Additive Rotor Support Structure for Thermal Stress Management

Resolve Bottlenecks,
Find Innovative Solutions
Generate Solutions

Solution Overview

Problem

Existing rotating structures in gas turbine engines lack improvements in design and manufacturing methods, particularly in integrating a shaft, bladed rotor, and support structure efficiently.

Innovation Solution

The method involves forming a monolithic body using additive manufacturing, which includes a shaft, a bladed rotor, and a support structure with a plurality of channels and baffles arranged circumferentially. This support structure is designed to provide structural integrity and thermal management.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Strength

If traditional manufacturing methods are used for rotating structures, then manufacturing process is simpler, but structural integrity and thermal management are insufficient

Engineering Contradiction:
Improvestructural integrityVSAvoidmanufacturing complexity
Core Design Contradiction:
StrengthVSEase of manufacture

Solution Approach 1:

The patent combines the shaft, bladed rotor, and support structure into a single monolithic body formed by additive manufacturing. This integration eliminates the need for separate manufacturing and assembly processes for these components, thereby improving structural integrity through unified construction while managing manufacturing complexity through advanced fabrication techniques.

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The support structure is formed within the monolithic body containing the shaft and bladed rotor, with channels and baffles nested within the support structure. This nested configuration allows multiple functional elements to be integrated efficiently, enhancing structural integrity and thermal management capabilities without proportionally increasing external dimensions.

Inventive Principle:
Principle #7Nested doll (Nesting)

2Reliability

If additive manufacturing is used to form monolithic body, then structural integrity and thermal management improve, but manufacturing complexity increases

Engineering Contradiction:
Improvethermal management effectivenessVSAvoidmanufacturing process complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The support structure incorporates channels and baffles with specific geometries optimized for thermal management. The channels are arranged with particular orientations and dimensions, and baffles are positioned at specific locations, creating localized functional regions within the monolithic body that enhance thermal management effectiveness while maintaining overall structural integrity.

Inventive Principle:
Principle #3Local quality

3Temperature

If channels and baffles are integrated into support structure, then thermal management improves, but manufacturing precision requirements increase

Engineering Contradiction:
Improvethermal stress managementVSAvoidchannel and baffle geometry precision
Core Design Contradiction:
TemperatureVSManufacturing precision

Solution Approach 1:

The additive manufacturing process enables precise control of geometric parameters for channels and baffles, including dimensions, orientations, and positions. By leveraging the capabilities of additive manufacturing to achieve high dimensional accuracy, the design can incorporate complex channel networks and baffle configurations that effectively manage thermal stresses while meeting precision requirements.

Inventive Principle:
Principle #35Parameter changes

Data Source

PatentUS12253093B2Support structure for forming turbine engine rotating structure
Publication Date: 2025.03.18 RTX CORP
  • US12253093B2 patent drawing
  • US12253093B2 patent drawing
  • US12253093B2 patent drawing

AI summary

A method of manufacturing is provided. During this method, a body is formed using an additive manufacturing process. The body includes a shaft, a bladed rotor and a support structure. The shaft projects axially along an axis out from the bladed rotor. The support structure projects radially out from the shaft and axially to the bladed rotor. The support structure includes a plurality of channels arranged circumferentially about the axis. Each of the channels projects radially into the support structure towards the axis and to a respective channel side. Each of the channels projects axially into the support structure towards the bladed rotor and to a respective channel end.