Method and a device for managing risks and alerts

1. A method of managing risks and alerts for a system, the system being an aircraft and including:

a plurality of source modules for identifying actual or potential risks of failure or of malfunction of the system;

a plurality of auxiliary modules for identifying actual or potential risks that are related to parameters external to the system and that might have impacts on operation of the system;

a central module connected to the source modules and to the auxiliary modules, the central module including at least one computer and receiving information relating to the actual or potential risks of failure or of malfunction of the system;

at least one action and information interface for an operator of the system, the at least one action and information interface being connected to the central module;

a lift rotor;

an auxiliary rotor; and

at least one engine driving a mechanical power transmission gearbox driving the lift rotor and the auxiliary rotor in rotation;

the method comprising the following steps:

determining at least one actual or potential risk of failure or of malfunction of the system by means of at least one source module;

determining at least one actual or potential risk that is related to parameters external to the system and that might have an impact on operation of the system, by means of at least one auxiliary module;

determining an overall risk level by combining the actual or potential risks and their effects on the system by means of the central module; and

controlling the at least one action and information interface as a function of the overall risk level; and

wherein, with the at least one action and information interface including a control device for controlling the aircraft, controlling the at least one action and information interface includes an action substep performed by means of the control device, the action substep performs at least one action on the lift rotor, the auxiliary rotor, and the at least one engine or the mechanical power transmission gearbox, automatically by means of the control device as a function of the overall risk level.

2. The method according to claim 1 ,

wherein, with the at least one action and information interface further including a display device, controlling the at least one action and information interface further includes a display substep for displaying the overall risk level and/or information relating to the system and/or to its environment on the display device.

3. The method according to claim 1 ,

wherein, with the at least one action and information interface further including a warning device, controlling the at least one action and information interface further includes a warning substep alerting an operator of the system as a function of the overall risk level by means of the warning device.

4. The method according to claim 1 ,

wherein, with the at least one action and information interface further including a display device and a validation device, controlling the at least one action and information interface further includes a display substep for displaying, on the display device, one or more actions to be performed and a validation substep for validation by an operator of the system by means of the validation device, the operator validating at least one action proposed during the validation substep by means of the validation device, and each validated action being performed automatically by means of the control device as a function of the overall risk level.

5. The method according to claim 1 ,

wherein determining the overall risk level is performed while using a weighting associated with each actual or potential risk relating to the system or to its environment.

6. The method according to claim 1 ,

wherein determining at least one actual or potential risk of failure or of malfunction of the system comprises the following substeps:

measuring at least one characteristic of an element of the system, at least one characteristic of a device of the system, at least one characteristic of a subsystem of the system or at least one parameter of the system;

analyzing the at least one characteristic; and

computing at least one actual or potential risk of failure or of malfunction of the system, which risk is associated with the at least one characteristic.

7. The method according to claim 1 ,

wherein determining at least one actual or potential risk associated with parameters external to the system comprises the following substeps:

measuring at least one parameter external to the system;

analyzing the at least one parameter external to the system; and

computing at least one actual or potential risk associated with the at least one parameter external to the system.

8. The method according to claim 1 ,

wherein determining the overall risk level is performed by means of an expert system, of artificial intelligence, or of a neuronal system.

9. The method according to claim 1 ,

wherein the information relating to the actual or potential risks related to the parameters external to the system concern weather conditions, flight conditions, a terrain and relief of the terrain, a purpose of a mission flown by the aircraft and a path of the aircraft, and a state of a pilot of the aircraft.

10. The method according to claim 1 ,

wherein the information relating to the actual or potential risks of failures or of malfunctioning of the system relate to engine health monitoring, monitoring of the aircraft, and/or to performance of the aircraft.

11. The method according to claim 1 ,

wherein the method further comprises an additional computation step for computing an intermediate level of risk as a function of certain actual or potential risks relating to the system or to parameters external to the system, the intermediate level of risk being used by the central module and combined with the other actual or potential risks to determine the overall risk level of the system.

