公开(公告)号：US20130282307A1

公开(公告)日：2013-10-24

申请号：US13806597

申请日：2010-06-22

申请人： Omar Mohamed El Shamy ,  Nidal Awni Ghizawi ,  Denis Guillaume Jean Guenard ,  Vittorio Michelassi ,  Sivasubramaniyan Sankaran ,  Clary Susanne Ingeborg Svendotter

发明人： Omar Mohamed El Shamy ,  Nidal Awni Ghizawi ,  Denis Guillaume Jean Guenard ,  Vittorio Michelassi ,  Sivasubramaniyan Sankaran ,  Clary Susanne Ingeborg Svendotter

IPC分类号： G06F17/50

CPC分类号： G06F17/5086 ,  G06F17/5009 ,  G06F2217/16

摘要： System and method for automatically determining a final set of tuning/calibration parameters for designing a new turbo-machinery. The method includes inputing an initial set of tuning/calibration parameters; calculating family turbo-machinery quantities based on the initial set of tuning/calibration parameters; comparing the calculated family turbo-machinery quantities with measured quantities and calculating a first error between the calculated family quantities and the measured quantities; calculating a second error between the initial set of tuning/calibration parameters and default values of the turbo-machine variables; forming a modified objective function that includes both the first and second errors; during an iterative process, varying the initial set of tuning/calibration parameters in such a way that the final set of tuning/calibration parameters is found; and storing in a database the final set of tuning/calibration parameters for the family.

摘要翻译： 用于自动确定用于设计新的涡轮机械的最后一组调谐/校准参数的系统和方法。 该方法包括输入初始的调谐/校准参数集合; 根据初始设置的调谐/校准参数计算家庭涡轮机械数量; 将计算的家庭涡轮机械量与测量的数量进行比较，并计算所计算的家庭数量与测量数量之间的第一误差; 计算初始设置的调谐/校准参数和涡轮机变量的默认值之间的第二个误差; 形成包括第一误差和第二误差的修正目标函数; 在迭代过程中，以调整/校准参数的最终集合的方式改变初始调谐/校准参数集合; 并在数据库中存储家庭的最终调谐/校准参数。