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improving design by analysis James Farrar Business Development Manager The PROMOTE Software

Development of Rolls-Royce Process Modelling Capability for Aerospace Discs and Shaft Assemblies

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Funded by the Technology Strategy Board (TSB) and undertaken in conjunction with Rolls-Royce, Nottingham University and Birmingham University, Wilde Analysis has developed a user-friendly software tool allowing non-simulation specialists to undertake simulations of the manufacture of disks and shafts for turbines. Future efficient lightweight aero-engines will rely on the next generation of high temperature materials. However, they present new manufacturing challenges, particularly in joining where friction welding has been identified as a key enabling technology. Sponsored by the TSB, the Process Modelling for Tomorrow’s Engines (PROMOTE) project is a collaborative project involving Rolls-Royce, Wilde Analysis and the Universities of Nottingham and Birmingham, which was tasked with capturing the state-of-the-art in materials and process modelling and implementing it in an end user-focused software tool. General details on the project were published in an article in Eureka Magazine (http://www.eurekamagazine.co.uk/article/22229/Process-modelling-improves-aero-engine-design.aspx) in 2010. This overview presentation has been made at conferences. Please contact us at http://WildeAnalysis.co.uk/contact for more information on: - The PROMOTE software and options to use it for your processes - DEFORM process modelling software and consulting services - Our software customisation services

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Page 1: Development of Rolls-Royce Process Modelling Capability for Aerospace Discs and Shaft Assemblies

improving design by analysis

James Farrar

Business Development Manager

The PROMOTE Software

Page 2: Development of Rolls-Royce Process Modelling Capability for Aerospace Discs and Shaft Assemblies

• Formed in 1980 as Finite Elements Ltd

• 1000+ clients

• Member of Wilde Group of 70+ employees and £10m +

turnover

• 24 employees involved in analysis sales, services and

administration – 21 are qualified engineers with significant experience using analysis

software

• ISO 9001:2008 Approved Quality Management System

• On UK-steering committee for NAFEMS and

involvement with many industry associations.

Wilde Overview

Page 3: Development of Rolls-Royce Process Modelling Capability for Aerospace Discs and Shaft Assemblies

DEFORM SYSTEM

raw material production forming heat treatment &

microstructure

machining machining distortion

& residual stress

Installation / in-

service performance

Page 4: Development of Rolls-Royce Process Modelling Capability for Aerospace Discs and Shaft Assemblies

• Wilde - UK Distributor for 15 years

• UK, Ireland, Northern Europe, France

• Software

• Training

• Technical support

• Consulting services

DEFORM Business

Page 5: Development of Rolls-Royce Process Modelling Capability for Aerospace Discs and Shaft Assemblies

PROMOTE Brief Overview

Post Solution HT Quench

Ageing Heat Treatment

Machining Operations

Inertia Welding

Machining Operations

Post Welding Heat

Treatment

• Manufacturing route for turbine discs and

shafts is well defined.

• Improved engine performance requires

optimisation of the manufacturing process

routes in each area.

• Aim of PROMOTE is to deliver a software tool

to model all of the processes involved in the

manufacture of aerospace disc and shaft

assemblies

Page 6: Development of Rolls-Royce Process Modelling Capability for Aerospace Discs and Shaft Assemblies

PROMOTE Interface Objective

• Deliver capability for modelling disc and shaft manufacturing routes.

• Provide process modelling capability to process and materials specialists rather

than a very small population of process modelling specialists.

• Deliver a user-friendly software environment to enable use of the modelling

capability in a quality controlled and efficient manner.

• Without the need for extensive training or specialist background knowledge in

process modelling.

• Enable users to input the required process parameters and automatically

convert this information to DEFORM requirements.

• Capture current state-of-art for current process modelling.

Process

Model

Process

Parameters

Initial

Geometry

Initial Material

Properties

Process

Model

Process

Parameters

Modified

Geometry

Material

Properties

etc.

