Adjustable Guide Vane Fixing Device for Turbomachines

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Solution Overview

Problem

Existing solutions for fixing the position of adjustable guide vane rows in turbomachines are not robust enough to withstand field conditions and lack flexibility in adjusting the position of synchronizing rings and guide vanes.

Innovation Solution

A device comprising a support arm, ring fixing sets with holding members and fixing bolts, where the fixing bolts are adjustable to securely engage with radial recesses or through-holes of synchronizing rings, allowing for variable positioning and angle adjustment of the guide vanes, and the support arm is securely fastened to the turbomachine.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If existing solutions are used to fix the position of adjustable guide vane rows, then the position can be fixed, but the solution is not robust enough to withstand field conditions and lacks flexibility in adjusting the position of synchronizing rings and guide vanes

Engineering Contradiction:
Improverobustness to withstand field conditionsVSAvoidflexibility in adjusting position
Core Design Contradiction:
ReliabilityVSAdaptability or versatility

Solution Approach 1:

The fixing device incorporates adjustable components including the support arm with adjustable angle relative to the turbine axis, the holding member with adjustable angle relative to the support arm, and the fixing bolt with adjustable position along both the longitudinal direction of the holding member and the longitudinal axis of the fixing bolt. These dynamic adjustment capabilities allow the device to adapt to different field conditions while maintaining reliable fixation of the synchronizing ring and guide vanes

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The device enables multiple parameter adjustments: the angle of the support arm relative to the turbine axis, the angle of the holding member relative to the support arm, and the position of the fixing bolt along the longitudinal direction of the holding member and its own longitudinal axis. By changing these parameters, the device achieves both reliability in fixation and flexibility in adaptation to various field conditions and turbomachine configurations

Inventive Principle:
Principle #35Parameter changes

2Reliability

If the fixing device provides robust fixation for field conditions, then reliability improves, but device complexity increases due to multiple adjustable components

Engineering Contradiction:
Improverobustness to withstand field conditionsVSAvoidstructure with multiple adjustable components
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The fixing device is divided into distinct functional segments: the support arm for positioning relative to the turbine, the holding member for securing the synchronizing ring, and the fixing bolt for final fixation. Each segment has specific adjustment capabilities, allowing the complex functionality to be distributed across modular components that can be independently adjusted and maintained

Inventive Principle:
Principle #1Segmentation

3Adaptability or versatility

If multiple adjustment capabilities are provided for flexibility, then adaptability improves, but ease of operation decreases due to multiple adjustment steps

Engineering Contradiction:
Improveflexibility in adjusting positionVSAvoidease of adjustment
Core Design Contradiction:
Adaptability or versatilityVSEase of operation

Solution Approach 1:

The device allows preliminary positioning through the support arm angle adjustment relative to the turbine axis, followed by securing the synchronizing ring through the holding member angle adjustment. The fixing bolt is then positioned along the longitudinal direction of the holding member and its own axis to lock the configuration. This sequential preliminary action approach breaks down complex adjustments into manageable steps, improving ease of operation while maintaining adaptability

Inventive Principle:
Principle #10Preliminary action

Data Source

PatentUS11988101B2Device for fixing position of adjustable rows of guide vanes of turbomachine
Publication Date: 2024.05.21 GE INFRASTRUCTURE TECH LLC
  • US11988101B2 patent drawing
  • US11988101B2 patent drawing
  • US11988101B2 patent drawing

AI summary

A device for fixing the position of adjustable vane rows of a turbomachine is disclosed. The device is intended for use with a turbomachine in which the guide vanes of a row of adjustable guide vanes are coupled together by a synchronizing ring. The device includes a support arm and at least one ring fixing set including a holding member and a fixing bolt. The fixing bolt is provided and dimensioned to engage an opening at the circumference of the synchronizing ring and to fix the position of the synchronizing ring and thus of the adjustable guide vanes coupled to the synchronizing ring.