Helicopter Engine Maintenance Prescription System

Resolve Bottlenecks,
Find Innovative Solutions
Generate Solutions

Solution Overview

Problem

Helicopter engines face complex maintenance challenges due to high variability in parts and operating conditions, leading to sub-optimal maintenance practices that impact performance and safety, as existing systems fail to account for the engine's specific configuration and maintenance history.

Innovation Solution

A maintenance prescription system that utilizes a centralized database to track operational usage state data, authorized modifications, and maintenance history, implementing alarms to ensure data completeness and relevance, and performs trend analyses to optimize maintenance plans and identify probable causes of unexpected events.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Ease of operation

If a simplified and synthetic representation of engine usage and configuration is used for maintenance tracking, then the ease of operation is improved, but the measurement precision and reliability of maintenance decisions deteriorate

Engineering Contradiction:
Improveease of maintenance trackingVSAvoidprecision of engine condition assessment
Core Design Contradiction:
Ease of operationVSMeasurement precision

Solution Approach 1:

The system segments maintenance tracking into multiple hierarchical levels: synthetic parameters for quick overview (Levels 1-2) and detailed operational parameters for precise analysis (Level 3). This allows technicians to use simplified views when needed while accessing comprehensive data when precision is required, resolving the contradiction between ease of operation and measurement precision.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The system adds a temporal dimension to maintenance tracking by implementing continuous monitoring of operational parameters over time. Instead of relying on static synthetic representations, the system captures dynamic changes in engine conditions across multiple time points, enabling precise assessment while maintaining user-friendly interfaces through progressive disclosure of data dimensions.

Inventive Principle:
Principle #17Another dimension (Dimensionality change)

2Reliability

If significant safety margins are applied to maintenance requirements to ensure flight safety, then the reliability is improved, but the productivity and maintenance efficiency deteriorate

Engineering Contradiction:
Improveflight safetyVSAvoidmaintenance efficiency
Core Design Contradiction:
ReliabilityVSProductivity

Solution Approach 1:

The system transitions from static safety margins to dynamic risk assessment. Maintenance intervals and requirements are continuously adjusted based on real-time monitoring of actual engine operational parameters, condition trends, and usage patterns. This allows the system to maintain high reliability by responding to actual engine needs while improving productivity by avoiding unnecessary conservative maintenance on engines in good condition.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The system changes maintenance parameters dynamically based on monitored operational conditions. Instead of applying fixed safety margins, the system adjusts maintenance thresholds, intervals, and priorities according to actual engine behavior, enabling optimized maintenance scheduling that maintains safety while reducing unnecessary maintenance operations.

Inventive Principle:
Principle #35Parameter changes

3Reliability

If the number and frequency of maintenance operations are increased to account for high variability in operating conditions, then the reliability is improved, but the loss of time and maintenance cost increase

Engineering Contradiction:
Improveengine safetyVSAvoidmaintenance time
Core Design Contradiction:
ReliabilityVSLoss of time

Solution Approach 1:

The system implements condition-based maintenance where the engine's own operational data serves as the indicator for maintenance needs. By continuously monitoring parameters such as temperature, vibration, and performance metrics, the system allows the engine to 'signal' when maintenance is actually required, rather than following predetermined schedules. This reduces unnecessary maintenance time while maintaining reliability through targeted interventions.

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

The system establishes continuous feedback loops between operational monitoring and maintenance decision-making. Real-time data from engine sensors feeds into predictive models that identify degradation trends, allowing maintenance to be scheduled based on actual condition evolution rather than conservative estimates. This feedback mechanism optimizes the balance between reliability and maintenance time loss.

Inventive Principle:
Principle #23Feedback

Data Source

PatentEP2538376B1System for prescribing maintenance of a helicopter engine
Publication Date: 2019.06.12 SAFRAN HELICOPTER ENGINES
  • EP2538376B1 patent drawingFigure 1
  • EP2538376B1 patent drawingFigure 2~4
  • EP2538376B1 patent drawingFigure 5

AI summary

The system has a centralized database (14) that is utilized for storing operational data e.g. maintenance action describing data, that is related to working condition, possible modifications and authorized modifications of engines of a helicopter (16), and definition of maintenance plans for the engines according to predetermined values of working condition indicators. The working condition indicators for each engine are obtained. An identification unit is utilized for identifying maintenance operation that is applied to each of the engines depending on the operational data. An independent claim is also included for a method for regulating maintenance of a helicopter engine.