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    • 11. 发明专利
    • STEAM TURBINE CASING FOR QUICK COOLING
    • JPH04325702A
    • 1992-11-16
    • JP9560791
    • 1991-04-25
    • TOSHIBA CORP
    • ISHII BUNJI
    • F01D25/12F01D25/24F01D25/28
    • PURPOSE:To quickly cool a steam turbine casing by covering the horizontal joint portion of the steam turbine casing with a case for cooling, and supplying cooling air to the case for cooling when required. CONSTITUTION:A steam turbine casing is constituted of 2 half casings of an upper half portion and a lower half portion, and each half casing is integrally constituted of a body portion 1 and a horizontal joint portion 2. Many fins 3 are provided on the horizontal joint portion 2 for widening a heat conduction area, and a thermocouple for detecting temperature is provided on the inner portion and the outer surface of the horizontal joint portion 2. Next, the horizontal joint portion 2 is covered with a case for cooling 4, and a passage portion 10 for flowing cooling air is provided between the case for cooling 4 and the horizontal joint portion 2. A cooling air supplying tube is connected on the upper side of the case for cooling 4, and air is supplied through a cooling air supply valve controlled by the signal of the thermocouple while discharged from a discharge tube on the lower side of the case 4 to the outside.
    • 12. 发明专利
    • METHOD OF TAKING REPLICA OF METAL DEFECT
    • JPH01280236A
    • 1989-11-10
    • JP10769388
    • 1988-05-02
    • TOSHIBA CORP
    • ISHII BUNJISUGAYA MASAYOSHI
    • G01N1/28
    • PURPOSE:To enable taking by using a transfer agent having a high electrical conductivity with a fewer number of production stages by coating a release agent onto the surface of a material to be inspected which is etched by an etching liquid after polishing, then coating the specific transfer agent thereon. CONSTITUTION:The release agent 3 is coated on the surface of the material 2 to be inspected which is etched by the etching liquid after polishing and thereafter, the transfer agent 1 consisting of 50-70wt.% C and 50-30wt.% epoxy resin is coated thereon. Voids 11 and carbides 12 are deposited by the creep damages formed on the material and extremely slight defect flaws 13 are distinctly exposed when the surface of the material 2 is etched. The transfer agent 1 coated on the surface is easily stopped if the release agent 3 is previously coated on the material 2 subjected to such surface treatment. The metal defects are distinctly microscopically examined by the X-rays, reflected electrons and secondary electron rays emitted from the transfer agent 1 if the transfer agent 1 is inspected by an electron microscope.
    • 15. 发明专利
    • METHOD FOR MONITORING LIFE OF HIGH TEMPERATURE STRUCTURAL PART
    • JPH03140841A
    • 1991-06-14
    • JP27926789
    • 1989-10-26
    • TOSHIBA CORP
    • ISHII BUNJI
    • G01N25/00G01N17/00G01N19/00
    • PURPOSE:To easily and accurately monitor the creep consumption life of a high temp. structural part by measuring the creep strain of the measuring place of the high temp. structural part by a capacity type strain gauge. CONSTITUTION:The creep strain of the predetermined place of a high temp. structural part is measured by a capacity type strain gauge 2 in a measured strain operation apparatus 9 and the temp. of the measuring place is measured by a thermocouple 3 and real creep strain is calculated from the measured creep strain and temp. by a real creep strain operation apparatus 11. Next, the change of the real creep strain with the elapse of time and the change rate of creep strain velocity are calculated by a creep measuring apparatus 12 and, from these results, a creep state is judged. Subsequently, creep like consumption quantity is calculated by a creep damage operation apparatus 13 and a creep breaking/ductility ratio is calculated by a creep breaking/ductility ratio calculation apparatus 14 and a creep strain curve is subsequently monitored by a diagnostic apparatus 15 and the elapse of the creep damage of the structural part is also monitored on the basis of cumulated creep life consumption quantity thereby. By this method, the creep consumption life of the high temp. structural part can be accurately monitored.
