Starter Injector Purge Circuit Clogging Detection

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Solution Overview

Problem

Fuel supply systems for aircraft turbomachines face clogging issues in the starter and purge circuits, leading to potential downtime despite existing purging methods, as coking can still occur and result in partial or total clogging.

Innovation Solution

A fuel supply system with a pressure representative value measuring means to detect clogging by measuring pressure between the starter injector and hydraulic resistance during purge air flow, allowing for early detection and maintenance before turbomachine downtime, and including a monitoring device to compare pressure values with thresholds to signal clogging information.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If reverse purge is used to clear fuel from the starter circuit, then fuel stagnation is reduced, but coking still occurs and clogging happens

Engineering Contradiction:
Improveclogging preventionVSAvoidcoking
Core Design Contradiction:
ReliabilityVSObject-affected harmful factors

Solution Approach 1:

The patent applies preliminary action by measuring pressure during the purge operation to detect clogging trends before they cause actual coking and system failure. The pressure measurement provides early warning, allowing maintenance to be performed before the harmful coking process completes and causes reliability issues.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The patent implements feedback by continuously monitoring pressure in the starter circuit during purge operations and comparing it against reference values. This feedback mechanism allows the system to detect deviations indicating clogging progression and trigger appropriate maintenance actions, creating a closed-loop system that prevents coking-related failures.

Inventive Principle:
Principle #23Feedback

2Difficulty of detecting and measuring

If pressure measurement is added to monitor clogging, then detection capability is improved, but device complexity increases

Engineering Contradiction:
Improveclogging detectionVSAvoidmeasurement system
Core Design Contradiction:
Difficulty of detecting and measuringVSDevice complexity

Solution Approach 1:

The patent applies universality by using a pressure sensor that serves multiple functions: it measures pressure during normal operation, monitors purge effectiveness, detects clogging trends, and provides diagnostic information. This multi-functional approach improves detection capability without adding dedicated specialized equipment for each function.

Inventive Principle:
Principle #6Universality (Multi-functionality)

Solution Approach 2:

The patent implements self-service by utilizing the existing purge system's pressure characteristics to detect clogging. The same purge air flow that is intended to clean the system also provides the pressure signal needed for detection, eliminating the need for separate diagnostic equipment and reducing overall system complexity.

Inventive Principle:
Principle #25Self-service

Applied Scientific Principles

This section explains which scientific principles are used to turn an abstract innovation direction into a practical engineering solution.

Function Achieved in This Case

Enables early detection and prevention of clogging in the fuel supply system, reducing the risk of turbomachine downtime by signaling maintenance needs before significant issues arise, thus ensuring continuous operation.

Implementation Method 1

a pressure representative value measuring means configured to measure a pressure representative value between the starter injector and the first hydraulic resistance, during a purge air flow between the starter injector and the first hydraulic resistance

Methodology Applied
Scientific EffectPressure measurement:

Implementation Method 2

The fuel present in the injector and the pipings is thus purged because of the pressure difference between pressurised air from the compressor outlet and air at atmospheric pressure

Methodology Applied
Scientific EffectPressure difference driven flow: Pressure Gradient

Data Source

PatentUS10947903B2Clogging monitoring in a starter injector purge circuit for a turbomachine
Publication Date: 2021.03.16 SAFRAN HELICOPTER ENGINES
  • US10947903B2 patent drawing
  • US10947903B2 patent drawing
  • US10947903B2 patent drawing

AI summary

A fuel supply system for a turbomachine. The supply system includes a starter circuit, at least one first hydraulic resistance and a purge circuit. The purge circuit includes a duct including an opening at the exterior of the supply system. The purge circuit is configured to make purge air flow between a starter injector and the opening through the first hydraulic resistance. The supply system includes a device for measuring a value representative of pressure, which devices are configured to measure a value representative of pressure between the starter injector and the first hydraulic resistance when purge air flows between the starter injector and the first hydraulic resistance.