Patent ID: 9708926
Date: 2017-07-18
CPC Classifications: F01D,F02K,F05D,G01L,G01M,G01P,Y02T

Claim:
1. Turbine engine, in particular for an aircraft, comprising at least one axial shaft rotatably mounted in a casing of the turbine engine, the turbine engine comprising: an annular reference part which is rigidly connected to a first portion of the shaft of the turbine engine, the reference part comprising short and long longitudinal reference teeth; first means for detecting the passage of the short and long reference teeth in a first transverse plane so as to measure the speed of the shaft of the turbine engine about its axis; an annular measurement part which is rigidly connected to a second portion (A second means for detecting the passage of the long reference teeth and the measurement teeth in a second transverse plane so as to measure the torque of the shaft of the turbine engine.