Pump health monitoring
A pump health monitoring system for an aircraft fuel pump. The health monitoring system compares environmental data to a reference environment and captures pump data when the environmental data matches the reference environment. The pump data captured is therefore normalized to the reference environment. A pump remaining useful life is calculated from the normalized pump data.
1. A pump health monitoring system for a fuel pump for pumping fuel in a fuel tank of an aircraft, the pump health monitoring system comprising:
a pump sensor interface configured to receive a value of one or more pump parameters relating to pump performance;
an environment sensor interface configured to receive a value of one or more environmental parameters selected from a group comprising: temperature, density, pressure, volume or head of fuel in the fuel tank; flow rate of fuel through the fuel pump; aircraft attitude; aircraft acceleration in one or more dimensions; and fuel pump acceleration in one or more dimensions;
a non-transitory storage device, wherein the storage device has stored therein:
a reference environment containing a predetermined reference value of one or more of the environmental parameters corresponding to an in-flight condition for the aircraft fuel pump; and
a set of instructions for:
comparing the value of one or more of the environmental parameters received via the environment sensor interface to the predetermined value of the same environmental parameter(s) of the reference environment; and
capturing a data set of instantaneous values including the one or more pump parameters and the one or more environmental parameters, if all the received environmental parameter values and the reference environmental parameter values match within a predefined range; and
a processor configured to execute the set of instructions and store a sample pump health indicator based on the captured data set.
2. The pump health monitoring system according to claim 1 , wherein the one or more pump parameters are selected from a group comprising: input Voltage, input current, frequency of input Voltage, missing phase of input Voltage, imbalance of input Voltage, motor Voltage, frequency of motor Voltage, motor current, motor speed, motor acceleration, control error, pump internal pressure, pump internal temperature, flow rate, vibration level, and internal system status.
3. The pump health monitoring system according to claim 1 , wherein the storage device further comprises one or more predetermined baseline pump health indicators.
4. The pump health monitoring system according to claim 3 , wherein the baseline pump health indicators are based on ideal or failure conditions.
5. The pump health monitoring system according to claim 4 , wherein the baseline pump health indicators are obtainable by out of service testing under controlled conditions.
6. The pump health monitoring system according to claim 3 , wherein the baseline pump health indicators stored in the storage device define one or more baseline pump health trends for pump health over time.
7. The pump health monitoring system according to claim 6 , wherein the storage device further comprises a set of instructions for comparing the sample pump health indicator to one or more baseline pump health indicators or trends.
8. The pump health monitoring system according to claim 7 , wherein the comparison between the sample pump health indicator and the one or more baseline pump health indicators or trends is made at a corresponding sample time.
9. The pump health monitoring system according to claim 7 , wherein the storage device further comprises a set of instructions for correcting the sample pump health indicator to account for differences between one or more environmental parameter values of the sample pump health indicator and of the baseline pump health indicators.
10. The pump health monitoring system according to claim 7 , wherein the storage device further comprises a set of instructions for calculating a Remaining Useful Life (RUL) of the pump based on the comparison between the sample pump health indicator and the one or more baseline pump health indicators or trends.
11. The pump health monitoring system according to claim 10 , wherein the RUL is a trajectory of predicted health decay over time.
12. The pump health monitoring system according to claim 10 , and further comprising a user interface for presenting the RUL to a user.
13. An aircraft fuel system comprising:
a fuel tank having a fuel pump for pumping fuel,
a pump health monitoring system comprising:
a pump sensor interface configured to receive a value of one or more pump parameters relating to pump performance;
an environment sensor interface configured to receive a value of one or more environmental parameters selected from a group comprising: temperature, density, pressure, volume or head of fuel in the fuel tank; flow rate of fuel through the fuel pump; aircraft attitude; aircraft acceleration in one or more dimensions; and fuel pump acceleration in one or more dimensions;
a non-transitory storage device, wherein the storage device has stored therein:
a reference environment containing a predetermined reference value of one or more of the environmental parameters corresponding to an in-flight condition for the aircraft fuel pump; and
a set of instructions for:
comparing the value of one or more of the environmental parameters received via the environment sensor interface to the predetermined value of the same environmental parameter(s) of the reference environment; and
capturing a data set of instantaneous values including the one or more pump parameters and the one or more environmental parameters, if all the received environmental parameter values and the reference environmental parameter values match within a predefined range; and
a processor configured to execute the set of instructions and store a sample pump health indicator based on the captured data set;
at least one pump sensor coupled to the pump sensor interface for inputting the value of one or more of the pump parameters, and
at least one environment sensor coupled to the environment sensor interface for inputting the value of the one or more of the environmental parameters.
14. The aircraft including the aircraft fuel system according to claim 13 wherein the aircraft includes a Fuel Quantity Management System (FQMS) or an Air Data Inertial Reference System (ADIRS), and the at least one environment sensor forms part of the FQMS or ADIRS.
15. A method of monitoring health of a fuel pump for pumping fuel in a fuel tank of an aircraft, the method comprising:
receiving a value of one or more pump parameters relating to pump performance;
receiving a value of one or more environmental parameters selected from a group comprising: temperature, density, pressure, volume or head of fuel in the fuel tank; flow rate of fuel through the fuel pump; aircraft attitude; aircraft acceleration in one or more dimensions; and fuel pump acceleration in one or more dimensions;
retrieving a reference environment containing a predetermined reference value of one or more of the environmental parameters corresponding to an in-flight condition for the aircraft fuel pump;
comparing a value of one or more of the environmental parameters to the predetermined value of the one or more of the environmental parameters of the reference environment;
capturing a data set of instantaneous values including the one or more pump parameters and the one or more environmental parameters, if all the received environmental parameter values and the reference environmental parameter values match within a predefined range; and
storing a sample pump health indicator based on the captured data set.
16. The method according to claim 15 , wherein the one or more pump parameters are selected from a group comprising: input Voltage, input current, frequency of input Voltage, missing phase of input Voltage, imbalance of input Voltage, motor Voltage, frequency of motor Voltage, motor current, motor speed, motor acceleration, control error, pump internal pressure, pump internal temperature, flow rate, vibration level, and internal system status.
17. The method according to claim 15 , further comprising comparing the sample pump health indicator to one or more baseline pump health indicators or baseline pump health trends for pump health over time.
18. The method according to claim 17 , further comprising correcting the sample pump health indicator to account for differences between one or more environmental parameter values of the sample pump health indicator and the baseline pump health indicators.
19. The method according to claim 17 , further comprising calculating a Remaining Useful Life (RUL) of the pump based on the comparison between the sample pump health indicator and the one or more baseline pump health indicators or trends.
20. The method according to claim 19 , further comprising presenting the pump RUL to a user.