Monitoring of an aircraft propulsion system

1. A method for monitoring the propulsion system of an aircraft, comprising:

selecting hardware elements contributing to operation of the propulsion system;

modeling the propulsion system by a model comprising the selected hardware elements, a set of exogenic parameters of the propulsion system, and interdependence relations between the hardware elements, operation of a given hardware element being modelled by at least one endogenic parameter dependent on at least one of the exogenic parameters and/or on at least one parameter of another hardware element;

analyzing hardware elements based on the modelling, the analysis of a given hardware element including an expression of the at least one endogenic parameter of the given element as a function of only exogenic parameters of the propulsion system and being performed using different layers, at least one layer for a given hardware element being capable of taking into account at least one endogenic or exogenic parameter that is a result from a layer of a different hardware element, when available; and

outputting an alert to a pilot and/or a ground station based on the analyzing,

wherein the function of only exogenic parameters of the propulsion system corresponding to the expression of the at least one endogenic parameter of the given hardware element is generated based on a statistical regression of learning data, and

wherein the analyzing further includes obtaining data from the selected hardware elements contributing to operation of the propulsion system from an aircraft parameter acquisition system.

2. The monitoring method according to claim 1 , wherein the analyzing further comprises analyzing hardware elements, the analysis of the given hardware element including the expression of the at least one endogenic parameter of the given hardware element as the function of only exogenic parameters of the propulsion system and being performed using different layers, the layers including a data acquisition layer, a data normalisation layer and an abnormal event detection layer.

3. The monitoring method according to claim 2 , wherein the analysis of the given element also comprises a diagnostic on the element.

4. The monitoring method according to claim 3 , wherein the analysis of the given element also comprises a prognostic on the element.

5. The monitoring method according to claim 1 , wherein the analysis comprises an initialization during which the propulsion system is considered as a whole, the initialization including an analysis of the propulsion system considered as a whole, as a function of exogenic parameters, to determine at least one endogenic parameter of each element of the propulsion system.

6. A system for monitoring the propulsion system of an aircraft comprising:

means for selecting hardware elements contributing to operation of the propulsion system;

means for modelling the propulsion system by a model comprising the selected hardware elements, a set of exogenic parameters of the propulsion system, and interdependence relations between hardware elements, operation of a given hardware element being modelled by at least one endogenic parameter dependent on at least one of the exogenic parameters and/or at least one parameter of another element;

means for analysing hardware elements based on the modelling, the analysis of the given hardware element including an expression of the at least one endogenic parameter of the given element as a function of only exogenic parameters of the propulsion system and being performed using different layers, at least one layer for a given hardware element being able to take into account at least one endogenic or exogenic parameter that is a result from a layer of a different hardware element, when available; and

means for outputting an alert to a pilot and/or a ground station based on the analyzing,

wherein the function of only exogenic parameters of the propulsion system corresponding to the expression of the at least one endogenic parameter of the given hardware element is generated based on a statistical regression of learning data, and

wherein the means for analyzing further includes means for obtaining the selected elements representative of operation of the propulsion system from an aircraft parameter acquisition system.

7. A system for monitoring the propulsion system of an aircraft comprising:

memory storing instructions; and

processing circuitry configured, based on the stored instructions, to

select hardware elements contributing to operation of the propulsion system,

model the propulsion system by a model comprising the selected hardware elements, a set of exogenic parameters of the propulsion system, and interdependence relations between hardware elements, operation of a given hardware element being modelled by at least one endogenic parameter dependent on at least one of the exogenic parameters and/or at least one parameter of another element,

analyze hardware elements based on the modelling, the analysis of the given hardware element including an expression of the at least one endogenic parameter of the given element as a function of only exogenic parameters of the propulsion system and being performed using different layers, at least one layer for a given hardware element being able to take into account at least one endogenic exogenic parameter that is a result from a layer of another element, when available, and

output an alert to a pilot and/or a ground station based on the analyzing,

wherein the function of only exogenic parameters of the propulsion system corresponding to the expression of the at least one endogenic parameter of the given hardware element is generated based on a statistical regression of learning data, and

wherein the circuitry is further configured to analyze hardware elements based on the modelling by selecting elements representative of operation of the propulsion system from an aircraft parameter acquisition system.