초록 ▼

A gas turbine plant, wherein a plurality of first gas turbines positioned coaxially with compressors and a second gas turbine positioned coaxially with a generator are rotated by a coolant heated by heat energy provided by the fission of a coated particle fuel. A flow in a bypass passage is controll

A gas turbine plant, wherein a plurality of first gas turbines positioned coaxially with compressors and a second gas turbine positioned coaxially with a generator are rotated by a coolant heated by heat energy provided by the fission of a coated particle fuel. A flow in a bypass passage is controlled by controlling the opening of bypass valves of (n-1) in quantity which bypass the first gas turbines on up to (n-1) shafts in starting. Accordingly, the rotational speeds of the first gas turbines on up to (n) shafts are increased to a rated rotational speed in order starting at the initial stage on the upstream side of a high temperature gas-cooled reactor toward the lower stage for each shaft.

대표청구항 ▼

What is claimed is: 1. A gas turbine plant comprising: a high-temperature gas-cooled reactor which warms a coolant by thermal energy being obtained by nuclear fission of clad fission products in coated-particle fuels; a number "n" of first gas turbines in series that are rotated by the coolant bein

What is claimed is: 1. A gas turbine plant comprising: a high-temperature gas-cooled reactor which warms a coolant by thermal energy being obtained by nuclear fission of clad fission products in coated-particle fuels; a number "n" of first gas turbines in series that are rotated by the coolant being warmed by the high-temperature gas-cooled reactor and share same shafts with compressors compressing the coolant; a second gas turbine that is rotated by the coolant being discharged from the last of the "n" first gas turbines serving as a last stage after rotating each of the "n" first gas turbines and shares a same shaft with a generator performing electrical power generation operation; and a number "n-1" of bypass flow passages with bypass valves that bypass each of corresponding "n-1" first gas turbines to a position downstream of the corresponding first gas turbine, excluding the first gas turbine in a first stage being closest to the high-temperature gas-cooled reactor, among the "n" first gas turbines; wherein, during start-up, by controlling a lift of the "n-1" bypass valves, each of the "n" first gas turbines has rotating speed thereof increased up to a rated rotating speed shaft by shaft sequentially, starting from the first gas turbine in a first stage. 2. A gas turbine plant as described in claim 1: wherein at least one of the "n-1" bypass flow passages with bypass valves bypasses the corresponding first gas turbine to a position downstream of the second gas turbine. 3. A gas turbine plant comprising: a high-temperature gas-cooled reactor which warms a coolant by thermal energy being obtained by nuclear fission of clad fission products in coated-particle fuels; a high pressure gas turbine which is rotated by the coolant being warmed by the high-temperature gas-cooled reactor and shares a same shaft with a high pressure compressor compressing the coolant; a low pressure gas turbine which is rotated by the coolant being discharged from the high pressure gas turbine and shares a same shaft with a low pressure compressor compressing the coolant; a gas turbine for electrical power generation which is rotated by the coolant being discharged from the low pressure gas turbine and shares a same shaft with a generator performing an electrical power generation; and a bypass flow passage with a bypass valve that bypasses the low pressure gas turbine to a position downstream of the low pressure gas turbine; wherein, during start-up, first, a rotating speed of the high pressure compressor is increased up to a rated rotating speed by adjusting a lift of the bypass valve after charging the coolant with the bypass valve fully closed, and then next, with the bypass valve fully closed, a rotating speed of the low pressure compressor is increased up to a rated rotating speed. 4. A gas turbine plant as described in claim 3: wherein the bypass flow passage with the bypass valve bypasses the low pressure gas turbine to a position downstream of the gas turbine for electrical power generation.