发明名称 METHOD FOR DETECTING AN INCREASE IN THE RATING OF A LOW-PRESSURE TURBINE OF AN AIRCRAFT REACTOR DURING A CRUISING FLIGHT PHASE, AND ASSOCIATED DEVICE AND METHOD FOR REGULATING THE COOLING AIR FLOW RATE OF A LOW-PRESSURE TURBINE
摘要 A method for detecting an increase in the rating of a low-pressure turbine of a detection of an increase in the rating of a low-pressure turbine of a reactor of an aircraft reactor during a cruising flight phase, comprising measuring (100) the rating (N1) of the low-pressure turbine via a sensor. The method comprises determining (110) a rating gradient (G) of the low-pressure turbine from the measured rating (N1), comparing (120) said determined rating gradient (G) to a reference rating gradient (Gref), determining a positive or negative indication that the aircraft is under cruising phase conditions from flight parameters of the aircraft, and activating (160) an alarm if the determined rating gradient (G) is higher than the reference rating gradient (Gref) and if said received indication is positive.
申请公布号 US2017046886(A1) 申请公布日期 2017.02.16
申请号 US201615232975 申请日期 2016.08.10
申请人 SAFRAN AIRCRAFT ENGINES 发明人 EVERWYN Alexandre Patrick Jacques Roger;RODHAIN Arnaud
分类号 G07C5/08;F01D17/14;G08B21/18 主分类号 G07C5/08
代理机构 代理人
主权项 1. A method for detecting an increase in the rating of a low-pressure turbine of an aircraft reactor during a cruising phase, comprising measuring the rating of the low-pressure turbine via a sensor, characterized in that it comprises determining a rating gradient of the low-pressure turbine from the measured rating, comparing said determined rating gradient to a reference rating gradient, determining a positive or negative indication that the aircraft is under cruising phase conditions from flight parameters of the aircraft, and activating an alarm if the determined rating gradient is higher than the reference rating gradient and if said received indication is positive.
地址 Paris FR