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Page 1: Merging Analysis with Design and Manufacturingesss.com.br/events/ansys2010/pdf/22_1_1150.pdf · merge FiberSIM with our engineering software and processes. Lockheed Martin’s goal
Page 2: Merging Analysis with Design and Manufacturingesss.com.br/events/ansys2010/pdf/22_1_1150.pdf · merge FiberSIM with our engineering software and processes. Lockheed Martin’s goal

©2010 C

onfidential

Merging Analysis with Design and Manufacturing

for Composites

Presented By:

Chuck Higgins

Director, Latin America

VISTAGY, Inc.

2010 ANSYS South America Conference & ESSS User Conference

29 October 2010

Atibaia, SP - Brasil

Page 3: Merging Analysis with Design and Manufacturingesss.com.br/events/ansys2010/pdf/22_1_1150.pdf · merge FiberSIM with our engineering software and processes. Lockheed Martin’s goal

©2010 C

onfidential

The VISTAGY Advantage

Domain

Expertise

Process

Knowledge

3D Integration

Industry-Specific

Solutions

Deep, synthetic,

cross disciplinary workflows

Deep understanding

of the industry

Airframe Structures

Composite Materials

Joints and Fasteners

Airframe Design/Analysis

Composite Manufacturing

Assembly Techniques

First Article Inspection

Native geometric integration

with underlying CAD/Viewer

data model

Catia, Pro/E, NX

Page 4: Merging Analysis with Design and Manufacturingesss.com.br/events/ansys2010/pdf/22_1_1150.pdf · merge FiberSIM with our engineering software and processes. Lockheed Martin’s goal

©2010 C

onfidential

Proven Track Record of Innovation

20111993 2001 2006

CATIA V3

Unigraphics / NX

Pro/ENGINEER

CATIA V5

CATIA V4

CATIA V6

Comanche

B787A350 XWB

V-22

F-22

S-92

JSF Boeing

JSF LMTAS

F-35

CRJ700

GE90

C-Series

G650

MS21

GEnx

Delta

A380

Premier

COMAC 919

Ares / CCM

Mockup Solids & Weights

Analysis

Interface

RTM3D Annotations

Cross sections etc.

Optimized UIComposite

Engineering

Environment

Template Based

Documentation

Fiber

Placement

Laser

ProjectionFlat Pattern

Producibility

Grid/Structure

Based Design

Variable Offset

Surface Technology

Model

Based

Design

Model Merge

Skin Transfer

XML Design

Checking

COS

Quality PE

SimXpert

Integration

DFM ADD Project

Go Deep

Project

Graphite

Project

Take Flight

GamesaCener

Vestas

Sinoma

TPI

Dong Feng

Page 5: Merging Analysis with Design and Manufacturingesss.com.br/events/ansys2010/pdf/22_1_1150.pdf · merge FiberSIM with our engineering software and processes. Lockheed Martin’s goal

©2010 C

onfidential

“A 4 to 1 savings in

production time was

achieved for complex parts

of the first aircraft.”

Bombardier Inc.

“VISTAGY promised

impressive reductions in

product development time for

our composite parts, and they

delivered on their promises.”

Renault F1 Team

“We have worked actively to

merge FiberSIM with our

engineering software and

processes. Lockheed Martin’s

goal is to integrate the most

productive composites design

and manufacturing tools

available.”

Lockheed Martin Corp.

“With FiberSIM, our first parts

were virtually perfect and we

were able to do it right the first

time.”

Sikorsky Aircraft Corp.

Page 6: Merging Analysis with Design and Manufacturingesss.com.br/events/ansys2010/pdf/22_1_1150.pdf · merge FiberSIM with our engineering software and processes. Lockheed Martin’s goal

©2010 C

onfidential

Increased Use of Composites Over Time

1%

747

3%757/767

11%777

50%

787

Source: Boeing

Carbon laminate

Carbon sandwich

Other composites

Alenia Aeronautica

Spirit Wichita

Fuji Heavy Ind.Boeing Seattle

Kawasaki Heavy Ind.

