Hybrid Alloy Isogrid Engine Case for Thermal Expansion Control

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Solution Overview

Problem

Existing isogrid engine cases in gas turbine engines face challenges in managing thermal expansion and structural integrity due to differential thermal expansion between materials, leading to potential clearance issues and increased stress concentrations.

Innovation Solution

The use of a hybrid alloy structure comprising a titanium alloy for the wall and a dissimilar alloy, such as iron-nickel-cobalt or aluminum, for the ribs, combined with additive manufacturing of ribs to enhance structural integrity and thermal expansion management, and the incorporation of hollow ribs with venting features to mitigate stress concentrations.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If a single alloy material is used for both the wall and ribs in isogrid structures, then manufacturing simplicity is maintained, but differential thermal expansion causes stress concentrations and clearance issues

Engineering Contradiction:
Improvestructural integrityVSAvoidmaterial composition
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The patent applies composite materials by combining titanium alloy for the wall with dissimilar alloy ribs (such as iron-nickel-cobalt or aluminum alloys). This composite construction allows each material to be selected for its optimal properties: titanium provides structural strength and heat resistance for the wall, while the dissimilar alloy ribs provide controlled thermal expansion characteristics. The differential thermal expansion between materials is managed through the specific material selection, reducing stress concentrations and maintaining clearance under thermal conditions.

Inventive Principle:
Principle #40Composite materials

2Reliability

If dissimilar alloys are used for wall and ribs, then thermal expansion management is improved, but manufacturing complexity increases

Engineering Contradiction:
Improvethermal expansion managementVSAvoidmanufacturing process
Core Design Contradiction:
ReliabilityVSEase of manufacture

Solution Approach 1:

The patent applies parameter changes by carefully selecting specific alloy compositions and their corresponding thermal expansion coefficients. The dissimilar alloy ribs are chosen to have thermal expansion properties that complement the titanium wall, creating a controlled differential expansion pattern. This parameter optimization allows the structure to manage thermal expansion effectively while maintaining manufacturability through established additive manufacturing processes for metal alloys.

Inventive Principle:
Principle #35Parameter changes

3Strength

If solid ribs are used in isogrid structures, then structural strength is maximized, but stress concentrations increase under thermal loading

Engineering Contradiction:
Improvestructural strengthVSAvoidstress concentration
Core Design Contradiction:
StrengthVSStress or pressure

Solution Approach 1:

The patent applies porous materials by implementing hollow ribs with internal cavities instead of solid ribs. These hollow ribs maintain sufficient structural strength while reducing mass and thermal inertia. The hollow configuration also reduces stress concentrations under thermal loading by distributing thermal stresses more evenly throughout the rib structure. The walls of the hollow ribs provide the necessary structural integrity while the empty interior reduces the overall stress burden during thermal cycling.

Inventive Principle:
Principle #31Porous materials

Applied Scientific Principles

This section explains which scientific principles are used to turn an abstract innovation direction into a practical engineering solution.

Function Achieved in This Case

The hybrid alloy structure effectively manages thermal expansion, reduces stress concentrations, and enhances structural integrity, ensuring consistent clearance and reduced deformation under varying thermal conditions.

Implementation Method 1

differential thermal expansion between materials, leading to potential clearance issues and increased stress concentrations

Methodology Applied
Scientific EffectThermal expansion: Thermal Expansion

Implementation Method 2

additive manufacturing of ribs to enhance structural integrity

Methodology Applied
Scientific EffectAdditive manufacturing: 3D Printing

Data Source

PatentEP4703569A2Isogrid structures, gas turbine engine, methods for manufacturing an isogrid structure, and method for using the isogrid structure
Publication Date: 2026.03.04 RTX CORP
  • EP4703569A2 patent drawingFigure 1
  • EP4703569A2 patent drawingFigure 2
  • EP4703569A2 patent drawingFigure 3

AI summary

An isogrid structure (22A; 22B) has a wall (38) having a first face (40) and a second face (42). An isogrid of hollow ribs (70, 72, 74) is formed on the wall second face (42). The ribs (70, 72, 74) of the isogrid have respective rib interiors. The wall (38) comprises a first alloy and the ribs (70, 72, 74) comprise a second alloy different from the first alloy. Junctions (76) of the ribs (70, 72, 74) are at bosses having an interior surface open to the rib interiors and an external environment.