IDG Wear Equalization via Pilot Feedback

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Solution Overview

Problem

Multi-engine aircraft experience uneven wear and maintenance needs due to uneven use of Integrated Drive Generators (IDGs) during single-engine or few-engine taxiing operations, leading to frequent shop visits and unscheduled removals.

Innovation Solution

An IDG equalization system that monitors and compares the operating times of multiple IDGs, providing a signal to the pilot to select the appropriate IDG for ground operations, thereby equalizing their use and reducing wear disparities.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Loss of energy

If single-engine taxiing is used for fuel savings and noise reduction, then fuel consumption and noise emissions are reduced, but uneven wear of IDGs occurs leading to frequent maintenance

Engineering Contradiction:
Improvefuel consumptionVSAvoidIDG wear uniformity
Core Design Contradiction:
Loss of energyVSReliability

Solution Approach 1:

The system continuously monitors the accumulated operating time of each IDG and provides feedback to the pilot through display indicators. This feedback mechanism enables the pilot to adjust engine usage patterns to equalize IDG wear, thus resolving the contradiction between fuel savings and uniform IDG wear.

Inventive Principle:
Principle #23Feedback

Solution Approach 2:

The system automatically tracks and compares IDG operating times without requiring manual intervention. The pilot simply follows the system's guidance to select which engine to operate, allowing the system to self-manage the equalization process while maintaining fuel efficiency.

Inventive Principle:
Principle #25Self-service

2Object-generated harmful factors

If single-engine taxiing is used to reduce noise emissions, then noise levels are reduced, but uneven IDG wear increases maintenance frequency

Engineering Contradiction:
Improvenoise emissionsVSAvoidmaintenance frequency
Core Design Contradiction:
Object-generated harmful factorsVSProductivity

Solution Approach 1:

The monitoring system provides real-time feedback on IDG wear status, enabling the pilot to make informed decisions about engine selection during taxi operations. This feedback loop allows noise reduction through single-engine operation while preventing excessive maintenance frequency through equalized wear management.

Inventive Principle:
Principle #23Feedback

3Ease of operation

If starboard engine is started first due to gate connection positioning, then operational convenience is improved, but port IDG experiences uneven wear

Engineering Contradiction:
Improveengine start convenienceVSAvoidIDG wear uniformity
Core Design Contradiction:
Ease of operationVSReliability

Solution Approach 1:

The system pre-calculates and displays the recommended engine selection based on accumulated wear data before the pilot makes a decision. This preliminary guidance allows the pilot to maintain operational convenience while proactively preventing uneven wear patterns.

Inventive Principle:
Principle #10Preliminary action

4Loss of energy

If one engine is shut down after landing for fuel savings, then fuel consumption is reduced, but the remaining IDG experiences increased wear and unscheduled removals

Engineering Contradiction:
Improvefuel consumptionVSAvoidIDG service life
Core Design Contradiction:
Loss of energyVSDuration of action of stationary object

Solution Approach 1:

The system monitors IDG operating hours and provides feedback guidance to the pilot for selecting which engine to operate during taxi-in and which to keep running after landing. This enables fuel savings through single-engine operation while distributing wear evenly to extend IDG service life.

Inventive Principle:
Principle #23Feedback

Data Source

PatentEP3809552B1Equalizing wearing of two or more electrical power generators of an aircraft
Publication Date: 2022.08.31 HAMILTON SUNDSTRAND CORP
  • EP3809552B1 patent drawingFigure 1
  • EP3809552B1 patent drawingFigure 2A
  • EP3809552B1 patent drawingFigure 2B

AI summary

Apparatus and associated methods relate to equalizing wearing of a plurality of electrical power generators of an aircraft. Such equalization is achieved by logging operating conditions of at least a powered subset of the electrical power generators and then comparing of the logged operating conditions of each of the plurality of electrical power generators. Based on the comparison of the logged operating conditions, one of the plurality of electrical power generators for use the aircraft is recommended. A signal indicative of the recommended one of the electrical power generators determined is then generated.