Off-Center Cooling Bore Reaming for Gas Turbine Rotors

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Solution Overview

Problem

Gas turbine engines face issues with material creep and cracking due to thermal stresses, which can be exacerbated by reaming cooling bores to increase diameter, leading to reduced efficiency and requiring extensive downtime and transport costs for maintenance.

Innovation Solution

A cooling bore guide system comprising a cutter guide and guide lock allows for off-center reaming of rotor cooling bores without removing the rotor from service, using a semicircular cutter guide and guide lock to create an enlarged portion while maintaining efficiency.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If cooling bores are reamed to increase diameter to address cracking, then rotor reliability is improved, but gas turbine efficiency deteriorates due to excess cooling air passage

Engineering Contradiction:
Improverotor reliabilityVSAvoidgas turbine efficiency
Core Design Contradiction:
ReliabilityVSLoss of energy

Solution Approach 1:

The patent applies local quality by creating an enlarged portion only at specific locations where cracks are detected in the cooling bore, rather than uniformly enlarging the entire bore. This allows targeted crack remediation while preserving the original bore dimensions in other areas, thus maintaining cooling efficiency and avoiding excess cooling air passage.

Inventive Principle:
Principle #3Local quality

Solution Approach 2:

The cooling bore is segmented into different zones: the original bore portion and the locally enlarged portion. The enlargement is applied segmentally only where needed (where cracks are present) rather than to the entire bore, allowing selective repair that balances reliability improvement with efficiency preservation.

Inventive Principle:
Principle #1Segmentation

2Reliability

If standard reaming methods are used to enlarge cooling bores, then cracking issues are addressed, but manufacturing complexity increases due to limited space and requirement for specialized workshops

Engineering Contradiction:
Improvecrack remediationVSAvoidmanufacturing complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The patent transitions from standard axial reaming to off-center reaming by positioning the reaming tool at an offset location. This dimensional change allows the creation of an enlarged portion within the existing bore space without requiring external specialized equipment or rotor removal, simplifying the manufacturing process.

Inventive Principle:
Principle #17Another dimension (Dimensionality change)

Solution Approach 2:

A guide tool is introduced as an intermediary device that facilitates the off-center reaming operation. The guide tool enables precise positioning of the reaming tool within the constrained space of the cooling bore, making the complex off-center enlargement operation feasible without specialized workshop equipment.

Inventive Principle:
Principle #24Intermediary (Mediator)

3Reliability

If rotor is removed from service for cooling bore reaming, then crack repair is possible, but loss of time increases due to extensive downtime and transport requirements

Engineering Contradiction:
Improvecrack repairVSAvoiddowntime
Core Design Contradiction:
ReliabilityVSLoss of time

Solution Approach 1:

The patent enables self-service repair by providing a complete off-center reaming system that can be applied to the rotor while it remains installed in the gas turbine engine. The guide tool and reaming tool are designed to access and repair cooling bores in-situ, eliminating the need for rotor removal and transport to specialized workshops.

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

The guide tool is designed with pre-positioned features that align with existing rotor structures, allowing rapid setup and immediate commencement of the reaming operation. This preliminary preparation enables crack repair to be performed quickly during scheduled maintenance without requiring extensive downtime or complex installation procedures.

Inventive Principle:
Principle #10Preliminary action

Data Source

PatentUS20240278344A1Out of center cooling bore drilling for gas turbine rotor
Publication Date: 2024.08.22 GE INFRASTRUCTURE TECH LLC
  • US20240278344A1 patent drawing
  • US20240278344A1 patent drawing
  • US20240278344A1 patent drawing

AI summary

A cooling bore guide for reaming an enlarged portion into a cooling bore of a rotor. The cooling bore guide may include a cutter guide for insertion into the cooling bore and a guide lock for insertion into an adjacent cooling bore.