12. A device for managing risks and alerts for an aircraft having a lift rotor, an auxiliary rotor, and at least one engine driving a mechanical power transmission gearbox driving the lift rotor and the auxiliary rotor in rotation, the device comprising:

a plurality of source modules for identifying actual or potential risks of failure or of malfunction of the aircraft;

a plurality of auxiliary modules for identifying actual or potential risks that are related to parameters external to the aircraft and that might have impacts on operation of the aircraft;

a central module connected to the source modules and to the auxiliary modules, the central module including at least one computer and receiving information relating to the actual or potential risks of failure or of malfunction of the aircraft; and

at least one action and information interface for an operator of the aircraft, the at least one action and information interface is connected to the central module and includes a control device for controlling the aircraft;

wherein the central module is configured to determine an overall risk level by combining the actual or potential risks and their effects on the aircraft; and

the central module is further configured to control the at least one action and information interface as a function of the overall risk level such that at least one action on the lift rotor, the auxiliary rotor, and the at least one engine or the mechanical power transmission gearbox is taken automatically by the control device of the at least one action and information interface as a function of the overall risk level.

13. An aircraft comprising:

a lift rotor;

an auxiliary rotor;

at least one engine driving a mechanical power transmission gearbox driving the lift rotor and the auxiliary rotor in rotation; and

a device for managing risks and alerts for the aircraft, the device including

a plurality of source modules for identifying actual or potential risks of failure or of malfunction of the aircraft;

a plurality of auxiliary modules for identifying actual or potential risks that are related to parameters external to the aircraft and that might have impacts on operation of the aircraft;

a central module connected to the source modules and to the auxiliary modules, the central module including at least one computer and receiving information relating to the actual or potential risks of failure or of malfunction of the aircraft; and

at least one action and information interface for an operator of the aircraft, the at least one action and information interface is connected to the central module and includes a control device for controlling the aircraft;

wherein the central module is configured to determine an overall risk level by combining the actual or potential risks and their effects on the aircraft; and

the central module is further configured to control the at least one action and information interface as a function of the overall risk level such that at least one action on the lift rotor, the auxiliary rotor, and the at least one engine or the mechanical power transmission gearbox is taken automatically by the control device of the at least one action and information interface as a function of the overall risk level.

14. The device according to claim 12 ,

wherein the at least one action and information interface further includes a display device; and

the central module is further configured to control the at least one action and information interface such that the display device displays the overall risk level and/or information relating to the aircraft and/or to its environment.

15. The device according to claim 12 ,

wherein the at least one action and information interface further includes a warning device; and

the central module is further configured to control the at least one action and information interface such that the warning device alerts the operator of the aircraft as a function of the overall risk level.

16. The device according to claim 12 ,

wherein the at least one action and information interface further includes a display device and a validation device; and

the central module is further configured to control the at least one action and information interface such that the display device displays one or more actions for validation by the operator of the aircraft with each action validated by the operator of the aircraft via the validation device being performed automatically by the control device as a function of the overall risk level.

17. The device according to claim 12 ,

wherein the information relating to the actual or potential risks related to the parameters external to the aircraft concern weather conditions, flight conditions, a terrain and relief of the terrain, a purpose of a mission flown by the aircraft and a path of the aircraft, and a state of a pilot of the aircraft.

18. The device according to claim 12 ,

wherein the information relating to the actual or potential risks of failures or of malfunctioning of the aircraft relate to engine health monitoring, monitoring of the aircraft, and/or to performance of the aircraft.

19. The aircraft according to claim 13 ,

wherein the information relating to the actual or potential risks related to the parameters external to the aircraft concern weather conditions, flight conditions, a terrain and relief of the terrain, a purpose of a mission flown by the aircraft and a path of the aircraft, and a state of a pilot of the aircraft.

20. The aircraft according to claim 13 ,

wherein the information relating to the actual or potential risks of failures or of malfunctioning of the aircraft relate to engine health monitoring, monitoring of the aircraft, and/or to performance of the aircraft.