Kim Allen, Sam O’Flaherty, and Austin Schantz. Design NOTE: All dimensions are in inches 3D Conceptual Design Front View Side View Top View.

Slides:



Advertisements
Similar presentations
PHYSICS 1401 JEFFERY DING ALAN JONES
Advertisements

Team Members: Jon DixonMatt SacksDarrin BeamNathan Murray
Suspension Systems - 1 Topics covered in this presentation:
James Rasmussen.  Original dash was made from sheet metal, foam, and vinyl  Was too heavy for its purpose  Didn’t offer standard gauge sizes  Didn’t.
AeroE 423 Composites Travis Brotherson Kevin Howard Mike Nielsen 1.
Frames, Forks, and Wheels Eliza Davis and Emma Wingreen.
Professor Joe Greene CSU, CHICO
Rolling Chassis Team Todd Anderson Matt Blackwood David Hovater Josh Smith Jessica Yoho.
Moments of Inertia Polar moment of inertia – Used when calculating the torsion – Indication of resistance to torsion – Solid Shaft – J = π R 4 / 2 Area.
Anatomy of A Bridge Atin Sinha, Ph.D., P.E. Albany State University Anatomy of A Bridge Atin Sinha, Ph.D., P.E. Albany State University.
Wall Form Design Example (Continued)
Optimization of the Oscillating Hydrofoil Propulsion System Sarah Blake, Scott Eaton, Mary Girard and Hassan Mazi Advisor: Michael “Mick” Peterson, Ph.D.
Vertical-Axis Wind Turbine Kang Zheng Aaron Peterson Mohd Ramjis.
University of the Pacific 1 Parabolic Food Aid Delivery System Mishari Al-Nahedh Chia Lee Lisa Mak December 5, 2002 Engineering 5 Section 6 University.
Feasibility MSA P Base Plate Feasibility 3 plastics were looked at for MSA mounting board material: ABS, Acrylic, and polypropylene. Due to cost.
1 New Castle Design Associates PROJECT Composite Generator Enclosure Team 12 Justin Schaffer Tom Winward Noel Goldstein Jeremy Freeman Members:
THE WASHINGTON MONUMENT (1884) The purpose of this study is to show how this structure supports its own weight and wind load, by calculating its efficiency.
Structures and stress BaDI 1.
University of the Pacific 1 Parabolic Food Aid Delivery System Mishari Al-Nahedh Chia Lee Lisa Mak December 5, 2002 Engineering 5 Section 6 University.
ME104Q PAPER RIVER CHASM BRIDGE Team Boomerang Mechanical Engineering University of Rochester Executive Summary The premise of this experiment is built.
Team 7: Vincent Borsello, Michael Brill, Daniel Gempesaw, Travis Mease
Dane BatemaBenoit Blier Drew Capps Patricia Roman Kyle Ryan Audrey Serra John TapeeCarlos Vergara Team 1: Structures 1 PDR Team “Canard” October 12th,
Home Work #7 Due Date:29 April, 2010 (Turn in your assignment at the mail box of S581 outside the ME general office) The solutions must be written on single-side.
Team 5 Structures PDR Presented By: Ross May James Roesch Charles Stangle.
CTC / MTC 222 Strength of Materials
CLARKSON UNIVERSITY Department of Mechanical and Aeronautical Engineering Introduction to AIRCRAFT STRUCTURES Ratan Jha (CAMP 364, ,
 The axle shaft (half shaft) transmits the drive from the differential sun wheel to the rear hub. The arrangement of a simple rear axle can be seen in.
Final Presentation Crew: Mike Lanteigne Wallace Barkhouse Scott Donahoe Blair MacKay Captain: Dr. Jimmy Chuang April 4 th 2012.
Pulleys Simple Machines.
Structural Member Properties Moment of Inertia (I) is a mathematical property of a cross section (measured in inches 4 ) that gives important information.
Sandwich Construction Thin composite skins bonded to thicker, lightweight core. Large increase in second moment of area without weight penalty. Core needs.
Structural Engineering
Telescoping Wheelchair Ramp
Open Differentials Naeem Shariff.
MECHANICAL ADVANTAGE.
Braking System for a Hospital Bed Approach Calculations Design Team Nicholas Beechnau Aaron Cole Nicholas Nwabueze Matthew Hays Brainstorming sessions.
Factor of Safety (Safety Factor) In the calculations, Material strengths, Manufacturing process Is used to provide a design margin over the theoretical.
A PRESENTATION on “ SUSPENSION SYSTEM ”
Composite Panels & Adhesives. Composite Panels Panels are fiberglass on both sides with a core in the middle consisting of either foam or a honeycomb.
NCSX Modular Coil Turning Fixture FDR. Background Modular Coil winding forms are cast structures which provide the foundation on which the coils are constructed.
Engineering 309: Machine Design I Instructor: Dr. Min Lu Presented by: Mike Kraft Thanh Nguyen.
Mousetrap Car TIPS View in full slide show mode and use headphones
VXD Mechanical R&D at the University of Washington H. Lubatti, C. Daly, W. Kuykendall LCRD in conjunction with Fermilab, SLAC.
Case Studies Chapter 1 Design using Carbon Nanotubes.
Composite Materials Manufacturing Composite Materials Manufacturing 정분방.
AerE 423 Ehrich Rodgers and Nick Williams. Background -Golf shafts provide a way for the golfer to generate force on the golf ball -To do this the golfer’s.
Paper Structure. Problem  Design, construct and test a structure that will support lbs.
PRY Base - Contents l PRY Support/Base/Platform in the MICE Hall l Requirements l Environment l Design l Structural Integrity l Preparation l Installation.
Sam Krueger.  Entertainment Center  Preliminary design  Initial  36 plies, glass epoxy  [0 11 /±45 1 /90 5 ] s  No core  Modified design  36 plies,
Engineering/Failure Analysis
Structures PDR 1 Team Boiler Xpress Oneeb Bhutta Matthew Basiletti Ryan Beech Micheal VanMeter October 12, 2000.
{ Catapult Project. We started with just a ¾ inch piece of pvc pipe and decided we needed it more rigid.
23rd ANNUAL BATTERY CAR RACE FEB. 27,2015 BY: Homer Johnson & Sammy Smith (Ingomar Middle School) (Picture of car here) Car Name: THE ROAD RUNNER.
Adrian Garza.  Composites of structural fibers like carbon are used for the frame  Wheels, derailleurs, brakes, and chains, are made with stainless.
Engineering Analysis October 23, 2006 Team Moondogs Chris Culver Rahul Kirtikar Elias Krauklis Christopher Sampson Michael Widerquist.
Reinforcement Information - Code
1 ASU Satellite Laboratory Fuselage Design Presenter: Eric Chen.
1 MFGT 104 Materials and Quality Compression, Shear, Flexural, Impact Testing Professor Joe Greene CSU, CHICO.
© Goodheart-Willcox Co., Inc. Wheels and Tires Unit.
NASA Great Moonbuggy Race 2012 SpacePokes Design Lesley Young Leader Davis FayRecorder Alisa FrohbieterProject Engineer Ryan WilliamsProject Engineer.
Composite Joining Techniques: Bolted Joints LBNL Composites Workshop February 29-March 3, 2016.
Eric McDonald Drew Krutak Jeremy Hanneman. Our objective was to design and fabricate a High-Speed Treadmill that is capable of measuring the horizontal.
AVIVA™ ELECTRIC BIKES VIPER ASSEMBLY INSTRUCTIONS Aviva™ - For A New Way Of Life.
Tim Wyckoff David Cenidoza Sachin Narvekar Felix Liu Weston Wells
Stresses, Strains and Deflections of Steel Beams in Pure Bending
GROUP NINE Cross-Slope Compensation for Wheelchairs
Bridge Project: Team Truss-Arch
Introduction to Structural Member Properties
Suspension Systems - 1 Topics covered in this presentation:
Gravity Vehicle San Diego Regional.
Presentation transcript:

