| 摘要 |
The invention relates to a turbine engine, in particular for an aircraft, comprising at least one axial shaft (2) rotatably mounted in a casing of the turbine engine, the turbine engine comprising: a reference annular part (10) comprising short (11) and long (12) longitudinal reference teeth; first means for detecting the passage of the short (11) and long (12) reference teeth such as to measure the speed of the shaft (2) of the turbine engine (1) about the axis (X) thereof; an annular measurement part (20) comprising longitudinal measurement teeth (21); and second means for detecting the passage of the long reference teeth (12) and the measurement teeth (21) such as to measure the torque of the turbine engine shaft (2). |