    • 16. 发明专利
    • MATERIAL TESTING DEVICE
    • JPS62130337A
    • 1987-06-12
    • JP27060485
    • 1985-12-03
    • TOSHIBA CORP
    • ISHII BUNJISUGAYA MASAYOSHI
    • G01N3/08G01N3/18
    • PURPOSE:To apply uniform pressure to a test piece by enabling the pressure receiving parts and pressure chamber of the test piece to function as a piston and a cylinder respectively and feeding and discharging fluid to and from the space in the pressure chamber partitioned by the pressure receiving parts of the test piece. CONSTITUTION:The round test piece 1 equipped with the discoid pressure receiving parts 1a at both end parts penetrates a casing 2 and is so extended that the pressure receiving parts 1a slide on the side wall of the pressure chamber 3 formed in the casing 2. When a tension load is placed on the test piece 1, a pressure regulating device 7 is put in operation to admit working oil from feed/discharge pipes 6a and 6b and fill spaces A and B partitioned with the pressure receiving parts 1a with the working oil, and the hydraulic pressure of the working oil supplied to the pipe 6b is increased gradually to raise the internal pressure in the space B and push the pressure receiving parts 1a outward, so that tensile stress operates on the test piece 1. When a compression load is placed on the test piece 1, on the other hand, the pressure of the working oil supplied to the pipe 6a is increased to raise the internal pressure in the space A, and compressive stress operates on the pressure receiving part 1b of the test piece 1, so that the test piece 1 is given the uniform stress.
    • 17. 发明专利
    • APPARATUS FOR MEASURING POLARIZATION
    • JPS61256250A
    • 1986-11-13
    • JP9675785
    • 1985-05-09
    • TOSHIBA CORP
    • ISHII BUNJISAITO KIYOSHIFUKUDA KIYOSHI
    • G01N27/26G01N17/00
    • PURPOSE:To measure polarization with high accuracy, in the measurement of the polarization of the change with time of a device such as a turbine rotor, by constituting an electrolytic cell having the member as a bottom surface and providing a heater to the surface of the member to hold the temp. difference between the surface of the member and an electrolyte. CONSTITUTION:An electrolytic cell 5 having the surface of a member 2 such as a turbine casing closely adhered thereto as the bottom surface thereof is formed to the surface of the member. An electrolyte 4 is received in said electrolytic cell 5 and the member 2, a collimation electrode 8 and an opposed electrode 11 are connected to a potentiostat 13 to measure polarization. A heater 20 is provided to the outer periphery, with which the electrolytic cell 5 is contacted, of the member 2 to heat said cell 5 and the surface temp. of the member 2 and that of the electrolyte are detected by thermocouples 22, 23 and the temp. difference between the surface temp. of the member 2 and the temp. of the electrolyte is constantly controlled. The electrolyte is convected by said temp. difference and an eluted metal ion is rapidly diffused and the stagnation of the reaction product on the surface of the member 2 being a measuring object is eliminated. Because the heater is provided, the measurement of polarization is stably performed and the effect of environmental temp. is eliminated and a measuring time can be shortened.
    • 18. 发明专利
    • Apparatus for measuring stress magnifying coefficient for structural member
    • 用于结构构件测量应力放大系数的装置
    • JPS61107135A
    • 1986-05-26
    • JP22835284
    • 1984-10-30
    • Toshiba Corp
    • ISHII BUNJI
    • G01N3/00
    • G01N3/00G01N2203/0062
    • PURPOSE:To make it possible to easily and rapidly measure the stress magnifying coefficient of a crack, by calculating the stress magnifying coefficient of the surface crack contained in a structural member by using the max. shearing stress calculated by a magnetizing type stress measuring device and the coordinates at the leading end of the crack and a measuring point. CONSTITUTION:The detection signal from a magnetizing type stress measuring probe 16 is applied to a magnetizing type stress difference (sigma1-sigma2) is measured. This output voltage is applied to a stress magnifying coefficient operator 19 through an interface 18. Two polar coordinates at measuring positions, where the material indication and leasing end of the crack of an article to be measured are sets as origins, are inputted and these values are applied to the operation 19 through an interface 21. The operator 19 analyzes the non-linear equation of the mixed mode of max. shearing stress and stress magnifying coefficients K1, KII on the basis of these input data according to a method of least squares and the values KI, KII obtained as the result of analysis are displayed on a display apparatus 22.
