Patent ID: 9097122
Filing Date: 2015-08-04
Classification: F01D,F05D

Abstract:
1. A turbine engine system, comprising: a turbine engine shaft comprising a shaft bore formed by a shaft wall, the shaft bore extending along an axial centerline through the turbine engine shaft between a first shaft end and a second shaft end; a first rotor connected to the turbine engine shaft at the first shaft end; a second rotor connected to the turbine engine shaft at the second shaft end; and an engine monitoring system comprising a sensor connected to the second rotor, a transmitter arranged at the first shaft end, and a plurality of conduit assemblies, wherein each of the plurality of conduit assemblies comprises a conduit extending axially within the shaft bore and connected to the shaft wall, and a first of the plurality of conduit assemblies further comprises a wire extending through the respective conduit and connecting the sensor and the transmitter.