Method and computer program for the monitoring of a thrust reverser having hydraulic actuators

Patent metadata

Field	Value
Publication number	US-10147245-B2
Application number	US-201415109714-A
Country	US
Kind code	B2
Filing date	Dec 24, 2014
Priority date	Jan 8, 2014
Publication date	Dec 4, 2018
Grant date	Dec 4, 2018

Abstract

A method for monitoring an aircraft thrust reverser having stowable doors, the thrust reverser being a reverser having hydraulic actuators equipped with switches arranged to each return a data item on the position of the doors, the engine including a computer configured to make measurements of a representative parameter of the position of the switches based on the data returned by the switches, includes computation of one or a plurality of statistical indicators of the parameter measured and an analysis of the temporal progression of the statistical indicator(s) computed. The invention also applies to a computer program for the implementation of this method.

First claim

The invention claimed is:

1. A method for monitoring a thrust reverser of an aircraft engine, the thrust reverser having stowable doors and hydraulic actuators and being equipped with switches arranged to each return a data item on a position of the doors, the method comprising:
measuring a representative parameter of a position of the switches based on the data items returned by the switches, wherein the measured representative parameter is a voltage ratio between a voltage divided by a voltage divider circuit and a power supply voltage of the voltage divider circuit, the voltage divider circuit comprising an output resistor in series with modules interconnected in parallel, each module comprising one of said switches connected in series with a first or a second module resistor based on the position of said switch;
computing a statistical indicator of the measured representative parameter; and
analyzing a temporal progression of the computed statistical indicator.

2. The method according to claim 1 , wherein the computing the statistical indicator of the measured representative parameter comprises determining at least one of a mean, a median, a standard deviation, and a distribution type of the measured representative parameter.

3. The method according to claim 1 , wherein the analyzing the temporal progression of the computed statistical indicator comprises computing a slope of the computed statistical indicator over a time window.

4. The method according to claim 1 , wherein the analyzing the temporal progression of the computed statistical indicator comprises comparing the computed statistical indicator with a reference indicator previously computed based on measurements of the representative parameter made during sound operation of the thrust reverser.

5. The method according to claim 1 , further comprising
comparing a result of the analyzing the temporal progression of the computed statistical indicator to a threshold, and
issuing a fault detection alert in an event of overshoot of the threshold.

6. The method according to claim 5 , further comprising, in the event of overshoot of the threshold, computing a detected fault signature based on the computed statistical indicator, and comparing the detected fault signature to one or a plurality of reference signatures each characteristic of a type of failure.

7. The method according to claim 1 , further comprising computing, based on a result of the analyzing the temporal progression of the computed statistical indicator, a probability of occurrence of a fault.

8. A computer program product comprising code instructions for executing the steps of the method according to claim 1 , when said program is executed on a computer.

9. The method according to claim 1 , wherein the measuring the representative parameter of the position of the switches is made during at least one operating phase of the thrust reverser including a transient opening phase, a stabilized opening phase, a transient closing phase, and a stabilized closing phase.

Assignees

• Safran Aircraft Engines

Inventors

• Coupard Josselin
• Tran Hang-Mi

Classifications

• G05B23/0283

  Predictive maintenance, e.g. involving the monitoring of a system and, based on the monitoring results, taking decisions on the maintenance schedule of the monitored system; Estimating remaining useful life [RUL] (preventive maintenance, i.e. planning maintenance according to the available resources without monitoring the system G06Q10/06) · CPC title

• F05D2270/821

  Displacement measuring means, e.g. inductive · CPC title

• B64D2045/0085

  Devices for aircraft health monitoring, e.g. monitoring flutter or vibration · CPC title

• G05B2219/32191

  Real time statistical process monitoring · CPC title

• B64D45/00

  Aircraft indicators or protectors not otherwise provided for · CPC title