Goodrich Aerospace

Vought Aircraft

Spirit Tulsa

Boeing Winnipeg

Korea Aerospace

Harbin AircraftFACC

Boeing Moscow

Korean Airlines

Aermacchi

DACC

787 - 50%Composites by Weight but almost

All Surfaces and Structure made of Composites

Page 7: Merging Analysis with Design and Manufacturingesss.com.br/events/ansys2010/pdf/22_1_1150.pdf · merge FiberSIM with our engineering software and processes. Lockheed Martin’s goal

©2010 C

onfidential

Industry Specific Solutions….

Quality Planning Environment (QPE)First Article Inspection Planning and

Execution for Parts and Assemblies

– Definition and Manufacturing of Composite Detailed Parts

Airframe Design Environment (ADE)Engineering Definition of

Parts, Assemblies, Joints & Fasteners

Airframe Manufacturing Environment (AME)Manufacturing Planning for Parts, Assemblies, Fasteners

Define Intermediate manufacturing states

Define Conditions of Supply

Industry has a need for considering the entire airframe in the design process!

Page 8: Merging Analysis with Design and Manufacturingesss.com.br/events/ansys2010/pdf/22_1_1150.pdf · merge FiberSIM with our engineering software and processes. Lockheed Martin’s goal

©2010 C

onfidential

XML XML XML

Manufacturing

Where Do VISTAGY Products Fit?

Conceptual Detailed

Installation

Quality

FS - CEE

ADE AME

System

Requirements,

Sizing

QPE

Preliminary

Loft,

Substructure,

Openings,

Sizing

FS-ACEE

Develop Design

in a Robust

Process

Planning for Efficient

and Low Cost

Manufacture

Verified

Requirements

Fabrication

CAPP

ERP

PDM

Page 9: Merging Analysis with Design and Manufacturingesss.com.br/events/ansys2010/pdf/22_1_1150.pdf · merge FiberSIM with our engineering software and processes. Lockheed Martin’s goal

©2010 C

onfidential

Flexible Solutions for Manufacturing

Manufacturing– Nesting software– Cutting systems– Laser projection systems– Path planning software– Fiber placement machines– Tape laying machines– Ply verification systems

Simulation– Materials analysis– Structural analysis– Composites FEA– RTM flow– Failure analysis

Other– Cost estimation– Process planning

•CUTTING MACHINES AND NESTING SOFTWARE

•LASER PROJECTION SYSTEMS

•ANALYSIS AND SIMULATION SOFTWARE (FEA, CFD)

•AUTOMATED DEPOSITION

Page 10: Merging Analysis with Design and Manufacturingesss.com.br/events/ansys2010/pdf/22_1_1150.pdf · merge FiberSIM with our engineering software and processes. Lockheed Martin’s goal

©2010 C

onfidential

Improving the Development Process

Efficient communications between Design, Analysis and

Manufacturing

Accommodate late changes to enable optimization

Bring appropriate feedback directly to design

Analysis

Shorter Development Time

More Optimized Structure

Design Manufacturing

ManufacturingDesign

Manufacturing

Page 11: Merging Analysis with Design and Manufacturingesss.com.br/events/ansys2010/pdf/22_1_1150.pdf · merge FiberSIM with our engineering software and processes. Lockheed Martin’s goal

©2010 C

onfidential

Engineering Starting Point

Geometry

• Loft Surface

• Part Boundary

• System Lines

Stress Data

• Laminate Spec

for “Bays”

Stacking Tables

Page 12: Merging Analysis with Design and Manufacturingesss.com.br/events/ansys2010/pdf/22_1_1150.pdf · merge FiberSIM with our engineering software and processes. Lockheed Martin’s goal

©2010 C

onfidential

FiberSIM Supports the Entire Engineering Process

FiberSIM Results

Loft Surface

Part Boundary

System Lines

Stress Data

Automatic Geometry Creation

Automatic Ply Creation

Automatic Change Updates

Page 13: Merging Analysis with Design and Manufacturingesss.com.br/events/ansys2010/pdf/22_1_1150.pdf · merge FiberSIM with our engineering software and processes. Lockheed Martin’s goal

