PFW Engineering - Presentation

Transcription

Presentation of PFW Engineering
February 2014
© All rights reserved. Reproduction or disclosure to third parties of this document or any part thereof for purposes other than intended for by this document, is not permitted,
except with prior and express written permission by PFW Engineering
1
PFW Engineering
PFW Engineering in a nutshell
CUSTOMERS
PEOPLE
(1st tier; examples)
280 qualified Engineers;
37 CVEs
EADS incl. Airbus, Boeing,
Lufthansa Technik
APPROVALS
EXPERIENCE
(examples)
est. 1995, but covers all
experience of the
DORNIER company
Design Organization
(DOA) acc. EASA Part
21J.033 for all ATA
chapters
CURRENTS
PROJECTS
Our offer
(examples)
TOOLS
(examples)
CATIA, CADAM, ENOVIA,
PRIMES, PATRAN,
NASTRAN
A350XWB, A400M, B767,
Do328, B787
to our customer
February 2014
2
PFW Engineering the Company
Milestones
History – key milestones
Nearly 20 years of experience in the aerospace sector
1995
Formation of ‘GCT Garner Inc '
1998
Formation of ‘GCT Engineering Services Ltd '
2002
Fairchild Dornier Insolvency
2003
Formation of ‘GCT Projects GmbH’
2006
Acquisition of Dornier EASA21J and Formation
of ‘GCT Design Organisation GmbH'
2006
PFW Acquisition of 20% of GCT Group
2009
PFW Acquisition of 100% of GCT Group
2010
Rename GCT Projects to SG Aerospace
GmbH and GCT Garner Inc to PFW GCT Inc
Airbus took over 74.9% of the shares of PFW
2012
Formation of ‘PFW Engineering Inc’ in Canada
2013
Rename of all GCT Companies to PFW
Engineering
February 2014
€M
Formation of ‘Garner CAD Technic GmbH'
1997
2011
Key figures 2010/2011/2012
Sales
Employees
2010
35.5
307
Sales
Employees
2011
33.1
302
Sales
Employees
2012
30.3
318
Group Products
Certifications
3%
Interiors
5%
Structures
42%
Technical
Publications
5%
Systems
45%
3
Group overview
Company structure & link shareholding companies
Airbus Operations GmbH
Hamburg, Germany
74.9%
PFW Aerospace GmbH
Speyer, Germany
PFW Engineering GmbH
100%
Oberpfaffenhofen, Germany
PFW Aerospace Engineering Ltd.
Poole, UK
PFW Engineering Inc.
Seattle, USA
PFW Aerospace Canada Inc.
Montreal, Canada
February 2014
4
PFW Group Organization
By Jan 2014
Sales & Marketing
R. Kästel
Engineering
CFO
M. Pacher
Ph. Visotschnig
Executive Board
SA - Airlines & MRO
ED - Head of DO
G. Hieber
EE - Engineering Design
E. van der Pluijm (iPU)
GXH - Resource Management
M. Gerner
incl. Site Services
B. Breitling
A. Bischl
EE1 - Structural Components
M. Sehrschön
GXQ - Quality & ERM
Y. Hoffmann
I. Sidsaff
EDS - Systems & Equipment
E. Sunarkito
EE2 - Aircraft Systems
A. Kollofrath
GXF - Finance & PMO Office
H. Felbinger
SE - Airbus / PAG
E. van der Pluijm
EDI - Interiors & Cabin Safety
G. Hieber (iPU)
EE3 - Concessions
GXI - IT Support & Services
Ch. Klingler
J. Bohlin
SB - Boeing
EDA - Airframe
SC - Canada
M. von Hacht
EDF - Flight Physics
K. Metzger
GXB - Fuselage FISI + BASI
C. Bresson
GXW - Wing FISI + HYSI
EDO - Airworthiness Office
Ch. Thallmayr
ES - Stress & Fatigue
M. Heinrich
ET - Tech Pub
P. Garside
GXD - Fuselage CDSI
Th. Kupfer (iPU)
H. Schuller
EC - Config Management*
N.N.
*) leadership for DO related activities B. Braune
February 2014
5
PFW Engineering
Who we are
• PFW Engineering was incorporated in 1995.
• In January 2006, PFW Engineering acquired the Design Organisation for the EASA 21J
Airworthiness Certificate for the Dornier 328 aircraft family.
• In June 2006, PFW Aerospace GmbH acquired a strategic shareholding in the PFW
Engineering and in January 2009 PFW acquired 100% of the PFW Engineering.
• PFW Engineering is a worldwide organisation with EASA 21J airworthiness certification with
over 350 engineers rendering engineering design services to all major aerospace customers
in mainland Europe, USA, Japan, UK, and Israel.
• PFW Engineering is a Tier 1 Engineering Supplier to Airbus and Lufthansa Technik as well as
with Tier 1 Suppliers: Premium AeroTec, Aerolia and PFW..
