Turbine Disk Support Plate Segmented Fixing Blocks

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Solution Overview

Problem

Existing turbine apparatuses face challenges in easily integrating a support plate onto a turbine disk, which complicates the assembly and stability of blades.

Innovation Solution

A turbine apparatus design featuring a turbine disk with protrusions and latching portions, supported by first and second fixing blocks, where the second fixing block's space width is narrower than the first, allowing for secure engagement and easy installation of a support plate.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Ease of operation

If a support plate is provided on a turbine disk using conventional methods, then the blades can be supported, but the assembly process becomes complicated and difficult to install

Engineering Contradiction:
Improveease of installationVSAvoidassembly complexity
Core Design Contradiction:
Ease of operationVSDevice complexity

Solution Approach 1:

The support plate is divided into multiple segments corresponding to different radial positions. Each segment has protrusions that engage with recesses in the turbine disk, allowing the support plate to be assembled in a modular fashion rather than as a single complex piece, thereby simplifying the installation process

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

Protrusions and recesses serve as intermediary elements that facilitate the connection between the support plate segments and the turbine disk. These intermediate features enable easy alignment and secure attachment without requiring complex fastening mechanisms

Inventive Principle:
Principle #24Intermediary (Mediator)

2Stability of the object's composition

If the support plate is securely fixed to prevent movement and rotation, then blade stability is improved, but the fixing mechanism becomes more complex

Engineering Contradiction:
Improvesupport plate stabilityVSAvoidfixing mechanism complexity
Core Design Contradiction:
Stability of the object's compositionVSDevice complexity

Solution Approach 1:

The protrusions on the support plate segments are designed with asymmetric shapes that correspond to asymmetric recesses in the turbine disk. This asymmetric geometry provides inherent anti-rotation capability, as the protrusions can only engage with their matching recesses in a specific orientation, thereby preventing rotation without requiring additional locking mechanisms

Inventive Principle:
Principle #4Asymmetry

Solution Approach 2:

Instead of using conventional fastening methods that require bolts or clips to prevent rotation, the design inverts the approach by using the protrusion-recess geometry itself to provide both the connection and the anti-rotation function. The shape of the protrusions is specifically designed to physically block rotation in the opposite direction

Inventive Principle:
Principle #13The other way round (Inversion)

Data Source

PatentUS10563526B2Turbine apparatus
Publication Date: 2020.02.18 HANWHA AEROSPACE CO LTD
  • US10563526B2 patent drawing
  • US10563526B2 patent drawing
  • US10563526B2 patent drawing

AI summary

According to an aspect of the present invention, a turbine apparatus includes a shaft; a turbine disk provided on the shaft and having a plurality of protrusions protruding in a direction of the shaft; blades provided on the turbine disk; a support plate provided on the turbine disk and having a plurality of latching portions engaged with the plurality of protrusions; a plurality of first fixing blocks located between the plurality of latching portions; and a second fixing block located between the plurality of protrusions and fixed to the plurality of first fixing blocks, wherein a width of a space where the second fixing block is located, from among spaces between the plurality of protrusions, is less than a width of a space where the plurality of first fixing blocks are located, from among spaces between the plurality of latching portions.