Failsafe Topology Optimization for Structural Redundancy

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Solution Overview

Problem

Current topology optimization methods fail to incorporate failsafe design principles, which are crucial for ensuring structural integrity in critical applications like aircraft and nuclear power plants, as they prioritize material efficiency over redundancy, leading to designs that are not robust against structural failures.

Innovation Solution

A computational scheme for failsafe topology optimization is developed, which involves defining a structural continuum with a finite damage population and using a Message Passing Interface (MPI) parallel implementation to optimize the distribution of material and voids, ensuring the structure remains functional even when material is removed from arbitrary locations, by minimizing compliance and maintaining stress thresholds.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Quantity of substance

If topology optimization pushes material utilization to maximum efficiency, then material efficiency is improved, but structural redundancy deteriorates

Engineering Contradiction:
Improvematerial efficiencyVSAvoidstructural redundancy
Core Design Contradiction:
Quantity of substanceVSReliability

Solution Approach 1:

The patent segments the structural domain into a finite population of discrete damage locations, where each location represents a potential failure point. This segmentation allows the optimization to explicitly consider multiple failure scenarios and design redundant load paths that can accommodate damage at any segmented location, thereby maintaining reliability while achieving material efficiency.

Inventive Principle:
Principle #1Segmentation

2Reliability

If failsafe design considers infinite damage population, then structural reliability is improved, but computational complexity deteriorates

Engineering Contradiction:
Improvestructural reliabilityVSAvoidcomputational complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The patent applies partial action by considering a finite subset of damage locations rather than an infinite population. By selecting a representative finite population of damage locations, the method achieves sufficient structural reliability for practical engineering applications while keeping computational complexity manageable through efficient parallel processing.

Inventive Principle:
Principle #16Partial or excessive action

Solution Approach 2:

The patent creates multiple copies of the structural model, each with damage applied at a different location from the finite damage population. These copied models are then analyzed in parallel using MPI, allowing the exhaustive evaluation of multiple failure scenarios to be performed efficiently without requiring a single overly complex computational model.

Inventive Principle:
Principle #26Copying

3Reliability

If exhaustive damage location analysis is performed, then material survival rate is improved, but computational time deteriorates

Engineering Contradiction:
Improvematerial survival rateVSAvoidcomputational time
Core Design Contradiction:
ReliabilityVSLoss of time

Solution Approach 1:

The patent performs preliminary action by pre-defining a finite population of damage locations before the optimization process begins. This pre-definition allows the computational framework to efficiently evaluate all specified damage scenarios without requiring adaptive refinement during optimization, thereby achieving comprehensive damage analysis while controlling computational time through upfront problem setup.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The patent maintains continuity of useful action by using MPI parallel processing to simultaneously evaluate all damage locations in the finite population. Rather than sequentially analyzing each damage scenario (which would be time-consuming), the parallel implementation continuously processes multiple damage cases simultaneously, maintaining high computational utilization and reducing total analysis time.

Inventive Principle:
Principle #20Continuity of useful action

Data Source

PatentUS10354024B2Failsafe topology optimization
Publication Date: 2019.07.16 SIEMENS INDUSTRY SOFTWARE INC
  • US10354024B2 patent drawing
  • US10354024B2 patent drawing
  • US10354024B2 patent drawing

AI summary

Failsafe robustness of critical load carrying structures is an important design philosophy for aerospace industry. The basic idea is that a structure should be designed to survive normal loading conditions when partial damage occurred. Such damage is quantified as complete failure of a structural member, or a partial damage of a larger structural part. This paper establishes for the first time the concept and formulation of failsafe requirement within the context of topology optimization. Efficient computational scheme and computer implementation are carried out. Several examples are shown to demonstrate the impact of failsafe requirement to design concept generated by topology optimization.