Aerospace turbomachine adaptive machine learning controls with health monitoring capability
A turbomachine monitoring and control system includes a temperature sensor configured to measure temperature of a turbomachine disposed onboard a vehicle, a vibration sensor configured to measure vibration of the turbomachine, and a controller including one or more processors. The controller is configured to receive and analyze temperature data generated by the temperature sensor and vibration data generated by the vibration sensor. The controller is further configured to determine a health condition of the turbomachine based on the analysis.
1 . A monitoring and control system comprising:
a temperature sensor configured to measure temperature of a turbomachine disposed onboard a vehicle;
a vibration sensor configured to measure vibration of the turbomachine; and
a controller including one or more processors, wherein the controller is configured to receive and analyze temperature data generated by the temperature sensor and vibration data generated by the vibration sensor, wherein the controller is further configured to determine a health condition of the turbomachine based on the analysis, wherein the vibration data generated by the vibration sensor includes raw waveform data, wherein the controller is further configured to analyze the raw waveform data and determine a current energy level at a frequency of interest, and wherein the controller is further configured to compare the current energy level at the frequency of interest to a baseline energy value to determine the health condition of the turbomachine.
2 . The monitoring and control system of claim 1 , wherein the controller is further configured to determine a predicted remaining life of the turbomachine based on the health condition that is determined.
3 . The monitoring and control system of claim 1 , wherein the turbomachine includes a rotor that is driven by an electric motor, and wherein the temperature sensor is configured to measure the temperature of the electric motor.
4 . The monitoring and control system of claim 3 , wherein the vibration sensor is configured to measure the vibration of the rotor.
5 . The monitoring and control system of claim 4 , wherein the controller is configured to analyze the temperature data that is generated by the temperature sensor while the turbomachine is at a steady state operational stage, and wherein the controller is configured to analyze the vibration data that is generated by the vibration sensor while the turbomachine is at a transient operational stage.
6 . The monitoring and control system of claim 1 , wherein the controller is further configured to adjust one or more operating settings of the turbomachine based on the health condition indicating that the turbomachine is degraded, and wherein the controller is further configured to adjust the one or more operating settings to maintain a desired level of performance of the turbomachine.
7 . The monitoring and control system of claim 6 , wherein the controller is configured to adjust the one or more operating settings in relation to a level of degradation of the turbomachine.
8 . The monitoring and control system of claim 1 , wherein the controller is further configured to modify a performance curve that is used to control operation of the turbomachine based on the health condition that is determined, and wherein the performance curve includes constant speed lines, mass flow rates, and pressure ratios.
9 . The monitoring and control system of claim 1 , wherein the controller is further configured to modify a commanded position of diffuser vanes of the turbomachine based on the health condition that is determined.
10 . The monitoring and control system of claim 1 , wherein the turbomachine includes a rotor that is driven by an electric motor, and wherein the controller is further configured to increase electrical power supplied to the electric motor based on the health condition indicating that the turbomachine is degraded.
11 . The monitoring and control system of claim 1 , wherein responsive to the health condition indicating that the turbomachine is degraded, the controller is further configured to restrict operation of at least one of the turbomachine or the vehicle during a trip.
12 . The monitoring and control system of claim 1 , wherein the controller is configured to determine the health condition of the turbomachine by one or both of (i) comparing a temperature value of the temperature data to a designated temperature range and comparing a vibration value of the vibration data to a designated vibration range or (ii) comparing the temperature value to historical temperature data of the turbomachine generated by the temperature sensor and comparing the vibration value to historical vibration data of the turbomachine generated by the vibration sensor.
13 . The monitoring and control system of claim 1 , wherein the turbomachine is a compressor configured to compress air for at least one of pressurization or air conditioning within a cabin of the vehicle.
14 . A method comprising:
obtaining temperature data generated by a temperature sensor indicating a measured temperature of a turbomachine disposed onboard a vehicle;
obtaining vibration data generated by a vibration sensor indicating a measured vibration of the turbomachine; and
determining a health condition of the turbomachine based on an analysis of the temperature data and the vibration data,
wherein, responsive to determining the health condition of the turbomachine, the method further comprises one or more of:
modifying a performance curve that is used to control operation of the turbomachine based on the health condition, wherein the performance curve includes constant speed lines, mass flow rates, and pressure ratios;
modifying a commanded position of diffuser vanes of the turbomachine based on the health condition; or
increasing electrical power supplied to an electric motor of the turbomachine based on the health condition.
15 . The method of claim 14 , wherein said obtaining the temperature data comprises obtaining only temperature data that is generated by the temperature sensor while the turbomachine is at a steady state operational stage, and wherein said obtaining the vibration data comprises obtaining only vibration data that is generated by the vibration sensor while the turbomachine is at a transient operational stage.
16 . The method of claim 14 , further comprising adjusting one or more operating settings of the turbomachine based on the health condition indicating that the turbomachine is degraded, wherein the one or more operating settings are adjusted to maintain a desired level of performance of the turbomachine.
17 . The method of claim 14 , wherein the vibration data generated by the vibration sensor includes raw waveform data, and the method further includes:
determining a current energy level at a frequency of interest based on an analysis of the raw waveform data; and
comparing the current energy level at the frequency of interest to a baseline energy value to determine the health condition of the turbomachine.
18 . An aircraft comprising:
a turbomachine installed onboard the aircraft, wherein the turbomachine includes a rotor that is configured to compress air and an electric motor that is configured to drive rotation of the rotor; and
a monitoring and control system disposed onboard the aircraft, wherein the monitoring and control system comprises:
a temperature sensor configured to measure temperature of a turbomachine disposed onboard a vehicle;
a vibration sensor configured to measure vibration of the turbomachine; and
a controller including one or more processors, wherein the controller is configured to:
receive and analyze temperature data generated by the temperature sensor and vibration data generated by the vibration sensor,
determine a health condition of the turbomachine based on the analysis,
in response to determining the health condition of the turbomachine, one or more of: (a) modify a performance curve that is used to control operation of the turbomachine based on the health condition, wherein the performance curve includes constant speed lines, mass flow rates, and pressure ratios, (b) modify a commanded position of diffuser vanes of the turbomachine based on the health condition, or (c) increase electrical power supplied to an electric motor of the turbomachine based on the health condition.
19 . The aircraft of claim 18 , wherein the vibration data generated by the vibration sensor includes raw waveform data, wherein the controller is further configured to analyze the raw waveform data and determine a current energy level at a frequency of interest, and wherein the controller is further configured to compare the current energy level at the frequency of interest to a baseline energy value to determine the health condition of the turbomachine.
20 . A method comprising:
obtaining temperature data generated by a temperature sensor indicating a measured temperature of a turbomachine disposed onboard a vehicle;
obtaining vibration data generated by a vibration sensor indicating a measured vibration of the turbomachine, wherein the vibration data generated by the vibration sensor includes raw waveform data;
determining a current energy level at a frequency of interest based on an analysis of the raw waveform data; and
comparing the current energy level at the frequency of interest to a baseline energy value to determine the health condition of the turbomachine.