©2010 C

onfidential

Dynamic Design Changes with

FiberSIM ACEE

Design starts with loft surface and

substructure definition

Zones are created directly from

substructure definition

Ply layup is automatically generated

from zones

Model updates dynamically with

design changes–Stringer and frame spacing

–Zone thickness and laminate stress gage

–Ply drop strategy

Page 14: Merging Analysis with Design and Manufacturingesss.com.br/events/ansys2010/pdf/22_1_1150.pdf · merge FiberSIM with our engineering software and processes. Lockheed Martin’s goal

©2010 C

onfidential

FiberSIM Integrated with FEA

Tools

FEA Tool

CAD/FiberSIM

Design Part

Mesh

Part

Populate

Properties

Run analysisLBC

•®

Fully defined

composite mesh

properties

Shared native

CAD geometry

Page 15: Merging Analysis with Design and Manufacturingesss.com.br/events/ansys2010/pdf/22_1_1150.pdf · merge FiberSIM with our engineering software and processes. Lockheed Martin’s goal

©2010 C

onfidential

Structural Requirements and

Optimization Driving Zone

Changes...

Sizing Specification -

Add Plies

This can be done in

either product

Zone Modification

FEA

Thickness Plot

Page 16: Merging Analysis with Design and Manufacturingesss.com.br/events/ansys2010/pdf/22_1_1150.pdf · merge FiberSIM with our engineering software and processes. Lockheed Martin’s goal

©2010 C

onfidential

... which Result in FiberSIM

Zone/Ply Changes ...

Import Ply and Laminate

changes into FiberSIM

Design rules are

automatically applied

NO MANUAL

INTERACTION

REQUIRED!

®

Page 17: Merging Analysis with Design and Manufacturingesss.com.br/events/ansys2010/pdf/22_1_1150.pdf · merge FiberSIM with our engineering software and processes. Lockheed Martin’s goal

©2010 C

onfidential

... and can be Validated as a Ply-

Based Analysis

Load-cases are run against true Layup

Drop-offs and thickness variations are expressed with fidelity of mesh

FiberSIM Simulation provides true thickness and fiber orientations

FEA

Thickness Plot

45o ?

Page 18: Merging Analysis with Design and Manufacturingesss.com.br/events/ansys2010/pdf/22_1_1150.pdf · merge FiberSIM with our engineering software and processes. Lockheed Martin’s goal

©2010 C

onfidential

Industry Specific Solutions for

Design…

Design

Release

Quickly Release

Designs To

Manufacturing

QPE

Loft

Datums

LoadsSizing Analysis

Structure Based

Skin Design

ProducibilityATL/AFP

Hand LayupForming

IML Surfaces Mockup, Mating,

Tooling

Joint

Definitions

Fast. Layout

Substructure

Design

Detailed

Fastener/Hole

DefinitionsDesign Rule

Validation

Metrics

ReportingWeights, CG, BOM

Release

DocumentationPlybooks, MBD

Page 19: Merging Analysis with Design and Manufacturingesss.com.br/events/ansys2010/pdf/22_1_1150.pdf · merge FiberSIM with our engineering software and processes. Lockheed Martin’s goal

©2010 C

onfidential

... and Manufacturing

Release to

Manufacturing

Condition of

Supply

On-time

On-budget

On-spec delivery

TM

Automated

Drilling and

Fastening

Automated

Composite

LayupInspection

Layup

Cured Laminate

Dimensional

(AS9102)

QPE

QPE

Flat Patterns

Laser

Guided

Layup

Page 20: Merging Analysis with Design and Manufacturingesss.com.br/events/ansys2010/pdf/22_1_1150.pdf · merge FiberSIM with our engineering software and processes. Lockheed Martin’s goal

200 Fifth Avenue ● Waltham, MA 02451 USA

+1.781.250.6800

www.vistagy.com

Chuck HigginsDirector, Latin America

[email protected]

+1.214.458.1775