1 Electroimpact Proprietary About Ben Hempstead, PE BSME - - PowerPoint PPT Presentation

1
SMART_READER_LITE
LIVE PREVIEW

1 Electroimpact Proprietary About Ben Hempstead, PE BSME - - PowerPoint PPT Presentation

1 Electroimpact Proprietary About Ben Hempstead, PE BSME University of Washington Started at EI in 1994 Mechanical Engineer (Lead) for automation projects Chief of Staff 2 Electroimpact Proprietary Electroimpact is a world


slide-1
SLIDE 1

Electroimpact Proprietary

1

slide-2
SLIDE 2

Electroimpact Proprietary

About Ben Hempstead, PE

  • BSME University of Washington
  • Started at EI in 1994
  • Mechanical Engineer (Lead) for

automation projects

  • Chief of Staff

2

slide-3
SLIDE 3

Electroimpact Proprietary

Electroimpact is a world leader in design

  • f automated aerospace assembly

equipment.

Completing large scale projects for companies including Airbus, Boeing, SpaceX, NASA, Spirit Aerospace, Northrop-Grumman, Lockheed, XAC/AVIC, Bombardier, and Embraer among

  • thers.
slide-4
SLIDE 4

Electroimpact Proprietary

ELECTROIMPACT, Inc.

  • Founded in 1986 by President Peter Zieve Ph.D.
  • Since 1987 Vice-President John Hartmann
  • Since 2014 Vice-President Michael Zieve
  • 766 Employees worldwide
  • 615 Full-time Degreed Engineers (80%)
  • Offices:

– Mukilteo WA 595 employees + interns – Hawarden UK 130 employees – Filton UK 3 employees – Melbourne Australia 1 employee – Charleston SC 2 employees – Wichita KS 1 employee – Evora Portugal 3 employees – Ankara Turkey 1 employee – Xian China 8 employees – Toronto 1 employee – Belfast 1 employee

4

slide-5
SLIDE 5

Electroimpact Proprietary

History of Employment

5

slide-6
SLIDE 6

Electroimpact Proprietary

Mukilteo, Wa Campus

6

slide-7
SLIDE 7

Electroimpact Proprietary

Broughton, UK Campus

7

slide-8
SLIDE 8

Electroimpact Proprietary

Electroimpact Properties

8

slide-9
SLIDE 9

Electroimpact Proprietary

slide-10
SLIDE 10

Electroimpact Proprietary

Organization Highlights

  • Engineering Focus
  • Vertical Integration
  • Concentrated Responsibility
  • Communication Methods
  • Data storage and accessibility
  • Personal responsibility and integrity

10

slide-11
SLIDE 11

Electroimpact Proprietary

EI Systems Integration Experience

  • 28 years of in-house Production Auto-Fastening

Machines

  • 23 years of Turnkey Aircraft Assembly Systems

Supply

  • 18 years of Production Tool Design, Fabrication and

Metrology

  • Boeing (NWP) Approved Design/Build Tooling

Supplier

  • Full Integrated Project Teams under one roof.
  • Fully developed international supply chain.
  • Responsive Local Support for all engineering

disciplines

11

slide-12
SLIDE 12

Electroimpact Proprietary

12

slide-13
SLIDE 13

Electroimpact Proprietary

Wing Spar Fastening

13

slide-14
SLIDE 14

Electroimpact Proprietary

Wing Skin Fastening Systems

Flexible A380 A380 A340 A320

14

slide-15
SLIDE 15

Electroimpact Proprietary

Post Riveting Machines

15

slide-16
SLIDE 16

Electroimpact Proprietary

16

Flextrack

slide-17
SLIDE 17

Electroimpact Proprietary

Robot Drilling/Fastening

17

slide-18
SLIDE 18

Electroimpact Proprietary

Automated Fiber Placement Machines

18

slide-19
SLIDE 19

Electroimpact Proprietary

Time for a Break!

Videos of Automated Fiber Placement Machines

EI’s AFP Channel on Youtube: https://www.youtube.com/user/AFPatEI NASA Marshall Robotic AFP: https://www.youtube.com/watch?v=uWhoV0 2AuTU

19

slide-20
SLIDE 20

Electroimpact Proprietary

20

Integrating Tooling & Automation – A380

slide-21
SLIDE 21

Electroimpact Proprietary

PAL – 737

21

slide-22
SLIDE 22

Electroimpact Proprietary

Wing Assembly Lines

22

slide-23
SLIDE 23

Electroimpact Proprietary

23

EI Automated Wing Assembly Systems (34 In Production to Date)