• PFW Engineering is involved in design to spec on B787, A380, A350XWB, STC Dornier 328
and STC VIP Aircraft.
• Customer Focus
From the office locations in UK, mainland Europe, Israel and the USA, we can undertake staff
projects to fulfil customer programme requirements
February 2014
6
PFW Engineering
Mission Statement
We provide in the most cost effective way to our clients, products and services which
conform to their standard of quality and integrity and encompass the following factors:
• Creating trust
• Developing partnership
• A better identification of, and response to, client needs
• Delivering commitments
• Solving problems, not creating them
• Providing value for money
• Achieve customer and end-user satisfaction
• Focus on the contribution that everyone can make to the business and thereby the community
February 2014
7
Our Service
we deliver to our customer
complete engineering solutions
PFW Engineering undertakes work packages or turn-key projects in our own offices using the
latest CAD and analysis tools. We provide a full service, including project management and
sub-supplier coordination and monitoring.
aircraft certification services
As an EASA approved design and airworthiness organisation, PFW Engineering offers
development and certification services ranging from individual systems to complete aircraft.
supply of aerospace engineers
PFW Engineering provides professional engineers and qualified technicians for all aspects of
aerospace and for all development phases.
design and build solutions
Through our partnerships with prime aerospace manufacturing companies, PFW Engineering
is able to offer design and build solutions supporting the complete product life cycle.
technical publications
PFW Engineering develops and provides update services for technical publications including
Aircraft Flight Operation, Maintenance Planning, Maintenance Manuals, Structural Repair
Manuals and Illustrated Parts Catalogues.
customer services
February 2014
PFW Engineering undertakes upgrades, repairs, concessions, STC’s, Tech Doc’s for Airlines
and
VVIP.
© All rights
reserved. Reproduction or disclosure to third parties of this document or any part thereof for purposes other than intended for by this document, is not permitted,
8
PFW Engineering
Phone: +49 8153 9313 0
Fax: +49 8153 9313 999
PFW Engineering Office Bremen
Airbus-Allee 1
28199 Bremen
Phone: +49 421 538 4035
Fax:+49 421 5967536
USA
PFW Engineering Inc
1700 Seventh Avenue
Suite 2100
Seattle, WA 98101
Phone: +1 206 826 7188
Fax:+1 206 826 7189
Montreal
PFW Aerospace Canada Inc
6500 TransCanada Hwy, 4th floor,
Pointe-Claire, Quebec H9R 0A5
Phone: +1 514 426 6166
Fax:+1 514 426 6101
Phone: +44 2476 321241
Fax:+44 2476 321270
UK
PFW Aerospace Engineering
Ltd.
Unit A30
Arena Business Centre
Holyrood Close, Poole
Dorset. BH17 7FJ.
United Kingdom
France
PFW Engineering Office France
5, ave Albert Durand
31700 Blagnac
Phone: +33 534 60 69 21
Fax:+ 33 534 60 69 30
25227 Shave Zion POB 14
Phone: +972 545 315 815
Fax:+972 498 25252
Germany
Headquarters
Sonderflughafen Oberpfaffenhofen
Geb. 335
82234 Wessling
Israel
Worldwide Presence
February 2014
HQ Oberpfaffenhofen
Seattle office
9
PFW Engineering Headquarters
LOCATION: Airfield Oberpfaffenhofen
Airfield data
– Certified for all aircraft, only limitations in:
– yearly noise contingent / runway and taxiway load
factors
– Runway 2,286 x 45 m
– Landing systems: ILS/DME, CAT I, Min. 1000 m /
200 ft
– Owners: 80% Dornier GmbH (EADS) / 20% DLR
– Operator: EDMO GmbH (EADS)
Locations
1.
2.
3.
4.
5.
PFW Engineering Headquarters
RUAG Aerospace Deutschland
RUAG Aerospace Services
RUAG Aerospace Structures
DLR
Ground Traffic Connection
–
–
–
Expressway (300m)
Train Station (1000m)
Track Connection on-site
2
1
Distances
5
3
4
– to Munich International Airport 55 km
– to Munich downtown 20 km
– to EADS 30 km
February 2014
10
PFW Engineering
Customer Base (outline)
February 2014
11
PFW Engineering
Design Organization Approval (DOA) according EASA.21J.033
From January 2006 to September 2011, PFW Engineering DO GmbH took over
the Design Organisation Approval EASA Part 21J for the 328 Aircraft with 328
SSG being the TC holder.
The DO of PFW Engineering offers today
• employees 50 staff including CVEs (DREs) and Technical Publications which fulfils
the Design Organisation Approval for all ATA chapters.
• Supplemental Type Certificates (STCs)
• Major and Minor Repairs
• Continuous Airworthiness issues
• Technical Publications
February 2014
12
Design Organization Approval (DOA)
according EASA.21J.033 (cont.)
