Axial Compressor Rotor Repair Using Segmented Shaft Replacement

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Solution Overview

Problem

The existing methods for repairing a gas turbine's multi-stage axial compressor rotor are burdensome, requiring the complete removal and replacement of the shaft to replace damaged bladed discs, which is time-consuming and costly, and necessitates the use of expensive, high-temperature-resistant materials like stainless steel.

Innovation Solution

A method involving cutting the rotor shaft to separate the damaged disc section, using new discs with solid hubs and a new solid shaft section, and securing them with anchor bolts, allowing for easier replacement and reducing the need for high-temperature materials.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Ease of operation

If the last bladed discs are replaced by heating to increase internal diameter and reduce interference, then the discs can be removed from the shaft, but the heat required would irreparably damage both the discs and the shaft

Engineering Contradiction:
Improveease of disc removalVSAvoidintegrity of shaft and discs
Core Design Contradiction:
Ease of operationVSReliability

Solution Approach 1:

The shaft is divided into two separate parts: the remaining shaft portion that retains usable discs and a new end shaft portion that will accommodate the replacement discs. This segmentation allows the replacement operation to be localized without affecting the integrity of the main shaft and usable discs.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The problematic interference fit connection is extracted and replaced by an alternative connection method. Instead of relying on thermal expansion for removal, the discs are secured using anchor bolts that pass through the new end shaft portion and into the remaining shaft, eliminating the need for high-temperature heating that would cause damage.

Inventive Principle:
Principle #2Taking out (Extraction)

2Ease of repair

If material is removed from the shaft to allow disc removal, then the discs can be replaced, but the shaft becomes unusable and must be completely rebuilt

Engineering Contradiction:
Improveease of disc replacementVSAvoidcomplexity of shaft reconstruction
Core Design Contradiction:
Ease of repairVSDevice complexity

Solution Approach 1:

The shaft is segmented into a reusable remaining portion and a replaceable new end portion. This allows the majority of the shaft with intact discs to be preserved and reused, while only the end portion needing disc accommodation is manufactured anew and attached.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

Instead of discarding the entire shaft when disc replacement is needed, the method recovers and reuses the remaining shaft portion that still has functional discs. Only the minimal necessary end portion is discarded and replaced, significantly reducing material waste and repair complexity.

Inventive Principle:
Principle #34Discarding and recovering

3Reliability

If stainless steel discs are used to resist high temperatures and maintain interference fit, then the discs can withstand operating conditions, but the cost increases and hydrogen embrittlement occurs

Engineering Contradiction:
Improveresistance to high temperatureVSAvoidcost and material suitability
Core Design Contradiction:
ReliabilityVSEase of manufacture

Solution Approach 1:

The thermal interference fit mechanism is replaced with a mechanical fastening system using anchor bolts. This substitution eliminates the need for discs to maintain interference through thermal expansion, allowing the use of cheaper micro-alloyed steel that is not subject to hydrogen embrittlement while still providing secure attachment through the bolt mechanism.

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

Data Source

PatentUS11174733B2Method for repairing a rotor of a multi-stage axial compressor of a gas turbine
Publication Date: 2021.11.16 ETHOSENERGY ITAL SPA
  • US11174733B2 patent drawing
  • US11174733B2 patent drawing

AI summary

The method comprises the steps of: a) cutting the shaft of the rotor at a section plane perpendicular to the axis of rotation of the shaft so as to separate the end portion of the shaft on which the bladed discs to be replaced are mounted from the remaining portion of the shaft; b) providing, for each bladed disc to be replaced, a corresponding new bladed disc with a respective hub having a solid cross-section; c) providing a new end portion of the shaft with a solid cross-section; and d) clamping the new bladed discs between the remaining portion of the shaft and the new end portion of the shaft, securing them to the remaining portion of the shaft by anchor bolts.