A380 A400M A350 CSeries Legacy KC390 C919 777x (in design)

slide-24
SLIDE 24

Electroimpact Proprietary

A350 Wing Assembly

24

slide-25
SLIDE 25

Electroimpact Proprietary

Secondary position feedback

  • * Mount at axis output * for each of the 6 robot axes (EI Patent Pending)
  • Control axis position directly from secondary feedback

Accurate Robots

slide-26
SLIDE 26

Electroimpact Proprietary

Results:

  • Test 1a: Off-part accuracy, entire volume: +/-0.0063” 3-sigma
  • Test 1b: Off-part accuracy, entire volume: +/-0.0049” 3-sigma

Accurate Robot – System Validation

Axes in mm 0.25mm = 0.010” Axes in mm 0.25mm = 0.010”

slide-27
SLIDE 27

Electroimpact Proprietary

787 Trailing Edge Assembly

27

slide-28
SLIDE 28

Electroimpact Proprietary

HISTORY AND OUTLOOK

Riveting and Composites

28

slide-29
SLIDE 29

Electroimpact Proprietary

C-17 Spar Machine

  • EI designed, built, and installed the ASAT4

spar riveting machine and fixtures in 1998

  • 3-axis riveter and servo-controlled fixture
  • Purchase customer was McDonnell-

Douglas

  • Boeing & M-D merged before handover
  • October 2014 the 279th and final spar set

was built

  • System sold at auction in 2015

29

slide-30
SLIDE 30

Electroimpact Proprietary

C-17 Spar Machine

30

slide-31
SLIDE 31

Electroimpact Proprietary

C-17

31

slide-32
SLIDE 32

Electroimpact Proprietary

Economic Forecast for Projects

  • Boeing:

– Mostly 777x

  • Embraer:

– Mostly E2

  • Airbus:

– A350 and refurbs

  • Other

32

slide-33
SLIDE 33

Electroimpact Proprietary

What is a Composite Aircraft?

33

http://aviation-futur.e-monsite.com/medias/images/787-1.vs

787 777x

A350 has CFRP fuse panels

slide-34
SLIDE 34

Electroimpact Proprietary

Published Customer Backlog

Boeing & Airbus Only

34

Assumes a multiplier between 6-10 representing the additional “work” required to build wide-body aircraft. Backlog as reported on Boeing and Airbus commercial aircraft websites as

  • f 2/1/16.
slide-35
SLIDE 35

Electroimpact Proprietary

C-130J Aft Fuselage

35

slide-36
SLIDE 36

Electroimpact Proprietary

C-130J – Why a new Machine?

  • Rate increase due to recent sales
  • Aging workforce
  • Quality concerns with manual work
  • Engineering solution for the lower ram
  • Smaller footprint than legacy machines
  • Siemens control vs Fanuc

36

slide-37
SLIDE 37

Electroimpact Proprietary

C-130J Flaps

37

slide-38
SLIDE 38

Electroimpact Proprietary

777x Center Wingbox

38

slide-39
SLIDE 39

Electroimpact Proprietary

Riveting Machine Outlook

  • EI believes there is a significant market &

is aggressively developing new technology

  • 737 backlog is 8 years at current rates
  • 777x riveted fuselage is not even in

production yet

  • E2 and other regional aircraft are riveted

39

slide-40
SLIDE 40

Electroimpact Proprietary

Composites Outlook

  • CFRP wingboxes for wide-bodies are here

to stay

  • Aluminum looks to be better for fuselages
  • Will CFRP make its way into the single-

aisle product?

– Bombardier’s Cseries is interesting

40

slide-41
SLIDE 41

Electroimpact Proprietary

777x Skin and Spar AFP

  • EI is currently installing carbon fiber

lamination machines that are purpose-built for the 777x wing skins and wing spars.

  • We are contracted to deliver 2 of each

type.

  • Future orders will depend on the need and

performance of the overall cell.

  • Installation in Everett, WA.

41

slide-42
SLIDE 42

Electroimpact Proprietary

777x Wingbox Assembly

  • EI is under contract to design, build, and

install the factory system for wingbox assembly

  • Tools to fixture the spars, ribs, and skins
  • Machines to drill and fasten skins to ribs

and spars

  • Material handling equipment to pulse the

wingbox and parts

  • Installation in Everett, WA

42

slide-43
SLIDE 43

Electroimpact Proprietary

Summary

EI provides equipment and tooling with Predictable and Verified Performance to meet design requirements. Questions? benh@electroimpact.com 425 609 4980

Find me on:

https://www.linkedin.com/in/benhempstead

Also TEDx on Youtube:

https://www.youtube.com/watch?v=r540VOI Vufc

43