Turbine Water Ingestion Detection via Multi-Indicator Summation

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Solution Overview

Problem

Current methods for detecting water or hail ingestion in aeroengine gas turbines are not robust, effective, or fast, often leading to undetected ingestion under various circumstances, especially at idling speeds or during descent.

Innovation Solution

A detection method that estimates two different indicators of water or hail ingestion and calculates a global indicator by summing these, allowing for detection under diverse conditions, including temperature and rotation speed measurements, with normalization functions to minimize false positives.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If temperature difference detection method is used (FR 2 681 377), then water ingestion can be detected under certain conditions, but detection reliability deteriorates when characteristics must be determined empirically and detection fails under various circumstances

Engineering Contradiction:
Improvedetection reliabilityVSAvoidempirical characteristic determination
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The patent changes the detection parameters from empirical temperature differences to directly measurable physical quantities (temperature T3 at combustion chamber inlet, rotation speed N2). This eliminates the need for empirical characteristic determination while improving detection reliability across various operating conditions.

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The patent segments the detection approach by using multiple independent indicators (temperature-based indicator and rotation speed-based indicator) that are summed to form a global indicator. This segmentation allows each indicator to be calculated independently from direct measurements without empirical calibration.

Inventive Principle:
Principle #1Segmentation

2Reliability

If pressure detection in combustion chamber is used (U.S. Pat. No. 5,471,831), then water ingestion detection is attempted, but measurement precision deteriorates due to small pressure variations

Engineering Contradiction:
Improveingestion detectionVSAvoidpressure variation measurement
Core Design Contradiction:
ReliabilityVSMeasurement precision

Solution Approach 1:

The patent replaces the mechanical pressure measurement system with thermal and rotational measurement systems. Temperature T3 and rotation speed N2 provide more precise and reliable indicators of water ingestion than the small pressure variations in the combustion chamber.

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

Solution Approach 2:

The patent introduces temperature T3 at the combustion chamber inlet and rotation speed N2 as intermediary parameters that more sensitively indicate water ingestion than direct pressure measurement. These intermediaries amplify the detection signal for better precision.

Inventive Principle:
Principle #24Intermediary (Mediator)

3Adaptability or versatility

If single indicator detection is used, then detection system remains simple, but detection effectiveness deteriorates under diverse operating circumstances

Engineering Contradiction:
Improvedetection under various circumstancesVSAvoidmultiple indicators and summation
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

The patent merges multiple detection indicators (temperature-based indicator I1 and rotation speed-based indicator I2) into a single global indicator IG by summation. This combining approach maintains detection simplicity while improving adaptability to diverse operating conditions through multi-parameter monitoring.

Inventive Principle:
Principle #5Merging (Combining)

Data Source

PatentUS9046040B2Detection of the ingress of water or hail into a turbine engine
Publication Date: 2015.06.02 SAFRAN AIRCRAFT ENGINES SAS
  • US9046040B2 patent drawing
  • US9046040B2 patent drawing
  • US9046040B2 patent drawing

AI summary

A detection method for detecting ingestion of water or hail in a gas turbine engine, the engine including at least a compressor, a combustion chamber, and a turbine, the method including: estimating a value of a first indicator representative of water or hail being ingested; estimating a value of a second indicator representative of water or hail being ingested, the second indicator being different from the first indicator; and calculating a value of a global indicator by summing at least the first indicator and the second indicator.