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Method for detection of ignition of mixture of propellants in combustion chamber of jet engine of rocket, involves determining ignition of mixture of propellants when reference variable has reached predetermined threshold
Method for detection of ignition of mixture of propellants in combustion chamber of jet engine of rocket, involves determining ignition of mixture of propellants when reference variable has reached predetermined threshold
The method involves forecasting a beginning (t all debut) of a temporal beach of ignition according to a set of initial conditions. A physical parameter (PRGC) is measured in a combustion chamber. A reference variable (PRGC f der) is calculated according to a signal corresponding to the physical parameter. Ignition of mixture of propellants is determined when the reference variable has reached a predetermined threshold after beginning of the temporal beach of ignition. Independent claims are also included for the following: (1) a system for detection of ignition of a mixture of propellants (2) a computer program comprising instructions for performing a method for detection of ignition of a mixture of propellants (3) a data storage medium comprising instructions for performing the method for detection of ignition of a mixture of propellants.
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机译：该方法涉及根据一组初始条件预测暂时的点火海滩的开始（全部初次亮相）。在燃烧室内测量物理参数（PRGC）。根据对应于物理参数的信号计算参考变量（PRGC f der）。当参考变量在暂时点火开始后达到预定阈值时，确定混合推进剂的点火。还包括以下方面的独立权利要求：（1）用于检测推进剂混合物着火的系统（2）计算机程序，包括用于执行检测用于推进剂混合物着火的方法的指令（3）数据存储该介质包括用于执行用于检测推进剂混合物着火的方法的指令。
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