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    • 4. 发明专利
    • GAS TURBINE
    • JPH1073004A
    • 1998-03-17
    • JP22826196
    • 1996-08-29
    • TOSHIBA CORP
    • OTOMO FUMIOFUKUYAMA YOSHITAKANAKADA YUJISATO IWATAROOKAMURA TAKANARIFUKUDA MASAFUMIUTSUNOMIYA MASAHARUDOSONO GIICHI
    • F01D5/18F01D9/02F01D11/04F02C7/16
    • PROBLEM TO BE SOLVED: To improve cooling effect of a turbine blade by providing with a first cooling system of a flow passage structure formed in such a constitution that a cooling medium is injected from the surface part of the turbine blade to an outside after feeding to the cooling flow passage in the turbine blade, and a second cooling system of a flow passage structure for leading the cooling medium in a stationary blade. SOLUTION: In a device for respectively cooling each stationary blade 45 to 47 in a gas turbine by a stationary blade cooling system 51 and each moving blade 49, 50 by a moving blade cooling system 52, low pressure steam from a steam supplying system is fed to low pressure cooling flow passages 55 to 57 provided by dividing into three systems in the stationary blade 45 by a low pressure cooling system 53, and it is fed to low pressure cooling flow passages 58, 59 provided by dividing into two systems in the stationary blade 46, and its steam makes flow from a plurality of injection holes to a blade outside so as to film-cool a stationary blade surface. High pressure steam is fed in series with high pressure cooling fluid flows 81 to 83 arranged in each stationary blade by a high pressure cooling system 54, and then it is returned into a steam heating system 84.
    • 7. 发明专利
    • ICE HEAT ACCUMULATOR
    • JP2000121212A
    • 2000-04-28
    • JP29030398
    • 1998-10-13
    • TOSHIBA CORP
    • SHINGU HAJIMEUTSUNOMIYA MASAHARU
    • F24F5/00F25C1/00
    • PROBLEM TO BE SOLVED: To prevent a liquid drop from coming into direct collision against the separation interface between water and a cooling medium after a heat exchange by providing a separation interface with a part where multiple small spherical bodies having specific gravity between those of water and the cooling medium. SOLUTION: An ejection nozzle 3 is provided on the side wall of a heat storage tank 1 and an antifreeze solution 2 is ejected from the ejection nozzle 3 into the heat storage tank 1. Ice particles 7 are produced through the direct contact heat exchange of water 6 with the antifreeze solution 2 which is then taken out from an outlet 9 at the lower part of the heat storage tank, passed through a circulation pump 4 and cooled by a refrigerating machine 5 before returned to the heat storage tank 1. On the other hand, ice particles 7 are deposited above the heat storage tank 1. Small spherical bodies 8 having specific gravity between those of the water 6 and the antifreeze solution 2 are floated on the separation interface between the water 6 and the antifreeze solution 2 after the heat exchange and continuous operation is performed by circulating the antifreeze solution 2 while floating the small spherical bodies 8.
    • 8. 发明专利
    • GAS COMBINED POWER GENERATING FACILITY
    • JPH11294186A
    • 1999-10-26
    • JP9414798
    • 1998-04-07
    • ISHIKAWAJIMA HARIMA HEAVY INDTOSHIBA CORP
    • HASHIMOTO KEIICHIROKOYAKE YASUHIROFURUKAWA TOSHIKIUTSUNOMIYA MASAHARU
    • F01K23/10C10K1/08F02C3/28F02C9/00
    • PROBLEM TO BE SOLVED: To provide a gas combined power generating facilities capable of sufficiently raise the temperature of the refined gas coming out of gas refining equipment for supplying it to a gas-turbine combined power generating facilities, having no possibility of internal clogging and inflow of dust or the like into the gas turbine, and allowing the refining gas heating system to be compact. SOLUTION: Gas combined power generating facilities are provided with an indirect gas cooling/heating device 10 for cooling crude gas by a heating medium having a higher pressure than that of the crude gas and refined gas, and for heating the refined gas. The indirect gas cooling/heating device 10 is made of a crude gas cooler 12 arranged between a gasifying/cooking apparatus A and a gas refining apparatus B for cooling the crude gas and for heating the heating medium, a refined gas heater 14 arranged between the gas refining apparatus B and a gas-turbine combined power generating facilities C for heating the refined gas by the heated heating medium, and a medium circulating line 16 for circulating the heating medium between the crude gas cooler 12 and the refined gas heater 14. The heating medium is water and steam, and the pressure of the medium circulating line is set so that it is evaporated in the crude gas cooler 12 and is condensed in the refined gas heater 14.