Pinned Platform for Gas Turbine Blade Attachment

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Solution Overview

Problem

Gas turbine engine turbine wheels face design challenges in coupling composite blades with metallic disks due to heat from combustion products, requiring innovative solutions to enhance durability and stress distribution.

Innovation Solution

A multi-piece disk assembly with a blade and platform system, featuring a dovetail-shaped root and airfoil, and a pin system that couples platforms with the disk for rotation, providing a secure and stress-reduced attachment mechanism.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Temperature

If composite blades are coupled with metallic disks in turbine wheels, then the turbine can withstand heat from combustion products, but stress concentration occurs at the blade attachment points

Engineering Contradiction:
Improveheat resistanceVSAvoidstress distribution
Core Design Contradiction:
TemperatureVSStrength

Solution Approach 1:

The disk is divided into multiple segments (first disk segment, second disk segment, third disk segment) that are arranged circumferentially to form a circumferential attachment feature. This segmentation allows the blade root to be distributed across multiple disk segments, reducing stress concentration at any single attachment point while maintaining the ability to withstand high temperatures through the metallic disk structure.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The attachment feature extends in the circumferential direction rather than only axially, creating a three-dimensional attachment structure. The circumferential attachment feature includes multiple disk segments arranged around the circumference, which distributes the blade attachment stresses across a larger circumferential area, reducing stress concentration while maintaining thermal resistance.

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

2Reliability

If larger attachment features are used to reduce stress, then durability improves, but device complexity increases

Engineering Contradiction:
ImprovedurabilityVSAvoidstructure complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The complex attachment structure is achieved through segmentation of the disk into multiple segments that can be manufactured separately and then assembled. The circumferential attachment feature is formed by arranging first, second, and third disk segments circumferentially, which allows for modular manufacturing and assembly while achieving the desired stress distribution and durability.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The circumferential attachment feature serves multiple functions: it provides stress distribution across multiple disk segments, maintains structural integrity under centrifugal loads, and enables thermal resistance through the metallic disk material. This multi-functional design achieves durability without proportionally increasing complexity.

Inventive Principle:
Principle #6Universality (Multi-functionality)

3Strength

If a multi-piece disk structure is used with circumferential attachment, then stress distribution improves, but manufacturing complexity increases

Engineering Contradiction:
Improvestress distributionVSAvoidmanufacturing complexity
Core Design Contradiction:
StrengthVSEase of manufacture

Solution Approach 1:

The disk is segmented into multiple manufacturable components (first disk segment, second disk segment, third disk segment) that can be produced using standard manufacturing processes. These segments are then assembled to form the complete circumferential attachment feature, allowing for specialized manufacturing of each segment while achieving superior stress distribution in the final assembly.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The disk segments are prepared in advance with specific geometries and attachment features that facilitate their circumferential arrangement. The blade root is designed with a dovetail shape that can be preliminarily fitted into the circumferential attachment feature, simplifying the final assembly process while ensuring proper stress distribution.

Inventive Principle:
Principle #10Preliminary action

Data Source

PatentUS11156111B2Pinned platform for blade with circumferential attachment
Publication Date: 2021.10.26 ROLLS ROYCE NORTH AMERICAN TECHNOLOGIES INC
  • US11156111B2 patent drawing
  • US11156111B2 patent drawing
  • US11156111B2 patent drawing

AI summary

A wheel assembly for a gas turbine engine includes a disk, a plurality of blades, and a platform system that includes a plurality of platforms and pins. The disk is configured to rotate about an axis during operation of the gas turbine engine. The blades each include a circumferentially extending root received in the disk and an airfoil that extends radially away from the root. The platforms are arranged around the wheel to define a flow path of the gas turbine engine and the pins extend into the platforms and the disk to couple the platforms with the disk.