Scope of work in detail
The Design Organisation Approval (DOA) has been
granted for:
• Design changes and repairs for small aircraft CS23
• Design changes and repairs for large aircraft CS25
• Demonstration of compliance with all applicable
airworthiness requirements to the authorities
(EASA/FAA)
13
PFW Engineering
CAAC STC
We received recently the 1st CAAC STC for an A319
February 2014
14
Airframe
Capabilities
•
Development
•
Structural Design
•
Static / Stress
•
Fatigue / Damage Tolerance
•
Materials
•
Processes Surfaces
•
Lightning Protection
February 2014
15
System & Equipment
Capabilities
• Mechanical Systems
• Fluid Systems
• Engine and APU
• Environmental System
• Electrical System
• Avionics System
• Interior VIP
February 2014
16
Flight Physics
Capabilities
3,2% Landing, JAR 25.119
2,1% Approach, CRI B-1.6
February 2014
•
•
•
•
•
Performance
Handling
Loads
Weight & Balance
Flight Test
17
Structure
by ATA chapter
021A Stress Analysis, Static Strength
50 Structure Interface
021B Stress Analysis, Static Strength
51 Structure General Structure Repair
021C Structural Tests, Static and Fatigue
52 Doors, Doors Structure Repair
021D Stress Analysis and Static Strength
52A Doors Mechanics
022A Fatigue Strength
52B Doors Structure
023 Bird Strike
53 Fuselage, Fuselage Structure Repair
027 Sonic Fatigue
54 Nacelles / Pylons Structure Repair
082 Levelling133 Lightning Protection direct
and indirect effects and Bonding
541 Engine Support
134 Composites
543 Pylon 328-300
134A Surface Protection
55 Stabilisers, Stabilisers Structure Repair
135 Materials (non Composite)
56 Windows
542 Bridge 328-300
57 Wings, Wings Structure Repair
71 Power Plant Structure Repair
78 Exhaust Structure Repair
February 2014
18
System
by ATA chapter
024 Crash Worthiness
22
Auto Flight
36
Pneumatic
026 Cabin Decompression
23
Communication
38
Water Waste
046 Human Factors
24
Electric Power
45
047 MMEL
25
Equipment / Furnishing
Central Maintenance
System
11
26
Fire Detection
49
Auxiliary Power Unit
131 System Interfaces
27
Flight Controls
71
Power Plant
137 Emergency Evacuation
28
Fuel
72
Engine
136 Rotor Burst
29
Hydraulic Power
73
Engine Fuel and Control
151 EMC
30
Ice & Rain Protection
74
Ignition System
152 HIRF
31
Indicating & Recording
75
Air System
21
32
Landing Gear
77
Engine Indicating
33
Lights
76
Engine Controls
34
Navigation
78
Exhaust
35
Oxygen
79
Oil System
80
Starting
90
Electric
Placards and Marking
Air Conditioning
February 2014
19
Avionics
Substantiation Approaches
• PFW Engineering has gathered significant experience with different design and
substantiation approaches, depending on
– Customer (Aircraft/ Equipment OEM, Operator, Maintenance Organisation)
– Available data (e.g. with operational documentation only, or with OEM data based on
agreements with TC holder)
Substantiation:
e.g. CFD Analysis of 747-8 Camera
Installation
First installation:
On-Site Conformity Inspection and
Ground Test
Certification:
Boeing 747-8 Belly Camera –
Display on Pilot‘s EFB
Operation:
PFW Engineering provides in Service
Support for STC customers
February 2014
20
Technical Publications
for all aircrafts and customers
Entire Technical Publications Services required from an aircraft OEM:
Develop and update all necessary Information in creation of Manuals or Documents for:
– Aircraft Flight Operation (e.g. Airplane Flight Manual, AFM)
– Maintenance Planning (e.g. Maintenance Planning Document, MPD)
– Maintenance (e.g. Aircraft Maintenance Manual, AMM)
– Repair (e.g. Structural Repair Manual, SRM)
– Parts Identification (e.g. Illustrated Parts Catalogue, IPC)
– Data Management
– Approval of Manuals/ Changes to Manuals (as part of EASA 21J DOA
– Administration
– Distribution of Manual
– Revision Service
– Technical Publications as required for changes to external TCs (based on Supplemental
Type Certificates, STCs) - Creation, Approval and Distribution of Manual Supplements
as
– Hard Copies
– Electronic Data like SGML, HTML and PDF
– Document Viewing System CAMSIS 3
– WEB-Format
February 2014
21
Customer Services
History - Main activities
PFW Engineering took over the Fairchild Dornier/AvCraft EASA21J033 certificate
and the continuous airworthiness activities including customer support.
Today's team still has that core competence and today we support , upgrades,
training, STCs , Technical Publications etc.
