SURVEILLANCE D'UN CAPTEUR DE TYPE TRANSFORMATEUR DIFFERENTIEL VARIABLE LINEAIRE
    2.
    发明公开
    SURVEILLANCE D'UN CAPTEUR DE TYPE TRANSFORMATEUR DIFFERENTIEL VARIABLE LINEAIRE 审中-公开
    监测线性差动变压器传感器

    公开(公告)号:EP2864737A2

    公开(公告)日:2015-04-29

    申请号:EP13744614.2

    申请日:2013-06-24

    申请人: Snecma

    IPC分类号: G01D5/22 G01D18/00

    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.

    PROCEDE ET SYSTEME DE RECALAGE D'UN MODELE NUMERIQUE
    4.
    发明公开
    PROCEDE ET SYSTEME DE RECALAGE D'UN MODELE NUMERIQUE 有权
    VERFAHREN UND系统ZURRÜCKSTELLUNGEINES DIGITALEN模块

    公开(公告)号:EP3011399A1

    公开(公告)日:2016-04-27

    申请号:EP14736891.4

    申请日:2014-06-11

    申请人: SNECMA

    发明人: DJELASSI, Cedrik

    IPC分类号: G05B17/02

    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).

    摘要翻译: 重置基本数字模型包括检测模型的至少一个第一参数的稳定状态的步骤,第一参数表示由传感器传递的信号; 在模型的第二参数和基本数字模型的第一参数的稳定状态下作为第一参数的函数获得模型的重置参数的步骤; 以及从基本数字模型和复位参数获得复位模型的步骤。

    PROCÉDÉ ET DISPOSITIF DE GÉNÉRATION D'UNE COMMANDE DE DÉBIT DE CARBURANT DESTINÉ À ÊTRE INJECTÉ DANS UNE CHAMBRE DE COMBUSTION D'UNE TURBOMACHINE

    公开(公告)号:EP2989311A1

    公开(公告)日:2016-03-02

    申请号:EP14727584.6

    申请日:2014-04-22

    申请人: SNECMA

    发明人: DJELASSI, Cedrik

    IPC分类号: F02C9/26

    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.

    PROCÉDÉ DE SYNCHRONISATION DES MOTEURS D'UN AVION
    8.
    发明公开
    PROCÉDÉ DE SYNCHRONISATION DES MOTEURS D'UN AVION 有权
    VERFAHREN ZUR同步产品TRIEBWERKE EINES FLUGZEUGS

    公开(公告)号:EP2753544A1

    公开(公告)日:2014-07-16

    申请号:EP12762347.8

    申请日:2012-09-03

    申请人: SNECMA

    IPC分类号: B64D31/12 F02C9/42

    CPC分类号: B64D31/12 F02C9/42

    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.

    摘要翻译: 一种根据限定停用状态(20),起动状态(22)和至少一个激活状态(16,18)的至少一个激活逻辑(10,10')同步飞机引擎的方法,以及 包括:当飞机的飞行员发出激活命令时,将(32)同步从停用状态传递到起动状态; 当满足至少某些安全和/或激活条件时,将(36)同步从引发状态传递到激活状态; 以及当所述飞行员发出停用命令时或者每当安全条件中的至少一些不被满足时,将(24,34)同步从激活或引发状态传递到停用状态。

    PROCÉDÉ DE COMMANDE D'UNE TURBOMACHINE
    9.
    发明公开
    PROCÉDÉ DE COMMANDE D'UNE TURBOMACHINE 有权
    用于控制涡轮机

    公开(公告)号:EP2633169A1

    公开(公告)日:2013-09-04

    申请号:EP11787711.8

    申请日:2011-10-17

    申请人: Snecma

    IPC分类号: F02C9/28

    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.

    PROCEDE DE DETECTION D'UN ETAT DE GIVRAGE OU DE BESOIN DE MAINTENANCE D'UN CIRCUIT DE CARBURANT DE TURBOMACHINE
    10.
    发明公开
    PROCEDE DE DETECTION D'UN ETAT DE GIVRAGE OU DE BESOIN DE MAINTENANCE D'UN CIRCUIT DE CARBURANT DE TURBOMACHINE 审中-公开
    方法结冰状况检测或涡轮发动机的燃料电路维护的要求

    公开(公告)号:EP2419617A1

    公开(公告)日:2012-02-22

    申请号:EP10723654.9

    申请日:2010-04-12

    申请人: Snecma

    IPC分类号: F02C7/224 F23R3/28 F23K5/02

    CPC分类号: F02C7/224 F23K5/04 F23K5/16

    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.