Kim Allen, Sam O’Flaherty, and Austin Schantz

Design NOTE: All dimensions are in inches 3D Conceptual Design Front View Side View Top View

Force Calculations

Force Calculations Continued  Known values F p =250 lbsFS=3 W=575 lbsFS=3  Calculated Values F w = lbs F B = lbs

Force Calculations Continued  Max Deflection=.1 inch  From this Max strain ε max-B =.025 ε max-w =  If F B = lbs Then σ B =F B /A=1.553 psi E B = σ B / ε max-B =61.32 psi= GPa  If F w = lbs Then σ w =F w /A=7.977 psi E w = σ w / ε max = psi=.0121GPa

Composite Design Theoretical Values E 1 (GPa)E 2 (GPa)G (GPa)ν In-Plane Load Bending Load  Initial Values  Calculated Values  Note that the E max =.0121 GPa. This composite lay-up should hold E 1 (GPa)E 2 (GPa)G (GPa)ν S-Glass Fiber/Epoxy Closed Cell Foam Core

Test Section  Small section with same material layup as project  Planned Use: Find the maximum compressive and torsion load the layup could withstand  Actual Use: Identify the difficulties in manufacturing and bagging a 3-D project

Manufacturing  Foam Core Construction Hot WireDrilling the hole for the axle Sanding

 Foam Core

 Laying Up the Foam with Glass Fiber Composite Beginning the Lay-up The Big Wheel Bagged and ready for vacuum curing

 Attaching Front yoke and Preliminary Testing Drilling Holes for BoltsAdjusting Yolk Making sure it holds our weight Making Sure it Moves Smoothly Making Sure it moves and can hold extra weight

Final Product

Testing  Testing Plan Ride around a parking lot Basic turns Riding up a small ramp Test completed 3 times  Results Tests completed successfully Withstood pull-up and torsion forces

Conclusion  Successes Weight rated for an adult rider Withstood forces Project completed!!!!!  Failures Pedals slip within the hub limiting acceleration Metal components added significant weight Test section not suitable for analysis

QUESTIONS?