Gas turbine, exhaust diffuser, and method of modifying gas turbine plant
View Patent ↗A method of modifying a gas turbine plant which is provided with a one-shaft gas turbine having a compressor for compressing air, a combustor for generating a combustion gas from the air compressed by the compressor and a fuel, and a one-shaft turbine driven by the combustion gas generated by the combustor and supported by a rotational axis common to the compressor, and an electric generator for generating electric power by driving force of the one-shaft turbine, wherein: the one-shaft turbine is replaced with a two-shaft gas turbine including a compressor for compressing air, a combustor for generating a combustion gas from the air compressed by the compressor and a fuel, and a high-pressure turbine driven by the combustion gas generated by the combustor and supported by a first rotational axis common to the compressor, and a low-pressure turbine driven by the combustion gas used to drive the high-pressure turbine and supported by a second rotational axis, which is different from the axis for the high-pressure turbine.
1. A gas turbine which is provided with a compressor for compressing air, a combustor for generating a combustion gas from the air compressed by the compressor and a fuel, a turbine driven by the combustion gas generated by the combustor, an exhaust diffuser which is in a flow path of the combustion gas used to drive the turbine, the flow path being formed of an inner circumferential casing and an outer circumferential casing, an exhaust duct from which the combustion gas is externally expelled, an exhaust chamber in which the exhaust diffuser and the exhaust duct are mutually connected, a turn vane provided in the exhaust diffuser to change a combustion gas flow, a plurality of support members provided in a direction of the combustion gas flow and extending through the turn vane for supporting the turn vane, and a strut to support the outer circumferential casing connecting to the inner circumferential casing, wherein:
a vertical distance from a center of a rotational axis to a top of the exhaust chamber is longer than a vertical distance from the center of the rotational axis to a bottom of the exhaust chamber; and
the support members are shaped with circular cross sections, extend from the inner circumferential casing, and do not reach the surface of the outer circumferential casing so as to suppress interference on a fluid flow in a circumferential direction of the rotational axis.
2. A gas turbine which is provided with a compressor for compressing air, a combustor for generating a combustion gas from the air compressed by the compressor and a fuel, a turbine driven by the combustion gas generated by the combustor,
an exhaust diffuser which is in a flow path of the combustion gas used to drive the turbine, the flow path being formed of an inner circumferential casing and an outer circumferential casing, an exhaust duct from which the combustion gas is externally expelled, an exhaust chamber in which the exhaust diffuser and the exhaust duct are mutually connected, a turn vane provided in the exhaust diffuser to change a combustion gas flow, a plurality of support members provided in a direction of the combustion gas flow and extending through the turn vane for supporting the turn vane, and a strut to support the outer circumferential casing connecting to the inner circumferential casing, wherein:
a vertical distance from a center of a rotational axis to a top of the exhaust chamber is longer than a vertical distance from the center of the rotational axis to a bottom of the exhaust chamber;
the support members are shaped with circular cross sections, extend from the inner circumferential casing, and do not reach the surface of the outer circumferential casing so as to suppress interference on a fluid flow in the exhaust diffuser; and
the support members in the exhaust diffuser differ, in a circumferential direction, in shape, placement, or both shape and placement.
3. An exhaust diffuser which is provided with an inner circumferential casing to form an inner side of a flow path, an outer circumferential casing to form an outer side of the flow path, a strut to support the outer circumferential casing connecting to the inner circumferential casing, a turn vane for redirecting a fluid flow, and a plurality of support members provided in a direction of the combustion gas flow for supporting the turn vane, wherein:
the support members are shaped with circular cross sections, extend from the inner circumferential casing and through the turn vane, and do not reach the surface of the outer circumferential casing so as to suppress interference on the fluid flow in a width direction of the turn vane.