Original just for the Dornier 328 and Dornier 328Jet, but today for various aircraft
including STC,s for A319, 747-800 and 767-400 VIP.
PFW Engineering has a Total Quality Management System that meets worldwide
recognized standards and reflects the state of the art for modern Quality
Management Systems.
Today’s PFW processes are based on Airworthiness Authority approvals:•EASA / LBA Design Organization approval to EASA Part 21 Subpart J
•Production Organization approval to EASA Part 21 Subpart G
•Maintenance Organization approval Part 145
•Approved Partner Training Organization to EASA Part 147 requirements.
Additionally our company possesses a Quality Management System approval in
accordance with ISO 9100 (equivalent to AS 9100) for Design, Production, Sales and
Maintenance.
FebruaryPFW
2014
© All EASA
rights reserved.
Reproduction
disclosure to third
of this document
or any part thereof for purposes
other than Part
intended for
by thisMaintenance
document, is not permitted, Organisation
: Certified
Part
21Jor Design
- parties
EASA
21G Production
- EASA
145
22
Customer Services
Capabilities - Maintenance Repair and Overhaul (MRO)
• PFW Engineering expertise in MRO support covers the entire range of
Engineering support, a Maintenance Organisation may require, e.g.:
– Design and Approval o Repairs on large aircraft (part ofDesign Organisation‘s 21J DOA
scope of approval)
– Minor/Major Changes (Design and Certification)
– Flight Testing under authority of an EASA 21J DOA
– Customer Support via PFW Engineering Customer Support Coordinator which provide
for example clarification if questions arise during installation of a Service Bulletin.
Sample pictures of PFW Engineering repairs
February 2014
23
PFW Engineering
Product Lifecycle
Design &
Engineering
Testing
+Qualification
+Technical Publications
Certification
EASA 21J
New
Technologies
Worldwide
Customer Support
Program
February 2014
Production
24
Project Management
EPM System
• Project Control
• Budget Usage and Technical
Progress
• Document Management (MS
SharePoint Services)
• Change Control and Claim
Management
• Resource Management
• Risk / Issues Management
• Online Collaboration
• Integrated Accounting – Realistic
Business Planning
• avoid any delays due to different
time zones.
February 2014
EPM – MS Project Server
Navision
Navision Resource = EPM Resource with costs
Project X
Project X
EPM Resource = Available person for GCT projects
Purpose: Project Availability, such as work hours,
calendar and absence.
EPM Resource
Pool
Deleted, with email notification,
manuell update in SM
EPM enabling seamless
integration of all its engineering
related activities with
administration, communication,
project management, and
financial functions.
Web based for Multi-site teams
using Microsoft Project Server for
Deleted
With email
notification
Internal Resource (manual update)
Temp
Resource Pool
Per Company
(new, deleted)
Navision
Resource
Pool
Internal Resource
in PayRoll
Company independent
resources
Status Hired
(not yet in EPM)
+ Email notification
Microsoft Dynamics
CRM
SM Resource
Skill Management
SM Resource = people that have shown
their interest for working at GCT.
Purpose: Skills
Integrated in Outlook
Project X
Opportunity
25
PFW the Company
Milestones
History – key milestones
1913
Nearly 100 years of experience in the aerospace sector
1937-1990
1991-1996
Formation of 'Pfalz Flugzeugwerke'
Unit of various companies, e.g. 'Flugzeugwerke
Saarpfalz' and 'MBB'
Part of 'Deutsche Airbus GmbH‘
(later 'Daimler-Benz Aerospace Airbus‘)
1997
Employee Buy-Out
2001
Acquisition by
Safeguard International Fund
2003
Formation of PFW HS (Turkey)
2004
Acquisition of RSM Aerospace (UK)
2006
Acquisition of Spécitubes
2008
Acquisition of 50,1% in HPL
2009
Acquisition of 100% in GCT
2009
Acquisition of 100% in HPL
2011
Airbus took over 74.9% of the shares
2012
Sell of PFW UK and PFW China
February 2014
Key figures 2011/2012
Sales
Employees
2011
227,4
2,164
Sales
Employees
2012
282
1,808
Employees excluding PFW temporary workers, including apprentices
Product groups
Cargo Laoding
Systems
7%
AeroStructures &
others
33%
Tubes & Ducts
60%
26
Today, PFW is present in Europe and North America
Production sites and Engineering offices