    • 目的:通过使用最大值来计算结构构件中包含的表面裂纹的应力放大系数,可以容易且快速地测量裂纹的应力放大系数。 通过磁化型应力测量装置计算的剪切应力和裂纹前端的坐标以及测量点。 结构:测量来自磁化型应力测量探头16的检测信号被应用于磁化型应力差(σ1-sigma2)。 该输出电压通过接口18施加到应力放大系数运算器19.输入要测量的物品的裂纹的材料指示和租赁结束作为起点的测量位置处的两个极坐标,并且这些值 通过接口21应用于操作19.操作者19分析最大混合模式的非线性方程式。 根据这些输入数据,根据最小二乘法和作为分析结果获得的值KI,KII,剪切应力和应力放大系数K1,KII被显示在显示装置22上。
    • 19. 发明专利
    • METHOD FOR DIAGNOSING SERVICE LIFE OF STRUCTURAL MEMBER USED UNDER HIGH TEMPERATURE
    • JPH06213791A
    • 1994-08-05
    • JP452993
    • 1993-01-14
    • TOSHIBA CORP
    • ISHII BUNJI
    • G01N3/32G01N3/60G01N33/20
    • PURPOSE:To diagnose the service life of a structural member by operating the member having a flat protrusion at the tip for a predetermined time under high temperature and then measuring the hardness thereof at various points thereby measuring the variation of hardness due to thermal deterioration at a point where the service life is evauated with no effect of stress. CONSTITUTION:Since a turbine rotor 1 rotates at high speed under high temperature, the corner part 7 at the root of the wheel 2 of the rotor 1 is subjected to nonsteady thermal stress due to centrifugal stress and start/stop operation of turbine. When the turbine is operated for a long term under that state, high temperature thermal deterioration takes place to cause creep fatigue through repetition of the operation. The corner part 7 is set as a service life diagnostic part 7 and a protrusion 6 is provided closely thereto on the side face of the wheel 2. The protrusion 6 is in same temperature state as the diagnostic part 7. The flat part at the tip of the protrusion 6 is in low stress state and the hardness can be measured thereat. The measurements are employed in the determination of low cycle fatigue characteristics and creep rapture characteristics thus diagnosing the service life.
    • 20. 发明专利
    • DAMAGE DIAGNOSTIC METHOD FOR GAS TURBINE HIGH-TEMPERATURE COMPONENT
    • JPH0425745A
    • 1992-01-29
    • JP13031790
    • 1990-05-22
    • TOSHIBA CORP
    • ISHII BUNJI
    • G01N3/32G01M13/02G01M99/00G01N3/00G01N33/20
    • PURPOSE:To evaluate creep damage and low-cycle fatigue damage with high accuracy and to evaluate the life expectancy by sampling a replica without destruction, performing the image processing of a gamma' phase, and calculating material characteristics efficiently with high accuracy, and using them. CONSTITUTION:An operation condition and component shape setter 1 sets border conditions for temperature and stress calculation and the nonstationary and stationary temperatures and stress of the component are calculated 2. A gamma' shape parameters is calculated 4 from an electron microscope photograph sampled by a metal structure sampler 3 and both low-cycle fatigue and creep breakage characteristics are calculated 5 by using the parameter, temperatures, and stress; and the stationary operation time and start/stop frequency of the component are set by an operation history setter 6 and both accumulation damage data on the low-cycle fatigue and creep are calculated 7 according to data on 12. Further, life expectancy arithmetic 9 is carried out by the setting 8 of the subsequent stationary operation time and start/stop frequency of the component and accumulation damage calculation 7, the diagnosis result based upon the both is displayed 10, and when the life almost ends, an alarm is generated. Consequently, a quantitative life expectancy diagnosis is taken in consideration of future operation configurations.