Turbine Blade-Anchored Service Tool for In-Situ Flowpath Maintenance

Resolve Bottlenecks,
Find Innovative Solutions
Generate Solutions

Solution Overview

Problem

Existing rotary machine inspection and repair methods, such as borescope inspections, struggle to access all locations within the machine, particularly non-rotating components, and often require partial disassembly for maintenance, leading to increased downtime and costs due to limited accessibility and unmitigated damage detection.

Innovation Solution

An insertion apparatus and service apparatus system that allows precise positioning of the service apparatus within the primary flowpath of rotary machines, using a steering interface and guide apparatus to access difficult-to-reach areas, enabling inspection and repair of rotating and stationary components without full disassembly.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Ease of operation

If borescope inspection is used to inspect rotary machine components, then inspection capability is provided, but accessibility to all locations is limited

Engineering Contradiction:
Improveinspection accessibilityVSAvoidinspection completeness
Core Design Contradiction:
Ease of operationVSReliability

Solution Approach 1:

The service apparatus is divided into multiple functional modules including inspection module, repair module, and positioning module that can be independently operated or combined, allowing flexible access to different locations within the rotary machine

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The service apparatus acts as an intermediary tool that bridges the gap between external inspection equipment and internal hard-to-reach components, providing both inspection and repair capabilities in locations previously inaccessible to borescopes

Inventive Principle:
Principle #24Intermediary (Mediator)

2Ease of repair

If rotary machine is disassembled for repair, then component repair is enabled, but maintenance time and downtime increase

Engineering Contradiction:
Improvecomponent repairabilityVSAvoidmaintenance downtime
Core Design Contradiction:
Ease of repairVSLoss of time

Solution Approach 1:

The service apparatus enables self-service repair capabilities by providing integrated inspection, repair, and positioning functions that can be operated within the rotary machine without complete disassembly, allowing maintenance personnel to perform repairs in-situ

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

The service apparatus combines multiple functions including inspection, repair, and positioning into a single universal tool that can service multiple components across different locations, eliminating the need for separate disassembly and repair procedures

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

3Measurement precision

If damage is detected during inspection, then component condition is assessed, but damage mitigation is delayed until disassembly

Engineering Contradiction:
Improvedamage detection accuracyVSAvoiddamage mitigation delay
Core Design Contradiction:
Measurement precisionVSLoss of time

Solution Approach 1:

The service apparatus performs preliminary repair actions immediately after damage detection by providing integrated repair modules that can address detected issues in-situ without waiting for disassembly, thus mitigating damage progression

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The service apparatus maintains continuous useful action by seamlessly transitioning from inspection mode to repair mode within the same operational session, eliminating the interruption and delay that occurs when damage must wait for scheduled disassembly

Inventive Principle:
Principle #20Continuity of useful action

Data Source

PatentEP3663515B1Service apparatus for use with a turbine assembly
Publication Date: 2025.03.26 GENERAL ELECTRIC CO
  • EP3663515B1 patent drawingFigure 1
  • EP3663515B1 patent drawingFigure 2~3
  • EP3663515B1 patent drawingFigure 4

AI summary

A system for use in maintaining a turbine assembly (100) includes a plurality of blades (122, 125) and a plurality of vanes (123, 124). The system includes an insertion apparatus (128) including an insertion end (130), a steering end (132) opposite the insertion end, and a body (162) extending from the insertion end to the steering end. The insertion end is positionable proximate at least one blade of the plurality of blades using a steering interface (138). The system also includes a service apparatus (101) for use in maintaining the turbine assembly. The service apparatus includes at least one maintenance device (180) and an anchoring feature (178). The service apparatus is proximate the insertion end of the insertion apparatus and is positionable in a plurality of orientations via the steering interface. The anchoring feature is configured to releasably couple the service apparatus to at least one blade of the plurality of blades.