PFW Group Headquarters
Speyer. Germany
• c. 1260 employees
• Production and management
of all programmes
PFW (HPL)
Nuneaton / Farnborough, UK
• 42 employees
• Tubes, Pipes and Connectors for A350
PFW Engineering
Seattle, USA
Montreal, Canada
• 10 employees
• Design and engineering centre
February 2014
Spécitubes
Samer and Nanterre,
France
• 168 employees
• Precision tubes
PFW Repair Shop
Hamburg, Germany
• c. 8 employees
• Repair and
maintenance
PFW Engineering
Oberpfaffenhofen, Germany
Bournemouth, UK
Seattle, USA
Montreal, Canada
• 158 employees + 160 subcontractors
• Design and engineering centre
PFW HS
Izmir, Turkey
• 171 employees
• Assembly of auxiliary tank,
Structural Components, Inner Flaps
and production of tubes for Airbus
and the Boeing 787 “Dreamliner”
27
PFW Service Offerings
Product range
Tubes & ducts
Cargo Loading Systems
Structural Components
Engineering
February 2014
28
Technology Evolution
2002
CATIA V4
2003
CATIA V5
2004
CATIA V5
2005
GCE - CATIA V5
& ENOVIA
2000
CATIA V4 & VPM
1997
CATIA V3
1995
CADAM
2006/2008
CATIA V5
2009
GCE - CATIA V5
ENOVIA &
2010-2013 PRIMES
A350 XWB and
Boeing 787
CATIA V5
VVIP-STC
Customer
Services
February 2014
29
EDP, like CAD
Comprehensive Development Infrastructure
Design 2D & 3D
•
•
•
•
CATIA V6
CATIA V5
CATIA V4
CADAM (CCD)
Analysis Tools
DMU Tools
•
•
•
•
•
CATIA V5 DMU
Delmia
CATIA V4 4D Navigator
dVise
Product View
February 2014
PDM Tools
• Enovia
• Smarteam
• PRIMES
• TAKSY
• Systel
• PDM Editor
•
•
•
•
•
•
Patran / Nastran
Isami
Optistruct / Hypermesh
Ansys
MathCAD 2000
Interleaf
30
Quality Assurance
Certification
Compliance with the Quality Standards of
• EASA 21J.033 Design Organisation
• DIN EN 9100:2009 and EN ISO 9001
• Airbus Design Approval for all Airbus Sites including
Germany, UK, Spain and France
• AP1020 Approved via PFW
• Boeing QM Digital Product Definition D6-51991
• IAQG Oasis Membership
February 2014
31
PFW Engineering
a System Integrator
The PFW Engineering – The System Integrator
February 2014
32
Projects
Current Projects
Current Projects
February 2014
33
Interior Project
GORE Compilations San Antonio FIRST Boeing 787 VIP
February 2014
34
Boeing 787
Overview
•
B787 Tubing and Ducting Systems for complete Aircraft with PFW. Build to
Specification contract – Design, integration and build.
• B787 Section 46 Door Surrounds for IAI to Alenia. Design to Speciation
• B787 Horizontal Tail Plane, Section 30, leading & training edge and tip for IAI for
Alenia. Design to Specification.
• B787 Pax and Cargo Floor Sections 46 and 47. Supply of Manpower.
• B787 Horizontal Tail Plane, Weight Saving Section 30, leading & training edge and
tip for IAI for Boeing. Design to Speciation.
• B787 KHI Manpower Supply for Section 43
• B787 FHI Systems integration and secondary structure for centre wing box
Sections 11/45
• B787 Engineering Modifications for Boeing direct for all sections of Fuselage, with
team located in Everett Final Assembly Line, PFW Engineering Mukilteo and PFW
Engineering Munich. Approx 120 people.
• B787 Design and Stress mods to Section 46 for Alenia located at PFW Engineering
Munich.
• B787 KHI Stress mods to Fuselage located at PFW Engineering Munich
• Export License for sections of Boeing 787 and all commercial Boeing Aircraft
February 2014
35
Boeing 787-8
Overview – cont.
Mods to Aircraft Sections for FAL
Section 41, 43, 44, 46, 47, 48
Center Wing Box
Section 30
Section 45
Horizontal Stabilizer
Alenia Italy
Section 11
KHI Japan
FHI Japan
Section11/45 (Integration)
FHI Japan
Section 46
Alenia Italy
February 2014
36
Current Project
Aerolia – Mechanical Systems Bombardier G7000 / G8000 Centre Fuselage
Design and Installation of the following systems
ATA 21 –
ECS and LP
Ducting
February 2014
ATA 38 –
Water and
waste systems
ATA 24 – LRU’s
37
Current Project
Airbus A350XWB
•
A350 XWB Tubing and Ducting Systems.
•
A350 XWB Plateau Phase with EADS Germany for Fuselage Sections 13&14 and
components of the Fuselage Sections 16&17.
•
A350 XWB Premium Aerotec Sections 16- 18 Side Shells and Pax Door Surrounds
•
A350XWB S16-18 Lower Cargo Framework.
•
A350XWB S16-18 Crossbeam Struts.
•
A350XWB S16-18 Floor Grid.
•
A350 XWB Aero Data for Loads Production.
