초록 ▼

A centrifugal chambers gas turbine is disclosed. The turbine comprises a housing, a main shaft mounted on the housing, a rotating cage rotatably mounted on the shaft, a primary combustion chamber mounted in the housing and comprising two concentric walls separated by a predetermined distance and hav

A centrifugal chambers gas turbine is disclosed. The turbine comprises a housing, a main shaft mounted on the housing, a rotating cage rotatably mounted on the shaft, a primary combustion chamber mounted in the housing and comprising two concentric walls separated by a predetermined distance and having at one end an opening permitting entry of compressed gas into the combustion chamber, and at its other end, an opening for exhaust of combustion gases, means for securing the outside wall of the primary combustion chamber to the housing and the inside wall of the primary combustion chamber to the rotating cage, a secondary combustion chamber in communication at one end with the exhaust opening of the primary combustion chamber, and having a plurality of transverse vanes located at its other end through which the exhaust gases of the secondary combustion chamber are ejected, a rotating nozzle including a plurality of transverse vanes located at the output of the vanes of the secondary combustion chamber and secured to the inside wall of the primary combustion chamber for rotation of the inside wall of the primary combustion chamber, a compressor coupled to the rotating cage for compressing gas into the primary and secondary combustion chambers, and a turbine output wheel mounted for rotation on the main shaft and having a plurality of transverse blades located at the output of the transverse vanes of the primary combustion chamber and permitting rotation of such turbine output wheel.

대표청구항 ▼

A gas turbine comprising: (a) a housing: (b) a main shaft mounted in said housing; (c) a rotating cage rotatable on said shaft; (d) a primary combustion chamber mounted in said housing and comprising two concentric walls separated by a predetermined distance and having at one end an opening permitti

A gas turbine comprising: (a) a housing: (b) a main shaft mounted in said housing; (c) a rotating cage rotatable on said shaft; (d) a primary combustion chamber mounted in said housing and comprising two concentric walls separated by a predetermined distance and having at one end an opening permitting entry of compressed gas into the combustion chamber, and at its other end an opening for the exhaust of combustion gases; (e) means for securing the outside wall of said combustion chamber to said housing and the inside wall of said combustion chamber to said rotating cage; (f) a secondary combustion chamber in communication at one end with the exhaust opening of the primary combustion chamber and having a plurality of transverse vanes located at its other end through with the exhaust gases of said secondary combustion chamber are ejected; (g) a rotating nozzle including a plurality of transverse vanes rotated at the output of the vanes of said secondary combustion chamber and secured to the inside wall of said primary combustion chamber for rotation of the inside wall of the primary combustion chamber; (h) a compressor coupled to said rotating cage for compressing gas into the primary and secondary combustion chambers; and (i) a turbine output wheel mounted for rotation on said main shaft and having a plurality of transverse blades located at the output of the transverse vanes of said primary combustion chamber and permitting rotation of said turbine output wheel.