摘要:
The invention relates to a method for monitoring an LVDT sensor comprising two secondary circuits, characterised in that it comprises the iterative steps of: calculating (E1) the difference between the voltages at the terminals of one of the secondary circuits at a given moment and at a preceding moment; calculating (E1) the difference between the voltages at the terminals of the other secondary circuit at the given moment and at the preceding moment; calculating (E2) the sum of two calculated differences; modifying (E3) an indicator in accordance with the distance from zero of the previously calculated sum; and comparing (E4) the indicator with at least one predetermined threshold.
摘要:
The method for resetting a basic digital model (5) according to the invention comprises: - a step (E10) of detecting a stable state of at least one first parameter (T25) of said model, said first parameter being representative of a signal delivered by a sensor (3); - a step (E60) of obtaining a resetting parameter (GainF) of said model, during said stable state of said first parameter (T25), on the basis of said first parameter, a second parameter (PCN12R) of said model, and said basic digital model (5); and - a step (E70) of obtaining a reset model from the basic digital model (5) and the resetting parameter (GainF).
摘要:
This module (5) allows the filtering of a raw setpoint (N1_CMD_OP) intended for a corrector network (6) in an engine regulating system (20). It comprises: - a module (54) for detecting a filtering condition of said raw setpoint, and; - means for providing said corrector network with a filtered setpoint (N1_CMD_LIM) in place of said raw setpoint, when the filtering condition is detected.
摘要:
The method according to the invention comprises, during a phase (EO) of starting up the turbomachine : — a step (E10) of open-loop generation of a control (WF_OL) of the flow of fuel based on at least one pre-established law; and — a step (E20-E30) of closed-loop monitoring of at least one operating parameter of the turbomachine selected from: o an acceleration rate (dN2/dt) of a compressor of the turbomachine, and o an output temperature (EGT) of a turbine of the turbomachine, this monitoring step comprising keeping (E30) the operating parameter within a range of predefined values, using at least one corrective network (R1, R2, R3) associated with this parameter and capable of providing a correction signal correcting the fuel flow control generated in an open loop manner, making it possible to keep the operating parameter within the range of predefined values.
摘要:
Method of synchronising the engines of an aircraft. Method of synchronising the engines of an aircraft, according to at least one activation logic (10, 10') defining a deactivated state (20), an armed state (22) and at least one activated state (16, 18), and comprising: -switching (32) of the synchronisation from the deactivated state to the armed state when an activation order is issued by a pilot of the aircraft; -switching (36) of the synchronisation from the armed state to the activated state when at least certain safety and/or activation conditions are satisfied; and -switching (24, 34) of the synchronisation from the activated or armed state to the deactivated state when a deactivation order is issued by the pilot or when at least a part of the safety conditions are not satisfied.
摘要:
Method of controlling a turbomachine comprising; - a step of measuring a first temperature (T25) by a first temperature sensor, - a step of measuring a second temperature (T3) by a second temperature sensor, - a step of estimating a third temperature (T25M) modelling said first temperature, - a step of determining at least one control setpoint for at least one item of equipment with variable geometry of the turbomachine, as a function of said first temperature measured, characterized in that said first sensor exhibits a time constant C1 greater than a time constant C2 of the second sensor, the method comprising: - a step of detecting an ingestion of water or of hail as a function of a drop in said second temperature measured, and - when an ingestion of water or of hail is detected, a step of determining said control setpoint as a function of said third estimated temperature.
摘要:
The invention relates to detecting an icing condition of a fuel circuit (1) of a turbine engine including: a step of acquiring information representative of a first fuel temperature T 1 downstream from the fuel metering valve (10) and of the comparison of the first temperature T 1 to a first reference temperature Toi; a step of detecting a clogging of the filtration unit (6); and, in the event the measured temperature T 1 is lower than the first reference temperature Toi and a clog is detected, transmitting a signal indicating an icing condition of the fuel circuit (1). Information representing a second temperature T 2 of the fuel in the tank (3) can be acquired and compared to a reference temperature T02 to confirm or render the icing condition invalid. A signal indicating a need for servicing a fuel circuit is transmitted when the acquired temperatures T 1 and T 2 are not lower than the reference temperatures Toi and T02 while a clog is detected.