion products.

16 cl, 9 dwg

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RU 2 551 469 C2

Authors

Bergen Ehrnst

Dates

2015-05-27Published

2009-10-29Filed