Experience with Stress Workflow Automation at Fokker Aerostructures - - PowerPoint PPT Presentation

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Experience with Stress Workflow Automation at Fokker Aerostructures - - PowerPoint PPT Presentation

Format Background > Picture or > browse Overview Experience with Stress Workflow Automation at Fokker Aerostructures Fokker Aerostructures Ronald van der Aa 5-Oct-2017 Overview Experience with Stress Workflow Automation at


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Overview

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Experience with Stress Workflow Automation at Fokker Aerostructures

Fokker Aerostructures

Ronald van der Aa 5-Oct-2017

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Experience with Stress Workflow Automation at Fokker Aerostructures 03:00 – 03:30

  • Introduction Fokker Aerostructures
  • Design process
  • Infrastructure ModelCenter / CenterLink Fokker
  • List of Modelcenter workflows
  • List of used application in MC workflows
  • Future WF (RiaM)
  • Conclusions
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Fokker Technologies, founded by aviation pioneer Anthony Fokker in 1919, was acquired by GKN Aerospace in 2015.

Electrical wiring interconnections systems

Fokker Elmo Fokker Services

Independent aerospace services provider Lightweight aerostructures & components

Fokker Aerostructures Fokker Landing Gear

Landing gear systems

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Fokker Technologies

Leading multi-technology specialist

Landing Gear Electrical and Wiring Services Aerostructures Office locations

Mexico

1 location

2

China

2 locations

1 1

India

1 location

1

Romania

2 locations

2

Turkey

1 location

1

Canada

1 location

1

Singapore

1 location

1 1

USA

4 locations

1 1 1 2

Netherlands

5 locations

2 2 1 3 1

2015 sales

€796 million

Number of employees

4,950

Number of locations 17 in 9 countries

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Introduction Fokker Aerostructures

We are market leading and technology leading in aerostructures, supporting our customers in making aircraft fly faster, further and greener. We provide empennages, wing structures, fuselages and components for major platforms ranging from helicopters to business jets and from advanced fighter aircraft to the most used single aisle aircraft and the largest passenger planes in the world. With lightweight composites, additive manufacturing and innovative high speed machining technologies we help to reduce emissions and weight on the aircraft and enhance passenger comfort.

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Introduction Fokker Aerostructures

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Fokker Design process

Design Definition Phase Proposal Phase Full Scale Development Phase Sustaining Phase

RFP

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Infrastructure ModelCenter / CenterLink Fokker

High speed connections

Linux legacy tools TH3 tools (existing) Light office tools Office 2003 Mathcad Small binaries Centerlink Clients ModelCenter ModelRunner Heavy office tools Office 2010 CAE tools Catia Patran Nastran Linux cluster Large nastran calculations (existing)

HP-Z400

MySQL

Windows Server 64bit multicore 8GB RAM

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List of Modelcenter workflows

Tool name Tool description

A.1.1.001 Composite skin Calculate composite skin strength and stability A.2.1.002 Metallic Ribs Webs Calculate metallic rib webs strength and stability A.3.1.005 Metallic Ribs stiffeners Calculate metallic rib longitudinal and transverse stiffener strength and stability A.4.1.002 Metallic Ribs flanges Calculate metallic rib flanges connection to skin and beams A.9.4.002 Diesel to FATDAC_SPRAC Convert Gulfstream Diesel output into FATDAC/SPRAC input A.9.4.002 Diesel to FATDAC_SPRAC Batch Convert Gulfstream Diesel output into FATDAC/SPRAC input A_101 Joint strength and bearing This application can be used to calculated the inplane MS of a joint (composite sandwich skin to metal substructure) A_102 Panel+facing stability This application can be used to calculated the stability MS of a composite sandwich panel and its facings A_103 Facing strain cutoff This application can be used to calculated the facing strain cut-off MS of a composite sandwich panel A_104 Core strength This application can be used to calculated the core strength MS of a composite sandwich panel A.302 Submit Isami stand alone analysis Submit Isami stand alone analysis with Excel- or text file template

A.16.1.001 Rainflow counting (SMS) Rainflow count the 28 Fatdac input files from Fatigue wizard and create one spectrum file and run fatdac A.16.1.001 Rainflow counting Batch (SMS) Rainflow count the 28 Fatdac input files from Fatigue wizard and create one spectrum file and run fatdac TH3.906 Calculate initial shear buckling stress of rectangular flat isotropic plates with one hole run Nastran batch Run all Nastran bdf files in a directory

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List of Modelcenter workflows

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List of used application in MC workflows

  • Used for GUI’s
  • Analysis
  • Running VBA macro’s
  • Linux programs
  • Nastran output files

VBScript for:

  • Copy files
  • Zip Files
  • Delete files
  • Show Message Box
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List of used application in MC workflows

GUI Example

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Future WF (RiaM)

With the Rudder In A Month (RiaM) project we want to reduce lead time for the design process.

  • Using:
  • Standardized design process. Workflow with integrated design logic and MDO.
  • Design process innovation (including knowledge management and IT

infrastructure).

  • Re-use of knowledge. Formalizing tacit knowledge and best practices.
  • Real-time connection between knowledge and solution / geometry.
  • Automation of business process and tasks where possible and helpful.
  • In order to:
  • Accelerate the execution of tasks on the critical path.
  • Reduce non-recurring cost of the total program by more than 50%.
  • React quicker to customer requests and changes.
  • Improve and expand available knowledge by front loading process (e.g. sensitivity

analysis, design space exploration, driving design parameters) and virtual rapid prototyping, in order to aid the creative process.

  • Improve quality of the product and process by having a predictable design process,

performing more iterations and having automated requirements compliance checks.

  • RiaM is not limited to Rudders only.
  • Objectives achieved for thermoplastic movable
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Goals RiaM

Development process

complexity transfer /reduction lead time gain due to simplicity

1 2 3 4

Plan 2016

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Future WF (RiaM)

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Future WF (RiaM)

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Future WF (RiaM)

Output of CAD2FEM (MSC Patran)

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Future WF (RiaM)

Run MSC Nastran

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Future WF (RiaM)

Stress Analysis

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Future WF (RiaM)

Stress Analysis Buckling

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Future WF (RiaM)

Stress Analysis Material Strength

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Conclusions

  • Using large files in file variables is not working well
  • Using plugins very user friendly
  • Linking input and outputs is very easy
  • QuickWrap very useful for programs which do not have a plugin
  • Centerlink components are very useful for web based access
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Thank you for Your attention

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Ronald van der Aa 5-Oct-2017