Mechanical assembly provided with means for monitoring for a structural anomaly, a gearbox provided with such a mechanical assembly, and a method of monitoring for a structural anomaly

1. A mechanical assembly provided with a sun gear together with a plurality of planet gears cooperable with said sun gear, the mechanical assembly having a planet carrier carrying each planet gear, each planet gear comprising a toothed body and rolling connection means interposed between a bottom portion of a pin of the planet gear and said body, each pin having a projecting top portion secured to said planet carrier, each body being movable in rotation firstly about its own first axis of rotation and secondly about a second axis of rotation of the planet carrier, said mechanical assembly including an outer annulus having an inner periphery that co-operates with each planet gear, each planet gear being movable in an annular space situated between said inner periphery and said sun gear, each planet gear including a vibration sensor forming part of monitoring means for monitoring for a structural anomaly, said monitoring means being provided with a control member configured to communicate with each vibration sensor in order to receive a measurement signal from each vibration sensor in order to enable anomaly monitoring to be performed, wherein said monitoring means includes at least one antenna placed on an outer periphery of said annulus, said control member being configured to communicate with at least one of the vibration sensors via said at least one antenna;

wherein said monitoring means is configured to, after acquiring a measurement signal, verify integrity of the signal in order to validate it, and wherein said monitoring means is further configured to eliminate each measurement signal of non-validated integrity.

2. The mechanical assembly according to claim 1 , wherein one of the vibration sensors is arranged inside the pin of one of the planet gears.

3. The mechanical assembly according to claim 2 , wherein the one vibration sensor is arranged inside the bottom portion of said pin.

4. The mechanical assembly according to claim 1 , wherein the rolling connection means of a given planet gear of the plurality of planet gears are contained in a rolling plane, and the vibration sensor of said given planet gear is arranged in a monitoring plane overlying said rolling plane.

5. The mechanical assembly according to claim 1 , wherein said vibration sensor of a given planet gear of the plurality of planet gears takes measurements in a measurement plane parallel to a rolling plane of said given planet gear.

6. The mechanical assembly according to claim 1 , wherein the vibration sensors are placed in a common monitoring plane.

7. The mechanical assembly according to claim 1 , wherein said monitoring means include a storage memory.

8. The mechanical assembly according to claim 1 , wherein said monitoring means include alarm means.

9. A rotorcraft gearbox, including the mechanical assembly according to claim 1 .

10. A method of monitoring a mechanical assembly for an anomaly, wherein the mechanical assembly includes a sun gear, a plurality of planet gears that are cooperable with the sun gear, and a planet carrier carrying each planet gear, each planet gear comprising a toothed body and rolling connection means interposed between a bottom portion of a pin of the planet gear and the body, each pin having a projecting top portion secured to the planet carrier, each body being movable in rotation firstly about its own first axis of rotation and secondly about a second axis of rotation of the planet carrier, and wherein the mechanical assembly further includes an outer annulus having an inner periphery that co-operates with each planet gear, each planet gear being movable in an annular space situated between the inner periphery and the sun gear, each planet gear including a vibration sensor forming part of monitoring means for monitoring for a structural anomaly, the monitoring means being provided with a control member configured to communicate with each vibration sensor in order to receive a measurement signal from each vibration sensor in order to enable anomaly monitoring to be performed, wherein the monitoring means further includes at least one antenna placed on an outer periphery of the annulus, the control member being configured to communicate with at least one of the vibration sensors via the at least one antenna, the method comprising:

acquiring one measurement signal per vibration sensor arranged in each respective planet gear;

generating one vibratory signature per acquired measurement signal;

comparing the vibratory signature coming from each vibration sensor with the vibratory signatures coming from other vibration sensors; and

observing that the anomaly is present in a given planet gear of the plurality of planet gears if the vibratory signature from the vibration sensor of said given planet gear differs from the vibratory signatures coming from other vibration sensors;

wherein after acquiring a measurement signal, integrity of the signal is verified in order to validate it, with each measurement signal of non-validated integrity being eliminated.

11. The method according to claim 10 , wherein the mechanical assembly has at least three vibration sensors, and the presence of the anomaly in a member connected to all of the planet gears is observed if the vibratory signatures coming from the vibration sensors differ from one another.

12. The method according to claim 10 , wherein the measurement signals are acquired using vibration sensors either simultaneously or else sequentially, and said measurement signals are transmitted to the control member in sequential manner prior to generating vibratory signatures.

13. A method of monitoring a mechanical assembly for an anomaly, wherein the assembly includes a sun gear, a plurality of planet gears that are cooperable with the sun gear and that are each provided with a vibration sensor, and a planet carrier carrying each planet gear, the method comprising:

acquiring a measurement signal per vibration sensor;

generating a vibratory signature per acquired measurement signal;

comparing the vibratory signature associated with each vibration sensor with the vibratory signatures associated with other vibration sensors; and

observing that an anomaly is present in a given planet gear of the plurality of planet gears if the vibratory signature associated with the vibration sensor of the given planet gear differs from the vibratory signatures associated with other vibration sensors;

wherein after acquiring a measurement signal, integrity of the signal is verified in order to validate it, with each measurement signal of non-validated integrity being eliminated.