Rotor Disk Recess Design for Stress Distribution

Resolve Bottlenecks,
Find Innovative Solutions
Generate Solutions

Solution Overview

Problem

Turbomachine rotor disks experience significant stress concentrations at orifices due to thermal and centrifugal forces, leading to reduced rotor life, and existing solutions either increase mass or disrupt air ventilation.

Innovation Solution

A recess design around orifices that alternates between first parts surrounding each orifice and second parts between adjacent orifices, with radially offset edges, and complementary geometry on the flange contact surfaces to distribute stresses homogeneously.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Strength

If the thickness of the fabric is increased around the orifices to reduce stress concentrations, then the strength and durability of the rotor disk is improved, but the mass of the fabric increases which induces higher centrifugal stresses and reduces overall efficiency

Engineering Contradiction:
ImprovestrengthVSAvoidmass
Core Design Contradiction:
StrengthVSWeight of moving object

Solution Approach 1:

The invention applies local quality by creating a recess only in the regions where stress concentration occurs (near the orifices) while maintaining the original thickness in other areas. This localized modification strengthens the critical zones without increasing the mass of the entire fabric, thereby improving strength without the negative centrifugal effects of global thickening.

Inventive Principle:
Principle #3Local quality

Solution Approach 2:

The invention transitions from modifying the fabric in the radial-thickness dimension (increasing thickness) to modifying it in the axial dimension (creating a recess). This dimensional shift allows stress distribution improvement without adding mass, as the recess redistributes stress through geometric configuration rather than material quantity.

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

2Stress or pressure

If oblong holes are made in the fabric between the mounting screw holes to influence stress distribution, then the stress distribution is improved, but the ventilation airflow of the rotor is disrupted by allowing air to circulate between the cavities

Engineering Contradiction:
Improvestress distributionVSAvoidventilation airflow disruption
Core Design Contradiction:
Stress or pressureVSObject-affected harmful factors

Solution Approach 1:

The recess is designed to be localized around the orifices where stress concentration occurs, rather than creating openings throughout the fabric. This localized approach modifies stress distribution in the critical areas while maintaining the fabric's integrity for ventilation in the surrounding regions, thus avoiding airflow disruption.

Inventive Principle:
Principle #3Local quality

Solution Approach 2:

The recess consists of an alternation of first parts surrounding each orifice and second parts between adjacent orifices. This segmented structure allows stress relief at each orifice location while the second parts maintain fabric continuity for ventilation, preventing uncontrolled air circulation between cavities.

Inventive Principle:
Principle #1Segmentation

3Duration of action of stationary object

If a recess is created around the orifices to distribute stresses homogeneously, then the stress concentration is reduced and rotor life is extended, but the manufacturing complexity increases

Engineering Contradiction:
Improverotor lifeVSAvoidmanufacturing complexity
Core Design Contradiction:
Duration of action of stationary objectVSDevice complexity

Solution Approach 1:

The recess is segmented into first parts and second parts with different radial positions. This segmentation allows the recess to be manufactured using standard CNC machining operations by defining it through alternating radial positions, making the complex geometry achievable with conventional manufacturing processes.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The recess features curved radial boundaries defined by alternating first and second parts. These curved geometries are easily generated using standard CNC machining tools and techniques, allowing the complex stress-distributing shape to be manufactured with conventional equipment rather than requiring specialized processes.

Inventive Principle:
Principle #14Spheroidality (Curvature)

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 recess design reduces internal stresses at orifices and enhances stress distribution, thereby extending rotor life without increasing mass or disrupting air ventilation.

Implementation Method 1

the distribution of stresses in the fabric to be modified compared to a fabric with a constant cross-section

Methodology Applied
Scientific EffectStress distribution:

Implementation Method 2

thermal and centrifugal stresses are exerted on the disc's web

Methodology Applied
Scientific EffectCentrifugal force: Centrifugal Force

Data Source

PatentEP3301258B1Rotor disk and rotor of turbomachinery including such a disk
Publication Date: 2023.10.25 SAFRAN AIRCRAFT ENGINES SAS
  • EP3301258B1 patent drawingFigure 1~2
  • EP3301258B1 patent drawingFigure 3~4

AI summary

The invention relates to a rotor disc (12) (10) comprising, with respect to the main axis of the disc (12), an annular radial web (14), a radially central hub (16) located at the inner radial end of the web (14), and a rim (18) located at the outer radial end of the web (14). The web (14) comprises an upstream face (14a) and a downstream face (14b), with respect to the main axis of the disc (12), and a plurality of bolt holes (28) (32, 34) for attaching at least one annular flange (26) belonging to another adjacent rotor disc (12) (10) on one or both of the upstream face (14a) or the downstream face (14b) of the web (14). The web is characterized in that said upstream face (14a) and/or said downstream face (14b) of the canvas (14),includes a generally annular recess (36) whose bottom is axially recessed towards the interior of the fabric (14) relative to the rest of said upstream face (14a) and/or said downstream face (14b) and which extends radially outwards from the hub (16) of the disc (12) towards the rim (18) and which surrounds, at a distance, a radially internal part of each of the orifices (28) of the fabric (14).