Fleet-Level Aircraft Prognostics for Condition-Based Maintenance

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Solution Overview

Problem

Current maintenance practices for complex vehicles like aircraft rely on predetermined schedules, which can be costly and inefficient, as they do not account for varying environmental conditions and usage patterns, leading to unnecessary maintenance and potential delays or unneeded stress on components.

Innovation Solution

A ground-based computing system analyzes performance data from multiple aircraft to determine degradation levels and remaining useful lifetime of components, enabling predictive maintenance schedules based on fleet-wide metrics, rather than fixed time intervals.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If predetermined scheduled maintenance is performed based on fixed time intervals, then maintenance is performed consistently across all aircraft, but unnecessary maintenance is performed and operational availability decreases

Engineering Contradiction:
Improvemaintenance consistencyVSAvoidoperational availability
Core Design Contradiction:
ReliabilityVSProductivity

Solution Approach 1:

The maintenance schedule transitions from static fixed time intervals to dynamic condition-based scheduling. The system continuously monitors component health parameters and adjusts maintenance timing based on actual degradation rates, allowing maintenance to be performed only when necessary rather than on predetermined schedules.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The system changes the parameter basis for maintenance scheduling from time-based parameters to condition-based parameters. By monitoring degradation parameters such as vibration, temperature, and performance metrics, the system determines maintenance needs based on actual component state rather than elapsed time.

Inventive Principle:
Principle #35Parameter changes

2Productivity

If condition-based maintenance is implemented for individual aircraft, then maintenance timing is optimized, but fleet-wide coordination and workforce utilization are inefficient

Engineering Contradiction:
Improvemaintenance timing optimizationVSAvoidfleet coordination complexity
Core Design Contradiction:
ProductivityVSDevice complexity

Solution Approach 1:

The system merges individual aircraft condition monitoring data into a centralized fleet-wide analysis platform. By combining data from multiple aircraft and identifying common degradation patterns, the system coordinates maintenance activities across the fleet to optimize workforce utilization and reduce overall maintenance costs.

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The system implements feedback loops where fleet-wide maintenance data is continuously analyzed and used to update predictive models for all aircraft. This feedback mechanism improves the accuracy of maintenance predictions over time and enables better coordination of maintenance activities across the fleet.

Inventive Principle:
Principle #23Feedback

3Productivity

If maintenance is delayed based on individual component condition, then unnecessary maintenance is avoided, but component failure risk increases without accurate prediction

Engineering Contradiction:
Improvemaintenance cost reductionVSAvoidcomponent failure risk
Core Design Contradiction:
ProductivityVSReliability

Solution Approach 1:

The system performs preliminary analysis of component degradation trends using historical data and predictive models to forecast future failure risks. By identifying components that are likely to fail within a specified time horizon, the system enables proactive maintenance scheduling that prevents failures while avoiding unnecessary maintenance of healthy components.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The system replaces mechanical judgment and manual inspection with automated predictive analytics and machine learning models. These computational systems analyze multiple sensor parameters simultaneously to predict component failure with higher accuracy than traditional mechanical assessment methods.

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

Data Source

PatentUS10964130B1Fleet level prognostics for improved maintenance of vehicles
Publication Date: 2021.03.30 NORTHROP GRUMMAN SYSTEMS CORP
  • US10964130B1 patent drawing
  • US10964130B1 patent drawing
  • US10964130B1 patent drawing

AI summary

A ground-based computing system receives data of performance parameters for like components disposed on like aircraft, and determines corresponding levels of degradation and rates of change of degradation for the respective like components. A fleet-level of degradation for groups of like components is generated based on analysis of the combined degradations of the like components in the respective group. At least one of a remaining useful lifetime (RUL) and a state-of-health (SOH) for each of the respective like components is determined based on a comparison of the levels of degradation for each of the like components and the fleet-level of degradation of the group of like components. A predicted time for maintenance for each like component is determined based on the corresponding at least one of the RUL and SOH of the like component, thereby enabling cost effective maintenance determinations for components based on a fleet-level information.