Actuator Lifetime Estimation via Control Command Analysis

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Solution Overview

Problem

Current methods for determining the repair timing of aircraft actuators lack precision, leading to potential failures before scheduled maintenance and unnecessary replacements, as operation records vary significantly between aircraft.

Innovation Solution

An actuator monitoring system that calculates the use time and torque of an electric actuator based on control commands and feedback signals, allowing for precise estimation of its lifetime and issuing warnings when the estimated lifetime is reached before the scheduled repair time.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Measurement precision

If repair timing is determined based on past repair records, then maintenance can be scheduled in advance, but the estimation precision of actuator lifetime is insufficient

Engineering Contradiction:
Improvelifetime estimation precisionVSAvoidmonitoring system complexity
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The system implements feedback by continuously monitoring operation records (on/off timing, operation time, load conditions) and using this information to dynamically update and refine lifetime estimation. The control unit accumulates operation history and feeds it back into the estimation algorithm, allowing the system to adapt to actual usage patterns and improve precision over time.

Inventive Principle:
Principle #23Feedback

Solution Approach 2:

The actuator monitoring system performs self-diagnosis and self-monitoring by automatically tracking its own operation records without external intervention. The control unit independently calculates usage metrics and estimates lifetime based on accumulated data, enabling the system to serve its own maintenance needs without requiring complex external monitoring infrastructure.

Inventive Principle:
Principle #25Self-service

2Reliability

If actuator is replaced based on fixed repair timing, then maintenance scheduling is simplified, but premature replacement or failure before maintenance occurs

Engineering Contradiction:
Improveactuator reliabilityVSAvoidmaintenance timing accuracy
Core Design Contradiction:
ReliabilityVSLoss of time

Solution Approach 1:

The system transitions from static fixed-schedule maintenance to dynamic condition-based maintenance. The control unit continuously updates lifetime estimation based on real-time operation records, allowing maintenance timing to adapt dynamically to actual actuator usage patterns and conditions, thereby optimizing reliability and preventing both premature replacement and unexpected failures.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The system performs preliminary assessment by continuously monitoring operation records and estimating remaining lifetime before actual failure occurs. This allows maintenance to be scheduled proactively based on predicted lifetime rather than reactively after failure or rigidly according to fixed schedules, improving both reliability and timing accuracy.

Inventive Principle:
Principle #10Preliminary action

Data Source

PatentUS10401261B2Actuator monitoring system
Publication Date: 2019.09.03 MITSUBISHI HEAVY IND LTD
  • US10401261B2 patent drawing
  • US10401261B2 patent drawing

AI summary

An actuator monitoring system is provided with an electric actuator having a motor and a control unit which outputs a control command (CMD) to the motor to control the operation of the motor. The control unit calculates a use time of the electric actuator based on the control command (CMD) outputted to the motor. Moreover, the control unit estimates the lifetime of the electric actuator based on the calculated use time.