•
A350 XWB CFD Calculations
•
A350 XWB Aerodynamics
•
A350 XWB Flap Sizing
•
Spice new galley system. Concept during last four years with Airbus and Airlines
February 2014
38
Current Project
ATR 42-500 Flight Inspection Conversion
• Currently PFW Engineering is working on an ATR 42-500 Flight Inspection System
Integration STC
ATR 42-500
• The project consists of following
modifications (per area):
– Flight Deck modification:
• Integration of 1 new Nav Display
• Integration of 1 new EHSI
(Bendix King)
• Centre pedestal layout change
• Relocation of existing units
• 2 additional push button panels
• C/B panel modification
– Antenna Installation
• 11 additional antennas as part
of the flight inspection system
– Interfaces to basic aircraft
avionics
• Integration of Arinc Decouplers
• Integration of Arinc Converters
ATR42-500 fuselage
– Interfaces to basic aircraft
electrical power system
• Development of an Automatic
load shedding logic
February 2014
Mission Rack Display (Cabin)
ATR42-500 Flight Deck- Modification Areas
Flight Inspection- Pushbutton panel
39
Airbus A350XWB (B2S)
Tubes and Ducts – cont.
• The marketing campaign started already in April 2007
• During 2009, PFW was awarded six Tubes and Ducts packages for the A350 XWB
• Fuselage Fuel/Inerting
• Fuselage Pneumatics
• Wing Fuel/Inerting
• Wing Pneumatics
• Wing Hydraulics
• Cargo Drainage
• The development program for these packages
started at the end of April 2009
A350 Wing with
PFW Fuel Pipes
February 2014
A350 Fuselage Section
with PFW Fuel tubes and
Pneumatic Ducts
40
Airbus A350XWB (B2S)
Tubes and Ducts – cont.
What is the PFW A350 XWB Tubes and Ducts Program?
• An international PFW Group program
• Making PFW a global player
• Multi-site teams – Hamburg, Toulouse and Filton
• Concurrent Engineering – different disciplines, e.g. design, ME, stress, production,
procurement etc. working together to ensure the most optimum design is achieved
• Introducing new technologies
– Wing Fuel System - Composite Tubes
– Fuselage Fuel System - Injection Molded PEEK Connector
– Cargo Drainage System – Heat forming of PEEK tubing
February 2014
41
Airbus A350XW-900-1000, Section 13/14-16/18
Stress: F&DT
• Fatigue justification for all metallic parts in Section 13/14-16/18
• According to the handbook FDT Issue 3, A350XWB
• Typical Parts:
– DFEMs typically used for
• Z-Strut attachment (Frame side).
• Shear ties
• Corner Fittings
– GFEM typically used for
• Hybrid couplings
• Metal couplings
• Tool-set for F&DT analysis
–
–
–
–
–
–
–
–
ISAMI version 7.2.1 or higher
Detailed FE-work with HyperWorks / Patran Nastran
3D – Joint Analysis
Frame Splicing Module
ISAMI Spectrum Analysis (1D/2D - FUEgen)
STF Tool
AFI Analysis (by Hand)
Lug analysis,
February 2014
A350 Fuselage Section
Definition of AP
42
Airbus A350XWB
A350XWB-900 and -1000 Sections 16-18
• left & right CFRP side shells including: Skins, Frames & Stringers
• Fibresim & V5 CPD
February 2014
43
Airbus A350XWB
A350XWB-900 Sections 16-18
Left & right PAX door surrounds
February 2014
44
Air Astana: Boeing 757-200 Interior Change
Engineering: STC
• Retrofit Campaign (Program), including Project Management
• As part of a maintenance layover, we modify the interior of 5 Boeing 757-200 MSNs currently
configured according to three different LOPAs
• The modifications are a change to type design, requiring a 21J DOA Approval (STC).
• The project results in an EASA STC as well as installation instructions for five aircraft MSNs.
After project end obligations (e.g. Continued Airworthiness tasks) as well as commercial rights
remain with PFW
• Scope of Work:
– Three A/C (P4-EAS, P4-FAS, P4-GAS) have the identical LOPA and will be upgraded
with new economy seats and IFE and an improved cabin appearance
– Two A/C will be upgraded with improved cabin appearance only
February 2014
45
Interior Projects
B767VIP, A319 Fin Camera and B787-8 Belly Fairing Camera
Supplemental Type Certificates (STCs)
February 2014
46
LHT: Attendant Seat for Boeing DLH 747-8 and A380
Engineering: Certification, PFW is a 21J partner for Design and Certification
• Design and Certification of Structural Provions for Cabin Attendant Seats on DLH 747-8i and
A380
• This modification program is to integrate a Patient Transport Compartment (PTC) on the
Lufthansa A380 and 747-8I aircraft, including:
– two High Comfort Cabin Attendant seats (HCCAS) for doctor and medical staff - one fwd facing, one aft
facing HCCAS, in total three of the Lufthansa 747-8 and three of the A380 will be equipped
• The installation shall be certified with EASA STC or an equivalent minor change approval
under the PFW DOA
• During the initial installation PFW will provide on-site support
February 2014
47
Projects
Previous Projects
Previous Projects
February 2014
48
Interior Projects
VIP STCs for a new Completion Centre
February 2014
49
Interior Projects
VIP STCs for a new Completion Centre
GCT Activity prior 1st A/C
Manuals
Str.
