Selective Turbine Cleaning via High-Viscosity Gel Composition

Resolve Bottlenecks,
Find Innovative Solutions
Generate Solutions

Solution Overview

Problem

Conventional cleaning methods for turbine engine components are inefficient and costly, often requiring multiple cycles, large volumes of cleaning fluid, and manual application, which can be environmentally and health hazardous, and struggle with selective cleaning of components with multiple materials or localized deposits.

Innovation Solution

A system and method using a high-viscosity cleaning composition that selectively contacts and removes engine deposits from turbine engine components, minimizing exposure to incompatible materials and allowing for efficient, targeted cleaning without excessive removal of the base metal, through a cleaning apparatus with a manifold assembly for circulation and recirculation of the cleaning composition.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If conventional cleaning methods are used, then cleaning effectiveness is achieved, but cleaning cost and time increase due to multiple cycles and large volumes of cleaning fluid

Engineering Contradiction:
Improvecleaning effectivenessVSAvoidcleaning cycle time
Core Design Contradiction:
ReliabilityVSLoss of time

Solution Approach 1:

The patent changes the physical parameter of the cleaning composition by increasing its viscosity to a gel-like state. This parameter change allows the cleaning composition to remain in contact with the component surface longer without running off, thereby achieving effective cleaning in a single cycle rather than requiring multiple cycles with conventional low-viscosity cleaners

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The high-viscosity cleaning composition maintains continuous contact with the component surface throughout the cleaning process. The gel structure ensures sustained exposure of the active cleaning agents to the deposits without interruption from fluid flow or runoff, enabling complete cleaning in one application

Inventive Principle:
Principle #20Continuity of useful action

2Reliability

If conventional cleaning methods are used, then cleaning effectiveness is achieved, but environmental and health hazards increase due to large volumes of cleaning fluid

Engineering Contradiction:
Improvecleaning effectivenessVSAvoidenvironmental and health hazards
Core Design Contradiction:
ReliabilityVSObject-affected harmful factors

Solution Approach 1:

By changing the viscosity parameter to create a gel-like cleaning composition, the patent reduces the total volume of cleaning fluid required. The thickened formulation stays localized on the component surface, minimizing spillage, evaporation, and disposal requirements, thereby reducing environmental and health hazards associated with large volumes of chemical cleaners

Inventive Principle:
Principle #35Parameter changes

3Manufacturing precision

If selective cleaning is required for components with multiple materials or localized deposits, then cleaning precision is improved, but process complexity increases due to additional steps

Engineering Contradiction:
Improvecleaning selectivityVSAvoidcleaning process complexity
Core Design Contradiction:
Manufacturing precisionVSDevice complexity

Solution Approach 1:

The high-viscosity gel cleaning composition enables local quality control by allowing precise application to specific areas of the component. The gel structure prevents the cleaner from flowing into areas where cleaning is not desired, naturally providing selectivity without requiring complex masking or disassembly procedures

Inventive Principle:
Principle #3Local quality

Solution Approach 2:

The patent introduces a thickening agent as an intermediary substance that modifies the physical properties of the cleaning composition. This intermediary creates a gel structure that acts as a self-limiting medium, confining the cleaning action to areas where the gel is applied while preventing unwanted contact with incompatible materials

Inventive Principle:
Principle #24Intermediary (Mediator)

4Reliability

If cleaning composition contact area is limited, then material compatibility is improved, but cleaning efficiency decreases without additional steps

Engineering Contradiction:
Improvematerial compatibilityVSAvoidcleaning efficiency
Core Design Contradiction:
ReliabilityVSProductivity

Solution Approach 1:

By changing the viscosity parameter to create a gel formulation, the patent enables the cleaning composition to be applied in a controlled, localized manner while maintaining cleaning efficiency. The gel structure allows the active ingredients to remain concentrated at the application site, providing both material compatibility through limited contact and high productivity through effective localized cleaning

Inventive Principle:
Principle #35Parameter changes

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 effective and efficient selective cleaning of turbine engine components, reducing corrosion, minimizing human contact, and allowing for the reuse and safe collection of the cleaning composition, while maintaining the integrity of the underlying metal.

Implementation Method 1

cleaning composition having a viscosity of at least 10 4 centipoises... selectively contacting the cleaning composition with a surface of the turbine engine component... at least partial removal of the oxide

Methodology Applied
Scientific EffectChemical reaction: Chemical Bonding

Data Source

PatentEP3991862B1System and methods for selective cleaning of turbine engine components
Publication Date: 2023.11.08 GENERAL ELECTRIC CO
  • EP3991862B1 patent drawingFigure 1A
  • EP3991862B1 patent drawingFigure 1B
  • EP3991862B1 patent drawingFigure 2

AI summary

System (200) for selectively contacting a cleaning composition (10) with a surface of a turbine engine component is presented. The system includes a cleaning apparatus (210) and a manifold assembly (220). The cleaning apparatus (210) includes an upper portion (211) and a lower portion (212) defining a cleaning chamber (213) configured to allow selective contact between the cleaning composition (10) and a surface of the first portion of the turbine engine component. The upper portion (211) includes a plurality of fill holes (201) in fluid communication with the cleaning chamber (213), and the lower portion (212) includes a plurality of drain holes (202) in fluid communication with the cleaning chamber (213). The manifold assembly (220) is configured to selectively circulate the cleaning composition (10) from a reservoir (250) to the cleaning chamber (213) via the plurality of fill holes (201), and recirculate the cleaning composition from the cleaning chamber (213) to the reservoir (250) via the plurality of drain holes (202). Methods for selectively cleaning a turbine engine component is also presented.