Method and a device for calculating a starting or stop sequence for an engine
View Patent ↗The method serves to calculate a start sequence or a stop sequence for an engine, said sequence comprising a plurality of cues at which predetermined actions should be performed in the control of said engine. The method comprises: a step of obtaining at least one thermodynamic condition of said engine; and a step of calculating said sequence as a function of: said at least one thermodynamic condition; dimensional parameters of said engine; and criteria for proper operation of said engine.
1. A calculation method for calculating a start sequence or a stop sequence for an engine, said start sequence or said stop sequence comprising a plurality of cues at which predetermined actions should be performed in the control of said engine, wherein the method comprises the steps of:
obtaining, by a computer associated with said engine, at least one thermodynamic condition of said engine; and
recalculating, by said computer after at least one start or stop of said engine, said start sequence or said stop sequence as a function of:
said at least one thermodynamic condition;
dimensional parameters of said engine; and
criteria for proper operation of said engine,
wherein said at least one thermodynamic condition of the engine that is taken into account for recalculating said start sequence by said computer includes:
the initial temperature of a regenerator circuit of said engine;
a coefficient representative of heating of said regenerator circuit; and
a coefficient representative of head loss of said regenerator circuit.
2. The calculation method according to claim 1 , wherein said at least one thermodynamic condition of the engine taken into account for recalculating said stop sequence by said computer includes:
a coefficient representative of heating of a regenerator circuit; and
a coefficient representative of head loss of said regenerator circuit.
3. The calculation method according to claim 1 , wherein said recalculating of said start sequence or said stop sequence comprises:
modeling, by said computer, a behavior of said engine using a predetermined system of regression equations, said model serving to express said criteria for proper operation as a function of said cues, of said dimensional parameters, and of said at least one thermodynamic condition; and
solving, by said computer, said predetermined system of regression equations by a method of least squares in order to obtain said cues.
4. A non-transitory computer-readable storage medium including computer-executable instructions for executing the steps of:
obtaining at least one thermodynamic condition of said engine; and
recalculating, after at least one start or stop of said engine, said start sequence or said stop sequence as a function of:
said at least one thermodynamic condition;
dimensional parameters of said engine; and
criteria for proper operation of said engine,
wherein said at least one thermodynamic condition of the engine that is taken into account for recalculating said start sequence includes:
the initial temperature of a regenerator circuit of said engine;
a coefficient representative of heating of said regenerator circuit; and
a coefficient representative of head loss of said regenerator circuit.
5. A calculation device for calculating a start sequence or a stop sequence for an engine, said start sequence or said stop sequence comprising a plurality of cues at which predetermined actions need to be taken in the control of said engine, wherein the device comprises:
a first computerized component for obtaining at least one thermodynamic condition of said engine; and
a second computerized component for recalculating, after at least one start or stop of said engine, said start sequence or said stop sequence as a function of:
said at least one thermodynamic condition;
dimensional parameters of said engine; and
criteria for proper operation of said engine,
wherein said at least one thermodynamic condition of the engine that is taken into account for recalculating said start sequence includes;
the initial temperature of a regenerator circuit of said engine;
a coefficient representative of heating of said regenerator circuit; and
a coefficient representative of head loss of said regenerator circuit.
6. The calculation device according to claim 5 , wherein said second computerized component for recalculating said start sequence or said stop sequence comprises:
a computerized prediction module suitable for predicting the proper operation critical as a function of the thermodynamic parameters and the dimensional parameters of the engine; and
a fuzzy logic system suitable for determining the cue vector as a function of the criteria determined by the computerized prediction module.
7. A rocket engine including calculation device for calculating a start sequence or a stop sequence for and engine, said start sequence or said stop sequence comprising a plurality of does at which predetermined actions need to be taken in the control of said engine, wherein the device comprises:
a first computerized component for obtaining at least one thermodynamic condition of said engine; and
a second computerized component for recalculating, after at least one start or stop of said engine, said start sequence or said stop sequence as a function of:
said at least one thermodynamic condition;
dimensional parameters of said engine; and
criteria for proper operation of said engine,
wherein said at least one thermodynamic condition of the engine that is taken into account for recalculating said start sequence includes:
the initial temperature of a regenerator circuit of said engine;
a coefficient representative of heating of said regenerator circuit; and
a coefficient representative of head loss of said regenerator circuit.