FIELD: engines and pumps.
SUBSTANCE: gas turbine combustion chamber consists of an outer and inner casings and a flame tube incorporating a front device made as a tapered blade-type swirler with its blades arranged between its inner and outer walls. The said swirler inner and outer walls are furnished with closed interconnected spaces in the blades with their outer edge provided with an open channel communicating with the aforesaid closed space. The swirler outer wall accommodates a bracket with an open space communicating with the aforesaid swirler outer wall space and a flange to be attached to the combustion chamber outer casing flange.
EFFECT: utilisation of pit-shaft petroleum gas by combusting it in the ground gas turbine combustion chamber.
3 dwg
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