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BOEING END EFFECTOR

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BOEING END EFFECTOR ME 416 Washington State University Boeing End Effector Problem Statement Design an End Effector Used to remove or install aircraft components ... – PowerPoint PPT presentation

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Title: BOEING END EFFECTOR


1
BOEING END EFFECTOR
  • ME 416 Washington State University

2
Boeing End Effector
  • Group Members
  • A.M.
  • Adam Dirkes, Jared Haight, Luna Michael
  • P.M.
  • Brett Buchholtz, Bryce Eschenbacher, Chi Jinchi,
  • Chung-Chi Chen, Jayson Eleccion, Shuko Kusaka

Contact Alex van Schoonhoven
3
Problem Statement
  • Design an End Effector
  • Used to remove or install aircraft components
  • specific needs provided by Boeing
  • Boeing has requested our services to build a
    manipulating end effector
  • End Effector must connect to existing hoist
  • Will be used to remove parts for maintenance
  • The end effector should be capable of translating
    three inches and rotating 30 degrees in the x, y
    and z planes.

4
Key Needs
  • 6 degrees of freedom
  • 3 inches of controlled linear movement
  • Rotational movement of 30 degrees
  • Lift 100-150 lbs
  • Weigh less than 250 lbs
  • Capable of removing/installing components safely
  • Compatible with existing boom

5
Design Concepts
Conceptual Design 1- Stewart Platform
  • Design Basics
  • Two parallel plates
  • Six triangulated pistons
  • Coordinated movements facilitates six degrees
    of freedom
  • Universal joints connect the piston to the
    plates

A Stewart Platform basically consists of a base
(lower platform) and end effector (top platform)
connected by six actuator driven legs.
6
Design Concepts
Conceptual Design 2- Translational Plates
  • Design Basics
  • Power jacks used for translational movement by
    way of worm gears
  • Power jacks provide the 3 axis of lateral
    movement
  • Rotational movement provided by an arm and
    piston mechanism

7
Final Design
  • Vertical Motion (translational and rotational) is
    controlled by machine screw jacks.
  • Translation in Horizontal plane controlled by
    lead screws and linear bearing.
  • Last two degrees of rotation controlled by
    turntables.

8
Benchmarking
  • Majority of Metrics and needs met
  • Strength
  • Travel and Rotation Distance
  • Ease of Operation
  • Translation/Machine Jack Controllability
  • Some metrics were not fully met
  • Turntable Controllability
  • Volume of End Effector
  • Weight of End Effector

9
Manufacturing Report
  • Manufacturing required basic shop skills
  • All plates cut using a shear
  • Drill press used to drill and tap all holes
  • Welding was done by Norm Martel (in charge of ME
    student shop)
  • Minimal Mill and Lathe work was necessary
  • Materials Used
  • Hot rolled low carbon steel was used for all
    plates
  • Brass ACME lead screws and nuts
  • All bolts and screws are SAE Grade 5 or higher
  • Linear bearings made of 10-60 Al with Teflon
    coated sliders

10
Bill of Materials/Cost
Total Cost 2,755.30 (Parts only, no labor)
11
Acknowledgements
  • Special thanks to the following people who
    contributed to the successful completion of this
    project.
  • Dr. Chuck Pezeshki
  • Dr. Findley
  • Kelley Racicot
  • Alex van Schoonhoven
  • Alan Cooke
  • Norm Martel
  • Jon Grimes
  • Robert Ames

12
Any Questions?
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