Single user-friendly interface

Residual

Stress

Model

Results

Modified

Geometry

Material

Properties

Residual

Stress

Model

Results

Page 7: Development of Rolls-Royce Process Modelling Capability for Aerospace Discs and Shaft Assemblies

PROMOTE Development

• WP1: Rolls Royce

• Material acquisition, characterisation, modelling and test sample

manufacturing (University of Birmingham)

• WP2: Rolls Royce - Manufacturing Process Modelling

• Heat Treatment

• Machining (Distortion)

• Inertia Welding (University of Nottingham)

• WP3: Wilde Analysis

• PROMOTE Software integration and system development

Page 8: Development of Rolls-Royce Process Modelling Capability for Aerospace Discs and Shaft Assemblies

PROMOTE - Basic Concepts

• Object-oriented paradigm:

– “Workpiece” object

– “Process” object

– Process changes state of workpiece

Label

Process

Label identifies

workpiece ID and

its current state

New label

Page 9: Development of Rolls-Royce Process Modelling Capability for Aerospace Discs and Shaft Assemblies

Basic Concepts – ctd

• Representation of manufacturing route

1a 2a

1b

Age

Machine

1c

Quench

2b

Weld

12a

Fore Aft

Time

Note: new workpiece

’12’ with initial state ‘a’

Page 10: Development of Rolls-Royce Process Modelling Capability for Aerospace Discs and Shaft Assemblies

Basic Concepts – ctd

• Define manufacturing route

• Define “process” object attributes

– Process parameters, jigs & fixtures, etc

• Define initial “workpiece” object attributes

– geometry, material, etc

• Subsequent object attributes determined by

preceding processes

Page 11: Development of Rolls-Royce Process Modelling Capability for Aerospace Discs and Shaft Assemblies

Basic Mechanics

• Process simulation in text-driven DEFORM Keyword

file(s)

Database

file

Pre-processor

Instruction(s): ‘read file’

Database

file

Instruction: ‘generate database’

Solver

Instruction: ‘run solver’

Text file(s) containing info on

workpiece, material, process

parameters and numerics

Binary file containing

complete problem description

Keyword

file

Instruction: ‘write

keyword file for

workpiece’

Text file containing complete

description of workpiece state

Page 12: Development of Rolls-Royce Process Modelling Capability for Aerospace Discs and Shaft Assemblies

Workpiece data entry

PROMOTE Workf low

Geometry

Material

Mesh

Geometry

display

Engine

assembly display

Import / specify

workpiece

Page 13: Development of Rolls-Royce Process Modelling Capability for Aerospace Discs and Shaft Assemblies

Age process data entry

PROMOTE Interface

Geometry

display

Engine

assembly display

Material

model inputs

MSRR file input

Process

inputs

Process schematic

Customised, automated model inputs

T ( C)

t(s)

User defined microstructure models

Available

processes

Geometry

display

Process schematic

Customised, automated model inputs

T ( C)

t(s)

User defined microstructure models

Available

processes

Geometry

display

Temperature profile input

Points for

auto – post

processing

Page 14: Development of Rolls-Royce Process Modelling Capability for Aerospace Discs and Shaft Assemblies

PROMOTE Interface Weld process inputs

Material

model inputs

Dies &

Fixtures

Weld inputs

(Load /

inetrtia)

Engine

assembly display

Page 15: Development of Rolls-Royce Process Modelling Capability for Aerospace Discs and Shaft Assemblies

PROMOTE Interface Machine process inputs

Engine

assembly display

Cut profiles

Page 16: Development of Rolls-Royce Process Modelling Capability for Aerospace Discs and Shaft Assemblies

PROMOTE Interface Machine process inputs

Engine

assembly display

Cut profiles

Page 17: Development of Rolls-Royce Process Modelling Capability for Aerospace Discs and Shaft Assemblies

PROMOTE Interface

Automated batch

run scheduling

Automated & interactive

post –processing options

Page 18: Development of Rolls-Royce Process Modelling Capability for Aerospace Discs and Shaft Assemblies

• Background information on DEFORM:

www.wildeanalysis.co.uk

www.deform.com

• Contact James Farrar to:

– Discuss your simulation requirements

– Arrange a company-specific web or live meeting on the

PROMOTE and DEFORM software

– Discuss evaluation options

[email protected] Tel: 0161 4747479

The Way Forward