Prognostic health monitoring and jam detection for use with an aircraft

Patent metadata

Field	Value
Publication number	US-10589871-B2
Application number	US-201715721268-A
Country	US
Kind code	B2
Filing date	Sep 29, 2017
Priority date	Sep 25, 2017
Publication date	Mar 17, 2020
Grant date	Mar 17, 2020

Abstract

A method of prognostic health monitoring is provided for use with an aircraft. The method includes generating torque for controlling positions of controllable surfaces at right- and left-hand-sides (RHS and LHS) of the aircraft in a power drive unit (PDU) based on torque-limiter (TL) thresholds, performing real-time monitoring of the torque at the RHS and LHS of the aircraft, generating RHS and LHS torque information from results of the performing of the real-time monitoring, analyzing the RHS and LHS torque information and controlling operations of the PDU based on results of the analysis by at least one of modifying, tuning and defining the TL thresholds.

First claim

What is claimed is:

1. A prognostic health monitoring system for use with an aircraft comprising a power drive unit (PDU) and actuators distributed along right- and left-hand-side (RHS and LHS) wings and driven by torque generated in the PDU as RHS and LHS driveline torques to control positions of controllable surfaces via RHS and LHS torque-limiters at each individual one of the actuators distributed along the RHS and LHS wings, respectively, the prognostic health monitoring system comprising:
RHS and LHS torque monitors respectively disposed at opposite operational sides of the PDU; and
a processing unit which is communicative with each RHS and LHS torque monitor and configured to perform by way of communications with the RHS and LHS torque monitors:
real-time monitoring of the RHS and LHS driveline torques,
an analysis of information derived from the real-time monitoring, and
feedback control of operations of the PDU based on results of the analysis comprising at least one of a modification, a tuning and a definition of torque-limiter (TL) thresholds of each of the RHS and LHS torque-limiters at each individual one of the actuators distributed along the RHS and LHS wings, respectively.

2. The prognostic health monitoring system according to claim 1 , wherein each RHS and LHS torque monitor comprises a floating or fixed torque-transducer.

3. The prognostic health monitoring system according to claim 1 , further comprising a database which is accessible by the processing unit and on which historic torque information is stored.

4. The prognostic health monitoring system according to claim 1 , wherein:
the processing unit is configured to continuously perform the real-time monitoring, and
the real-time monitoring comprises at least one of trend monitoring and active prognostic health monitoring.

5. The prognostic health monitoring system according to claim 1 , wherein the modification of the TL thresholds is based on at least one of actuator life, actuator station, aircraft airspeed and aircraft temperature.

6. The prognostic health monitoring system according to claim 1 , wherein the tuning of the TL thresholds is based on aircraft performance targets.

7. The prognostic health monitoring system according to claim 1 , wherein the definition of the TL thresholds is based on at least one of input torque, a rate of change of input torque and a magnitude of opposite wing actuator input torque.

8. A prognostic health monitoring system for use with an aircraft comprising a power drive unit (PDU) and actuators distributed along right- and left-hand-side (RHS and LHS) wings and driven by torque generated in the PDU to control positions of controllable surfaces via RHS and LHS torque-limiters at each individual one of the actuators distributed along the RHS and LHS wings, respectively, the prognostic health monitoring system comprising:
RHS and LHS torque monitors disposed at each individual one of the actuators distributed along the RHS and LHS wings, respectively; and
a processing unit which is communicative with each RHS and each LHS torque monitor and configured to perform by way of communications with the RHS and LHS torque monitors:
real-time monitoring of input torque for each individual one of the actuators distributed along the RHS wing and the LHS wing,
an analysis of information derived from the real-time monitoring, and
feedback control of operations of the PDU based on results of the analysis comprising at least one of a modification, a tuning and a definition of torque-limiter (TL) thresholds of each of the RHS and LHS torque-limiters at each individual one of the actuators distributed along the RHS and LHS wings, respectively.

9. The prognostic health monitoring system according to claim 8 , wherein each RHS and LHS torque monitor comprises a floating or fixed torque-transducer.

10. The prognostic health monitoring system according to claim 8 , wherein the modification of the TL thresholds is based on at least one of actuator life, actuator station, aircraft airspeed and aircraft temperature.

11. The prognostic health monitoring system according to claim 8 , wherein the tuning of the TL thresholds is based on aircraft performance targets.

12. The prognostic health monitoring system according to claim 8 , wherein the definition of the TL thresholds is based on at least one of input torque, a rate of change of input torque and a magnitude of opposite wing actuator input torque.

13. The prognostic health monitoring system according to claim 8 , further comprising a database which is accessible by the processing unit and on which historic torque information is stored.

14. The prognostic health monitoring system according to claim 8 , wherein:
the processing unit is configured to continuously perform the real-time monitoring, and
the real-time monitoring comprises at least one of trend monitoring and active prognostic health monitoring.

Assignees

• Hamilton Sundstrand Corp

Inventors

• Harrington Erik
• Miller Christian
• Bishop Yuniya S
• Kreienheder Jason B
• Skirtich Michael
• Wallen Gregory T

Classifications

• B64D2045/0085

  Devices for aircraft health monitoring, e.g. monitoring flutter or vibration · CPC title

• B64C13/38

  with power amplification · CPC title

• G07C5/085

  using electronic data carriers · CPC title

• G07C5/0808

  Diagnosing performance data (testing of vehicles G01M17/00; testing of electrical installation on vehicles G01R31/005) · CPC title

• B64D45/00 Primary

  Aircraft indicators or protectors not otherwise provided for · CPC title