Turbine Engine Inducer Assembly With Centrifugal Cooling-Air Separation

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Solution Overview

Problem

Particles such as dirt, dust, and other contaminants in the cooling air of turbine engines clog or obstruct the flow passages and surfaces of turbine blades, reducing the lifespan and operational time of the engine, particularly in environments with significant airborne particles.

Innovation Solution

Incorporation of particle separators, including centrifugal and inertial separators, into the bypass cooling circuit of turbine engines to remove contaminants from the cooling air before it reaches the hot portions of the engine, using a combination of centrifugal, gravitational, and inertial forces to separate particles from the cooling fluid stream.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Temperature

If cooling air is ducted from compressors to turbine blades, then cooling efficiency is improved, but particle accumulation in flow passages increases

Engineering Contradiction:
Improveturbine blade coolingVSAvoidparticle accumulation
Core Design Contradiction:
TemperatureVSObject-affected harmful factors

Solution Approach 1:

The particle separator is installed in the bypass cooling circuit upstream of the turbine blades to remove particles from the cooling air before it enters the turbine flow passages. This preliminary action prevents particle accumulation while maintaining the cooling function, resolving the technical contradiction between cooling efficiency and particle contamination.

Inventive Principle:
Principle #10Preliminary action

2Power

If turbine engines operate in harsh environments with airborne particles, then engine thrust and power are maintained, but operational time and lifespan are reduced

Engineering Contradiction:
Improveengine thrustVSAvoidoperational time
Core Design Contradiction:
PowerVSDuration of action of moving object

Solution Approach 1:

The particle separator performs preliminary removal of particles from the cooling air before it contacts the turbine blades, preventing clogging and damage that would reduce operational time. This allows the engine to maintain full power output in harsh environments while extending the duration between maintenance intervals.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The particle separator acts as an intermediary device in the cooling circuit, intercepting and removing harmful particles from the cooling air stream before they can reach and damage the turbine blades. This mediator protects the engine components while allowing continued operation in particle-laden environments.

Inventive Principle:
Principle #24Intermediary (Mediator)

3Object-affected harmful factors

If particle separators are added to the bypass cooling circuit, then particle removal is improved, but device complexity increases

Engineering Contradiction:
Improveparticle concentrationVSAvoidcooling circuit structure
Core Design Contradiction:
Object-affected harmful factorsVSDevice complexity

Solution Approach 1:

The particle separator is designed to be integrated into the existing bypass cooling circuit, allowing the same cooling air stream to serve both cooling and particle removal functions. This multi-functional approach reduces the need for separate systems and minimizes the increase in device complexity while achieving effective particle removal.

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

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

Enhances the cooling efficiency of turbine engines by reducing particle accumulation, thereby extending the operational time and lifespan of the engine components and maintaining performance in harsh environments.

Implementation Method 1

a centrifugal separator that uses centrifugal force to separate particles from the cooling fluid stream

Methodology Applied
Scientific EffectCentrifugal force: Centrifugal Force

Implementation Method 2

an inertial separator that uses inertial forces to separate particles from the cooling fluid stream

Methodology Applied
Scientific EffectInertial force: Inertia

Implementation Method 3

a gravitational separator that uses gravitational force to separate particles from the cooling fluid stream

Methodology Applied
Scientific EffectGravitational force: Gravitation

Data Source

PatentUS20250339801A1Inducer assembly for a turbine engine
Publication Date: 2025.11.06 GENERAL ELECTRIC CO
  • US20250339801A1 patent drawing
  • US20250339801A1 patent drawing
  • US20250339801A1 patent drawing

AI summary

A turbine engine having a compressor section, a combustor section, a turbine section, and a rotatable drive shaft. A bypass conduit couples the compressor section to the turbine section. At least one centrifugal separator is fluidly coupled to the bypass stream, where the at least one centrifugal separator includes a body, a center body, a separator inlet, and a separator outlet fluidly coupled with the turbine section to output a reduced-particle stream that is provided to the turbine section for cooling. The centrifugal separator includes an angular velocity increaser, a flow splitter, a first outlet passage defined by an inner annular wall that receives the reduced-particle stream, and an angular velocity decreaser located downstream of the flow splitter. A second outlet passage receives the concentrated-particle stream.