Patent GB-1228617-A (GB)
IPC: G21D3/12
Filed: 1968-07-29
Abstract: 1,228,617. Gas turbine plant-closed cycle type. SULZER BROS Ltd. July 29, 1968 [July 27, 1967], No.36074/68. Heading F1G. [Also in Division G6] The invention relates to a gas turbine and nuclear reactor plant comprising a circuit for a working fluid which is heated in the nuclear reactor, the circuit comprising two compression stages with interstage cooling, two turbine expansion stages with interstage reheat, the low-pressure turbine supplying power to an external load, and the nuclear reactor supplying heat for the interstage reheat. An adjustable throttle is provided immediately downstream of the low-pressure turbine, also a by-pass line by-passing the low-pressure turbine and the throttle and having a flow control member controllable by a delay means. The plant shown comprises an LP compressor 1 mounted on a shaft 16 and driven by an LP turbine 9 which also drives an external load in the form of an electric generator 15, an IP compressor 3, an HP compressor 5 and a working fluid pump 13 all mounted on a shaft 17 and driven by an HP turbine 7, and a nuclear reactor 8. The working fluid is C0 2 . C0 2  is compressed in compressor 1, cooled in interstage cooler 2 and further compressed in IP compressor 3. The CO 2  then divides into two streams, one stream passing directly to the HP compressor 5 and then to point 28; the other stream passes to a first cooler 11, a second cooler 12 where it is liquefied, the liquid C0 2  then passing to the pump 13 where its pressure is increased to critical pressure, the fluid then passing to a heat exchanger 14 where it is heated by CO 2  discharging from the LP turbine 9. The heated C0 2  then passes to the point 28 where it rejoins the first stream. The combined stream then passes to heat exchanger 6 where it is heated by C0 2  discharging from the LP turbine 9, the heated C0 2  then passing to the HP turbine 7, then through the nuclear reactor 8 where it is reheated, then through the LP turbine 9 finally discharging through the head exchangers 6 and 14, through a pre-cooler 10 back to the LP compressor 1. A throttle valve 60 is provided at the outlet of the LP turbine 9 and a by-pass line 61 containing a valve 62 is provided across the LP turbine and throttle valve 60, the valve 60 being controlled by a device 65 in response to speed of the LP shaft 16; the valve 62 is also responsive to the device 65 but through a time delay device 66. A further by-pass line 32 is provided between the outlet of the HP compressor 5 and the inlet of the LP turbine 9, the by-pass line containing a valve 33 controlled in dependence on speed of the HP shaft 17 as sensed by the device 37. Opening of the valve 33 would allow the working fluid to by-pass the HP turbine and the reactor. A further line 38 containing a valve 39 is provided between the liquefied C0 2  line downstream of the cooler 12 and the line downstream of the reactor, the valve 39 being controlled in dependence on pressure of the working fluid upstream of the reactor as sensed by the device 46. In place of the device 65 responsive to speed of the LP shaft, a device responsive to acceleration or a device responsive to the load on the generator may be provided. The closure of the valve 60 causes the pressure drop across the turbine 9 to be reduced considerably and the LP shaft is thus prevented from racing.