Composite Shell for Turbine Vane Geometry Modification

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Solution Overview

Problem

Hydraulic turbines face significant efficiency losses due to flow misalignment of water with stay vanes, which requires substantial time and costs to correct, involving heavy parts and safety concerns in confined spaces.

Innovation Solution

An apparatus and method using a composite material shell with a polymer casting to modify the geometry of stay vanes, allowing for attachment to existing turbines without dismantling, using a shell assembly with a fiber and polymeric material, and injecting a polymer casting to correct flow misalignment.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Manufacturing precision

If traditional methods are used to correct flow misalignment of stay vanes, then the misalignment can be corrected, but substantial time and costs are required, and heavy parts must be manipulated in confined spaces

Engineering Contradiction:
Improveflow misalignment correctionVSAvoidcorrection time
Core Design Contradiction:
Manufacturing precisionVSLoss of time

Solution Approach 1:

The patent changes the material parameter from traditional heavy metal to composite material, which fundamentally alters the weight characteristic. This enables the correction process to be performed with lighter materials, reducing manipulation difficulty and installation time while maintaining the geometric correction capability for flow misalignment

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The patent employs composite materials consisting of a shell and core with different material properties. The shell provides structural integrity while the core provides bulk, creating a lightweight yet strong correction component that can be easily installed in confined spaces without sacrificing correction precision

Inventive Principle:
Principle #40Composite materials

2Manufacturing precision

If traditional methods are used to correct flow misalignment of stay vanes, then the misalignment can be corrected, but substantial time and costs are required, and safety and handling issues arise

Engineering Contradiction:
Improveflow misalignment correctionVSAvoidhandling ease
Core Design Contradiction:
Manufacturing precisionVSEase of operation

Solution Approach 1:

By changing the material parameter from heavy metal to composite material, the weight is significantly reduced. This improves ease of operation by making the correction components easier to handle, transport, and install in confined turbine spaces, while eliminating safety concerns associated with heavy part manipulation

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The correction device is segmented into a shell and core structure, allowing for modular assembly and handling. This segmentation enables easier manipulation during installation and maintenance operations compared to monolithic heavy metal corrections

Inventive Principle:
Principle #1Segmentation

3Strength

If heavy metal components are used for stay vane correction, then structural strength is provided, but safety and handling issues increase

Engineering Contradiction:
Improvestructural strengthVSAvoidhandling ease
Core Design Contradiction:
StrengthVSEase of operation

Solution Approach 1:

The composite structure combines a shell and core materials that together provide the necessary structural strength while significantly reducing weight. The shell provides structural integrity and the core provides bulk support, achieving strength requirements without the handling difficulties of heavy metal components

Inventive Principle:
Principle #40Composite materials

Solution Approach 2:

Changing from metal to composite material parameters fundamentally alters the strength-to-weight ratio. The composite material achieves comparable structural strength through optimized material composition and structure, enabling easier handling while maintaining the mechanical strength required for turbine operation

Inventive Principle:
Principle #35Parameter changes

Data Source

PatentUS10704527B2Apparatus and method for modifying a geometry of a turbine part
Publication Date: 2020.07.07 GE RENEWABLE TECH
  • US10704527B2 patent drawing
  • US10704527B2 patent drawing
  • US10704527B2 patent drawing

AI summary

An apparatus is provided for modifying the geometry of at least one part of a turbine, which can include a shell assembly that includes an outer shell that is shaped to modify the shape of a pre-existing element of a turbine. The outer shell of the shell assembly can be composed of a fiber-reinforced polymeric material and can at least partially define an inner cavity. The outer shell can be bonded to a structure to modify the geometrical shape of that structure. Thereafter, a polymer casting can be injected into the inner cavity via at least one injection port attached to the shell assembly. In some embodiments, one or more stiffeners and/or a core can be positioned within the inner cavity to help improve the bonding of the polymer casting to the shell and/or improve a structural property of the apparatus.