Rotor Disk Recess Design for Stress Distribution
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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
Engineering 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
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.
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.
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
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.
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.
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
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.
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.
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
Implementation Method 2
thermal and centrifugal stresses are exerted on the disc's web
Data Source
Figure 1~2
Figure 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).