Cabinet
Description
A CTION
Panel Joints (M&T, T&G, Folding)
Concepts and Test Plans
Floor Attachments
DWG/Test
Panel Splices
DWG/Test
Standard Access Panels
DWG
Ground studs
Concept
Edge filling
SRT to issue PPS
Bonding
Concept/Test
Inserts
Concept/Test
Cabinet Lighting concept improvement
Concept
Deco Panels attachment
Concept
Drawer Concept and Front Panel
Concept
Decompression Panels
Preferred release elements - Definition
Doors - concepts for Decompression
As typical design
Adjustable shelves - Concept
As typical design
Slides
Slide Concepts/PN
Waste Bin
Concept
Access Panels
Concept
Internal Door Locks
Concept/PN
Hard Point Standard Design (Boing/Airbus)
Concept
Tie Rods
Attachment and Rods Definition
Air conditioning balancing expertise
Concept
Temp sensor Instl
Concept/PN
Motor valve Standard
Concept/PN
Solenoid valve standard
Concept/PN
Water system Standard fittings
Concept/PN
Gray water chamber
Concept/PN
Water heater standard
Concept/PN
Vent muffler
Concept/PN
Typ Tape heater
Concept/PN
Air conditioning ducts
Concept/PN
Material Manual
Manual
Standard Part Catalog
Manual
Design Manual
Manual - Update to be released
Model and Drawing Manual
Manual
February
2014 Standard Parts
Electrical
Catalog
Manual
except
with prior and express written
permission by PFW Engineering
50
Previous Projects
Airbus A380
•
A380 Integration of ALL Tubes and Ducts Systems
•
A380 Design of Floor Structure and Integration of Systems Sections 13, 18 and 15.
•
A380 Interiors Furnishings, Project Managing Customer Requirements Galleys,
Passenger and Cabin Attendant Seats, Trolley Lift IFE and Passenger Seat
Electrical Integration
•
A380 PAX Interior Provisions and Electrical Brackets. Secondary Structure
•
A380 Technical Publication Transnational Network, AMM, TSM, TDUR, CMM, DRM,
MAP, TLS
•
A380 Supply of Engineers
•
A380 FTI
•
A380 Change Management
•
A380 Wing jig Analysis
•
A380 Aircraft Master Surfacing & Geometry including Status 15a
•
A380 Slat and Flap Mechanical Systems and Flap Tracks
February 2014
51
Previous Projects
A380 Belly Fairing
2001-2002
Preliminary Design
2003
Detail Design
2003-2004
Certification
• Preparation of
Technical
Specifications in
response to Airbus
RFI and RFP.
• Supply of
Contractual Stress
Engineers,
Conceptual
Designers and
Detail Design
Engineers using
Catia Version 5 and
VPM
• Supply of
Certification
Designers
• Calculation of NRC
and RC Costs
• Project Managing
Bidding Programme
including Planning
and QA activities
• Development Design
and Integration in DBT
in Airbus Spain
February 2014
52
Previous Projects
A380 (EADS Ottobrunn)
A380 – Design and Integration of all Standard System Mountings
for Aluminium Crossbeams – Sections 13, 18 and 15 forward
upper unit.
• Responsible for full project management and control with a team ‘on-site’ in Airbus
Hamburg.
• Data Transfer established and managed to allow detail design and manufacturing
drawing release by a team ‘off-site’.
• Liaison and agreement of interfaces with the following systems: Hydraulics,
Water/Waste/Vacuum, Electric/Fuel/Bleed Air, Supplementary Cooling, Air
Conditioning
• Involvement in all phases from joint definition, detail design through to release of
manufacturing drawings and production support.
• All designs agreed with the relative manufacturing partner.
February 2014
53
Previous Projects
A380 PAX
A380 PAX Interior Provisions
• Development Design Team located in CDBT at Airbus Hamburg
• Development of Interior Components for different HOV
• Development of Brackets and Structural provisions for:
– Galley UD
– Lavatory / BAR UD
– Partitions / Minisiuts UD
– Spacers UD
– Bonding UD Monuments
– Attachments for Stairs house lining FWD
– Side wall Stowage
February 2014
54
Previous Projects
A380 – Analysis of transportation system for the wing
• Combination of Wing, Jig and Trailer models
• Calculation of total deflections of different combinations
• Assessment of different models and design solutions
February 2014
55
PFW Engineering Previous Projects
Airbus A400M
• A400M Supply of Engineers
• A400M Flap Tracks Structural Design
• A400M Whole Aircraft Master Surfacing & Geometry
• A400M Main Cargo Floor and Ramp.
