会员体验
专利管家(专利管理)
工作空间(专利管理)
风险监控(情报监控)
数据分析(专利分析)
侵权分析(诉讼无效)
联系我们
交流群
官方交流:
QQ群: 891211   
微信请扫码    >>>
现在联系顾问~
热词
    • 4. 发明专利
    • ANALYZING METHOD FOR GRADUALLY CHANGING TRANSPORTATION /DIFFUSION FIELD
    • JPS6451577A
    • 1989-02-27
    • JP20812487
    • 1987-08-24
    • HITACHI LTD
    • KATO CHIYUKIIKEGAWA MASAHIRO
    • G06F17/50G06F17/13G06F19/00
    • PURPOSE:To analyze a successively changing transportation/diffusion field by representing an analysis area as the aggregation of discrete points by a finite difference method or a finite volume method and obtaining the value of the quantity of a state after DELTAt time from a point going upstream by uDELTAt/2 (u is transportation vector) from the respective discrete points. CONSTITUTION:In the analysis of the unsteady temperature field of one of the transportation/diffusion fields, the analysis area is divided to proper grids intersecting orthogonally with each other. An area for storing the quantity phiof the status in the respective grid points (for instance, temperature), the quantity F of unbalance and flow velocities (u), (v), is maintained. The flow velocities ui,j, vi,j of the respective grid points are set. An initial temperature distribution Ti,j is set. The quantity of the unbalance of the quantity of the status is calculated and the temperature Ti,j of the respective grid points after DELTAt time from the calculated quantity of the unbalance is calculated. The numerical analysis of the unsteady temperature field can be attained by repeating such a calculation by the number of applied repetitions.
    • 9. 发明专利
    • NUMERICAL ANALYSIS METHOD
    • JPH06202750A
    • 1994-07-22
    • JP34794492
    • 1992-12-28
    • HITACHI LTD
    • WATANABE MASATOSHIIKEGAWA MASAHIRO
    • G01M9/00G06D5/00G06F17/10G06F15/31
    • PURPOSE:To shorten calculation time and to reduce a storage capacity by dividing the whole of an area into areas and reducing the dimensions to analyze the areas in the case of areas which can be approximated to lower dimensions. CONSTITUTION:With respect to formation of a compression wave due to, for example, plunge of a vehicle into a tunnel, its propagation, and analysis of its discharge to a tunnel exit shell, an area 31 is an entrance area until the vehicle plunges into a tunnel, and an area 32 in an area around the vehicle. The compression wave is generated when the vehicle included in the area 32 plunges into the tunnel. The compression wave is generated three-dimensionally; and when the vehicle velocity is smaller than the acoustic velocity, the compression wave proceeds in the tunnel more quickly than the vehicle because the compression wave proceeds forward at the acoustic velocity. Since the compression wave proceeding in the tunnel can be approximated as a one-dimensional phenomenon, a tunnel area 33 can be subjected to one-dimensional analysis. As the result, the storage capacity is made smaller and the calculation time is reduced in comparison with those for three-dimensional analysis of all of areas.
    • 10. 发明专利
    • NUMERICAL ANALYSIS METHOD FOR FLUID
    • JPH06195425A
    • 1994-07-15
    • JP34390592
    • 1992-12-24
    • HITACHI LTD
    • KATO CHIYUKIIKEGAWA MASAHIRO
    • G06F17/50G06F17/17G06F15/60G06F15/353
    • PURPOSE:To provide an accurate fluid analyzing method by providing a virtual flow passage which includes a virtual object such as a column and is attached a periodic condition at in/out-flow border and giving the outflow condition of the virtual flow passage as the inflow condition of an analytic flow passage. CONSTITUTION:An inflow turbulence intensity ko which is known by an experiment, etc., the shapes of the analytic flow-passage A and the virtual flow passage B (in which column is arranged) are set, the respective flow passages A and B are divided into differential meshes, a joint border C is set so as to set the outflow condition of the virtual flow passage B to be the inflow condition of the analytic flow passage A and the periodic condition is set at the in/out-flow border so as to grow turbulence in the virtual flow passage B. Then, a proper initial value to a parameter alpha is set so as to execute the flow calculation of the virtual flow passage B until convergence. Furthermore, when the value of the parameter alpha capable of realizing the necessary turbulence intensity ko is obtained, time (t) is set to be zero again so as to alternately execute the flow calculation of the virtual flow passage B and the analitic flow passage A until an objective time tend by a time step DELTAt.