Gas turbine containing an additional combustion gas compressor
AssigneeBBC Brown, Boveri & Company, Limited
InventorTadeusz Zaba
Life of this patent
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Abstract
A gas turbine containing an additional combustion gas compressor and a gearing drive which, on the one hand, is rotatably connected by means of a rigid coupling and an axial bearing with the gas turbine and, on the other hand, is rotatably connected by means of a further rigid coupling with the combustion gas compressor. Furthermore, the gearing drive serves to drive a generator by means of a power take-off shaft. The gears of the gearing drive possess helical teeth. For thrust compensation purposes the drive gear of the gearing drive is provided with pressure plates, and the helical teeth of the gears are designed such that a force acting upon the pressure plates and resulting from the thrust of the combustion gas compressor is reduced by the axial component of the helical teeth.
Claims2
A gas turbine installation comprising:
- a gas turbine;
- a combustible gas compressor;
- a gearing drive containing gears;
- a coupling and an axial bearing for rotatably connecting the gearing drive with the gas turbine;
- a further coupling for rotatably connecting said gearing drive with the combustible gas compressor;
- a generator;
- a power take-off shaft for driving said generator by means of said gearing drive;
- said gears of said gearing drive containing helical teeth;
- said gears of said gearing drive including a drive gear;
- pressure plates provided for said drive gear of said gearing drive for thrust compensation;
- and
- the helical teeth of the gears of said gearing drive possessing helix angles selected such that a force acting upon the pressure plates and resulting from a thrust applied by the combustible gas compressor is reduced by axial components of the helical teeth.
Dependencies are inferred from the claim text.