Snecma

Alstom Transport Technologies

Benjamin Pierre Lamoureux

Aziz Sif

Jean-Remi Andre Masse

Xavier Flandrois

Christian Aurousseau

Guilhem Foiret

Francois Demaison

Jean-Rémi André Masse

Quentin Thevenet

Frédéric Setan

Laurent Vagner

Régis Michel Paul Deldalle

Hicham Janati Idrissi

Francis Marquisseau

A health status assessment method and system for a transport vehicle automatic or semi-automatic access device is disclosed. The health status assessment system has at least one leaf actuated by a kinematic chain including at least one motor having an associated angular position or rotation speed encoder and at least one switch. The health status assessment method includes steps for analyzing at least one actuating cycle of the kinematic chain between a first and a second position wherein, during one said cycle, information is acquired representative of the electrical energy consumed by the motor, or position or speed information provided by said encoder or binary information indicating positions of switches. The method further includes dividing said cycle into a plurality of functional segments based on said acquired information, calculating at least one descriptor value, and then establishing a health status diagnosis of the health status assessment system.

Diagnostic operation method and system for a transport vehicle automatic or semi-automatic access device

A method for monitoring an ignition sequence of an engine, in particular a turbomachine engine, including the following steps: (i) defining an ignition time of the engine for a defined starting parameter, (ii) comparing the ignition time of the engine defined in this way with a reference ignition time expected for a reference engine and for this starting parameter, (iii) deducing an indicator of the bringing into operation of the engine, (iv) repeating steps (i) to (iii) for this starting parameter, for each bringing into operation of the engine of the sequence, and (v) on the basis of the change in the indicator, generating a degradation alert for the ignition sequence of the engine.

Method for monitoring an ignition sequence of a turbomachine engine

A method monitoring a servo-control loop, including: estimating monitoring parameters from operating data of the servo-control loop; obtaining indicators from the monitoring parameters; determining at least one signature from values of at least some of the indicators; and detecting and locating a degradation affecting the servo-control loop as a function of the at least one determined signature.

Method and a device for monitoring a servo-control loop of an actuator system for actuating variable-geometry components of a turbojet

A method for monitoring a control device of a fuel metering valve of an aircraft turbojet engine, the control device supplying a control current to a servo valve in order to modify the position of the fuel metering valve. The method includes determining the position of the fuel metering valve during a flight of the aircraft, determining the travelling speed of the fuel metering valve, and determining the control current when the travelling speed of the fuel metering valve is zero. A mean control current is calculated when the travelling speed of the fuel metering valve is zero, the mean control current forming an indicator of deterioration of the control device. The deterioration indicator is compared with a reference base of indicators with deterioration so as to infer the type of deterioration from it, and an abnormality score is calculated for the deterioration indicator. The abnormality score is compared with a decision threshold of abnormality characteristic of the type of deterioration, and an alarm is released in case of violation of the decision threshold of abnormality.

Method for monitoring a control device of a fuel metering valve of a turbojet engine

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Moissy Cramayel, France

Benjamin Pierre Lamoureux