Gas Turbine Separator Assembly for Cooling Air Particle Removal

Resolve Bottlenecks,
Find Innovative Solutions
Generate Solutions

Solution Overview

Problem

Gas turbine engines in aircraft face reduced cooling effectiveness and component durability issues due to airborne particles like fine sand, which accumulate on high-temperature surfaces, leading to increased metal temperatures and reduced operational time.

Innovation Solution

A separator assembly is designed to remove entrained particles from the cooling air stream, comprising a first particle separator and a particle remover, which separates the fluid stream into reduced-particle and particle-laden streams, with the particle remover further processing the particle-laden stream and returning a second reduced-particle stream to the separator to enhance particle removal efficiency.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Temperature

If cooling air is ducted from compressors to turbine components, then cooling effectiveness is improved, but particle accumulation on turbine surfaces increases

Engineering Contradiction:
Improveturbine component temperatureVSAvoidparticle accumulation
Core Design Contradiction:
TemperatureVSObject-affected harmful factors

Solution Approach 1:

The particle separator is positioned in the cooling air duct upstream of the turbine components, performing preliminary particle removal from the cooling air before it reaches the turbine surfaces. This prevents particle accumulation while maintaining the cooling function, resolving the contradiction by addressing the harmful factor before it can cause damage.

Inventive Principle:
Principle #10Preliminary action

2Productivity

If fine sand particles are present in cooling air, then cooling air flow is maintained, but cooling effectiveness is reduced due to particle deposition

Engineering Contradiction:
Improvecooling air flowVSAvoidcooling effectiveness
Core Design Contradiction:
ProductivityVSReliability

Solution Approach 1:

The particle separator extracts and removes sand particles from the cooling air stream while allowing the cooled air to continue flowing to the turbine components. This separation process maintains the cooling air flow productivity while eliminating the harmful particles that would reduce cooling effectiveness, thus resolving the contradiction.

Inventive Principle:
Principle #2Taking out (Extraction)

3Object-affected harmful factors

If particle separator is added to remove particles from cooling air, then particle accumulation is reduced, but device complexity increases

Engineering Contradiction:
Improveparticle accumulationVSAvoidcooling system complexity
Core Design Contradiction:
Object-affected harmful factorsVSDevice complexity

Solution Approach 1:

The particle separator utilizes pneumatic principles where centrifugal force generated by swirling flow separates particles from the air stream without moving mechanical parts. This passive pneumatic separation mechanism reduces device complexity compared to active mechanical separation systems, while still effectively reducing particle accumulation in the cooling air.

Inventive Principle:
Principle #29Pneumatics and hydraulics

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

The system effectively reduces particle accumulation in turbine components, improving cooling effectiveness and extending the operational lifespan of engine components by minimizing particle ingestion and deposition, thus enhancing engine durability and performance.

Implementation Method 1

a first particle separator for separating the fluid stream into a reduced-particle stream and a particle-laden stream

Methodology Applied
Scientific EffectCentrifugal separation: Centrifugal Separation

Implementation Method 2

a particle remover... having a return outlet emitting a second reduced-particle stream from the particle-laden stream

Methodology Applied
Scientific EffectParticle removal: Filter (physical)

Data Source

PatentUS10036319B2Separator assembly for a gas turbine engine
Publication Date: 2018.07.31 GENERAL ELECTRIC CO
  • US10036319B2 patent drawing
  • US10036319B2 patent drawing
  • US10036319B2 patent drawing

AI summary

A separator assembly for removing entrained particles from a fluid stream passing through a gas turbine engine includes a first particle separator for separating the fluid stream into a reduced-particle stream and a particle-laden stream, and emitting the particle-laden stream through a scavenge outlet. Another particle remover is fluidly coupled to the scavenge outlet to remove more particles from the air stream.