• A400M Cargo Loading System and Air Deployment System
• A400M Inlet, Outlet and Heat Exchanger
• A400M ECS NACA Inlet and Plenum
• A400M OBIGGS Ram Air NACA Inlets and Outlets
• A400M Technical Publication Transnational Network defining all WP for the all
technical documentation of the A400M.
February 2014
56
Previous Projects
A400M main cargo floor, CLS and ADS
A400M main Cargo Floor and Ramp
• Development, Design and Stress
• Compliance and certification documentation
• Final release of Manufacturing drawings
• Catia V5 and PRIMES
February 2014
57
Previous Projects
E2S A320 P2F – PAX to Freighter conversations
•
PFW Engineering has gained experience in PAX-Freighter-Conversions while
working for Elbe Flugzeugwerke (EFW)
•
A320 P2F floor grids, floor panel modifications, development of a main deck cargo
door frame shell including
•
Skin panels and doublers
•
Frame and frame coupling
•
Clips for frame skin connection
•
Stringer
•
Butt straps
•
Cleats
•
Door surrounding for cargo door
•
Brackets
•
System modifications
•
Stress
February 2014
58
Previous Project
XAC PAX Door MA600 and MA700
Study on the MA600 door
delivered successfully in
September 2012
Bidding for the MA700
design and build
February 2014
59
Previous Projects (Interior)
Fairchild Dornier 328 JET and 728 JET
VIP Interiors 328JET– Toliets
Design & Mockup728JET
February 2014
12 Seater 328JET VIP Cabin
VIP Interiors 328JET
12 Seater 328JET VIP Cabin
Airbus - SPICE
60
SPLICE
• PFW objectives & deliverables;
– Achieve next generation efficient modular cabin
monument design concepts.
– Make use of new advanced materials
– Create mission adaptive onboard service
equipment
– Perform technical research and development into
Modular / flexible definitions whilst achieving
certification requirements.
February 2014
61
SPLICE
February 2014
62
A380 and RECARO Aircraft Seating
A380 Interiors Business Class
Business Seat 6510
(RECARO)
February 2014
Economy Seat 3510
(RECARO)
63
Fairchild Dornier 728 JET
• In-house Work package Milestones for Structure and
Systems Integration
• Supply of over 200 Aerospace Engineers
February 2014
64
Previous Projects
Fairchild Dornier 728 JET – Belly Fairing
Wing Front Spar
MLG Door
Substructure
Wing Rear Spar
Fuselage Keelbeam
February 2014
65
Previous Projects
Fairchild Dornier 728 JET
Complete Cabin Interiors Industrial Design and
Full Size Mock-up for Farnborough 1998
• Development, Detail Design and Integration of the
728JET Insulation Blankets for Mexmil Inc.
• Preparation of PDR and CDR documents.
• Control of Concessions, Change Control and
Configuration of first prototype.
February 2014
66
Previous Projects
ARJ 21 Controls
Design of Rudder Pedals & Control Column for the ARJ21
February 2014
67
Previous Projects
Fairchild Dornier 428 JET Wing Structure and Systems
FD428JET Wing
Prime Contractor to Fairchild Dornier and IAI
Major Wing Components
FEM - Pylon
Pylon
Spar Box
“Hot” Leading Edge
Wing/Fuselage
Attachment
Wing Tip
Ground Spoiler 1
Aileron
Roll Spoiler
February 2014
Flap
Ground Spoiler 2
68
Previous Projects
Fairchild Dornier 428 JET Structures from IAI
428JET Cockpit, Fuselage& Empennage
Prime Contractor to Fairchild Dornier and IAI
FD 428JET & 728JET
Cockpit & Cabin Layout
428JET Empennage
February 2014
69
Previous Projects
Aermacchi M346 Cockpit Structures and System Integration
Aermacchi M-346 Advanced Trainer
Prime Contractor to Aermacchi
• Flight & Engine Controls
• Cabin Pressurisation
• Canopy Locking & Explosives
• Head-up Display
• Anti-G
• Emergency Landing Gear, Brake
• Seat Installation & Ejection
• Oxygen Supply
• Hydraulics & Fuel
and Park
• Inflatable Seal
• Electric Equipment
• Consoles & Panels
• Avionics
• Air Distribution
February 2014
70
Interested in our service?
Please contact us!
PFW Engineering
Sonderflughafen Oberpfaffenhofen
Building 335
82234 Wessling
Germany
Phone: +49 8153 9313 0
Fax: +49 8153 9313 999
Web: www.pfw.aero/engineering
Nigel Garner
PFW Global Sales
Phone: +49 8153 9313 210
Mobile: +49 172 8498640
Fax: +49 8153 9313 999
E-mail: [email protected]
Thank you
for your time!
February 2014
71

PFW Engineering - Presentation

Transcription

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