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    • 1. 发明申请
    • METHOD AND A DEVICE FOR NORMALIZING VALUES OF OPERATING PARAMETERS OF AN AEROENGINE
    • 方法和装置,用于标准化运行参数的值
    • US20150268131A1
    • 2015-09-24
    • US14478286
    • 2014-09-05
    • SNECMA
    • Aurelie GOUBY
    • G01M15/14G07C3/02
    • G01M15/14G05B23/0221G07C3/02
    • The normalization method comprises: normalizing a current value of each operating parameter relative to exogenous variables with the help of a first regression model defined on a space generated by the exogenous variables; associating the vector formed by the normalized current values of the parameters with at least one vector class of a set of predefined classes; using at least one second regression model defined on the space generated by the exogenous variables for said at least one class associated with the vector to construct for each parameter a third regression model onto said space; and normalizing the normalized current value of each parameter relative to the exogenous variables with the help of the third regression model.
    • 归一化方法包括:借助于由外生变量产生的空间定义的第一回归模型,对相对于外生变量的每个操作参数的当前值进行归一化; 将由参数的归一化电流值形成的矢量与一组预定义类别的至少一个矢量类相关联; 使用至少一个第二回归模型,所述至少一个第二回归模型在由所述至少一个与所述向量相关联的类别的所述外部变量生成的空间上定义,以对每个参数构建所述空间上的第三回归模型 并借助于第三回归模型,使每个参数相对于外生变量的归一化电流值进行归一化。
    • 3. 发明申请
    • NON-REGRESSION METHOD OF A TOOL FOR DESIGNING A MONITORING SYSTEM OF AN AIRCRAFT ENGINE
    • 用于设计飞机发动机监控系统的工具的非回归方法
    • US20150120214A1
    • 2015-04-30
    • US14506901
    • 2014-10-06
    • SNECMA
    • Aurelie GOUBYJerome Henri Noel LACAILLE
    • G01M15/00
    • G01M15/00G06F11/277G06F11/3688
    • The invention relates to a system of non-regression tests of a designing tool including modules (13) used to build a monitoring device (11) of an aircraft engine (7), said system of tests including: processing means (9) configured to automatically create an experience base (9e) by instrumenting behaviour tests upon executing the modules, said experience base including reference input signals (SIN—ref), sets of reference parameters, reference output signals (SOUT—ref), and collections of results of reference executions relating to said modules, processing means (9) configured to start again said behaviour tests on said modules (13) depending on the corresponding reference input signals and the corresponding sets of reference parameters thus generating test output signals (SOUT—test) and collections of results of test executions, and processing means (9) configured to compare said test output signals with the corresponding reference output signals and said collections of results of test execution with said corresponding collections of results of reference executions in order to test the non-regression of the designing tool.
    • 本发明涉及一种包括用于构建飞机发动机(7)的监视装置(11)的模块(13)的设计工具的非回归测试系统,所述测试系统包括:处理装置(9),被配置为 通过在执行模块时进行行为测试来自动创建体验基础(9e),所述经验基础包括参考输入信号(SIN-ref),参考参数集合,参考输出信号(SOUT-ref)以及参考结果集合 与所述模块相关的执行,处理装置(9)被配置为根据相应的参考输入信号和相应的参考参数集再次启动所述模块(13)上的行为测试,从而产生测试输出信号(SOUT-测试)和集合 以及处理装置(9),其被配置为将所述测试输出信号与相应的参考输出信号和所述结果集合 测试执行与相应的参考执行结果的集合,以测试设计工具的不回归。