Inverted Turbulators for Stator-Rotor Gas Leakage Containment

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Solution Overview

Problem

Turbine engines face significant challenges in reducing hot gas leakage from the stator-rotor assembly gaps, leading to energy loss and potential damage to components, with existing solutions like coolant air being costly and inefficient, particularly when compressor systems fail to provide sufficient purge air pressure.

Innovation Solution

The implementation of a pattern of inverted turbulators on the stator or rotor surfaces adjacent to the gaps, which impedes gas flow by creating local vortices that restrict leakage, thereby reducing the need for coolant air and maintaining engine efficiency.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Object-affected harmful factors

If coolant air is used to reduce hot gas leakage, then hot gas leakage is reduced, but energy loss increases due to the cost of diverting compressor air

Engineering Contradiction:
Improvehot gas leakageVSAvoidenergy loss
Core Design Contradiction:
Object-affected harmful factorsVSLoss of energy

Solution Approach 1:

The inverted turbulators create vortices that automatically restrict hot gas leakage through the gap between stator and rotor. The system uses the kinetic energy of the leaking gas itself to generate vortices that contain the flow, eliminating the need for external coolant air supply and its associated energy costs.

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

The invention converts the harmful hot gas leakage flow into a beneficial vortex flow that helps contain the gas. The kinetic energy of the leaking gas is transformed into rotational vortices through the inverted turbulators, which then act to restrict further leakage and protect downstream components.

Inventive Principle:
Principle #22Blessing in disguise (Convert harm into benefit)

2Object-affected harmful factors

If compressor systems are used to provide purge air pressure, then hot gas leakage is reduced, but reliability decreases when compressor systems fail to provide sufficient pressure

Engineering Contradiction:
Improvehot gas leakageVSAvoidreliability
Core Design Contradiction:
Object-affected harmful factorsVSReliability

Solution Approach 1:

The inverted turbulators create vortices that automatically restrict hot gas leakage through the gap between stator and rotor. The system uses the kinetic energy of the leaking gas itself to generate vortices that contain the flow, eliminating the need for external coolant air supply and its associated energy costs.

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

The invention extracts the dependency on compressor purge air systems by implementing a passive vortex generation mechanism. The inverted turbulators directly interact with the leaking gas to create containing vortices, removing the need for active compressor air supply and improving system reliability.

Inventive Principle:
Principle #2Taking out (Extraction)

3Ease of operation

If gaps are maintained at the stator-rotor interface, then ease of operation is improved, but hot gas leakage increases into wheel-space

Engineering Contradiction:
Improveease of operationVSAvoidhot gas leakage
Core Design Contradiction:
Ease of operationVSObject-affected harmful factors

Solution Approach 1:

The inverted turbulators are placed specifically at the stator-rotor interface gap region where hot gas leakage occurs. This localized feature modifies the flow characteristics only in the critical leakage path, allowing gaps to be maintained for operational ease while preventing hot gas intrusion into the wheel-space through vortex containment.

Inventive Principle:
Principle #3Local quality

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 use of inverted turbulators effectively minimizes hot gas leakage into undesirable regions, reducing energy loss and component damage, while maintaining overall engine efficiency and adaptability to various designs, including lower-temperature gases.

Implementation Method 1

The inverted turbulators create vortices that restrict flow through the gap

Methodology Applied
Scientific EffectVortex: Vortex Ring

Data Source

PatentUS7967559B2Stator-rotor assembly having surface feature for enhanced containment of gas flow and related processes
Publication Date: 2011.06.28 GE INFRASTRUCTURE TECH LLC
  • US7967559B2 patent drawing
  • US7967559B2 patent drawing
  • US7967559B2 patent drawing

AI summary

A stator-rotor assembly which includes at least one interface region between the stator and rotor is described. At least one stator or rotor surface in the interface region includes a pattern of inverted turbulators. The inverted turbulators restrict gas flow through a gap between the stator and the rotor. Various turbomachines which can contain such a stator-rotor assembly are also described. The disclosure also discusses methods to restrict gas flow through gaps in a stator-rotor assembly utilizing the inverted turbulators.