GAS TURBINE ENGINE COMBUSTION CHAMBER Russian patent published in 2013 - IPC F23R3/50 

FIELD: engines and pumps.

SUBSTANCE: gas turbine engine comprises a circular combustion chamber comprising walls formed by rotation, accordingly a radially internal one and a radially external one, relative to the axis of the gas turbine engine connected at their inlet ends by the circular bottom of the chamber equipped with facilities for fuel injection. The gas turbine engine comprises facilities for suspension of the inlet end of the combustion chamber to an external tray. Suspension facilities comprise at least one traction rod hingedly connected by its ends to the wall of the combustion chamber and to the external tray. Each end of the traction rod is hingedly installed around the transverse axis on the cylindrical rod, installed in holes of the eye of the external wall of the chamber or the tray, accordingly. The outlet end of the combustion chamber is connected to the inner or outer tray by flexible connections or supports.

EFFECT: higher efficiency and cost-effectiveness of engine operation.

13 cl, 8 dwg