LUNAR WHEEL TEAM TEAM: ADAM ANDERSON DAN BARRET RICHARD FREDRICKSON KRISTINA LYNN RAMOS ERIC SOLIS. ADVISORS: Dr. COLIN BRITCHER Dr.

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Transcription:

LUNAR WHEEL TEAM TEAM: ADAM ANDERSON DAN BARRET RICHARD FREDRICKSON KRISTINA LYNN RAMOS ERIC SOLIS ADVISORS: Dr. COLIN BRITCHER Dr. SEBASTIAN BAWAB

OBJECTIVE design a wheel that would be resistant to the harsh terrain and environment of the lunar surface. The Wheel must be able to hold an applied load of 5,000 pounds anticipated rules for the new competition are different from those of the previous one

OVERVIEW PROGRESS SO FAR DESIGN MATERIAL SELECTION CHARACTERISTICS & COSTS WHEEL BREAKDOWN OF IDEAS TREADS DIAMOND TREADS VERTICAL CHEVRONS HORIZONTAL CHEVRONS

INTRODUCTION Space is one of the only remaining frontiers It holds countless new discoveries Our closest celestial neighbors are the Moon, Mars, and Venus. The Moon http://www.space.com/55-earthsmoon-formation-composition-andorbit.html Mars http://teacher.scholastic.com/scholastic news/indepth/space/mars/index.asp?ar ticle=lifeonmars Venus http://www.earthtimes.org/scite ch/venus-ozone-layer/1486/

FACTS ABOUT THE MOON 384,000 km away from Earth No protective atmosphere Radiation Meteors Lunar Day: between 27.3 to 29.5 days Large temperature swings from 253 F to -387 F The coldest recorded temperature in our solar system was taken on the moon which was 4K Complete Vacuum View of earth from the moon http://www.planetsforkids.org/m oon-moon.html

FACTS ABOUT THE MOON CONT. Composed of igneous rocks Basalt Anorthosite. Covered by regolith extreme terrain variance Craters of varied grades and depths Anorthosite rock http://oedg.niu.edu/summer09/and erson/anorthosite.html Basalt rock http://en.wikipedia.or g/wiki/basalt Lunar Regolith http://www.psrd.hawaii.edu/jul y04/newmineral.html Lunar craters http://www.pbs.org/newshour/extra/features/science /jan-june09/moon_06-23.html

THE REVOLUTIONARY AEROSPACE SYSTEMS CONCEPTS ACADEMIC LINKAGE (RASC-AL) LUNAR WHEEL DESIGN CHALLENGE Held by NASA at Johnson Space Center Seeks ideas for technology to improve exploration on the moon and Mars Rules not currently released

MATERIAL SELECTION LIGHT WEIGHT INEXPENSIVE DESIGN CALLS FOR ELASTIC DEFORMATION ALUMINUM!!!

RANKED BY CHARACTERISTICS

RANKED BY COST * 24"x12"x1/4" SHEET ** 24"x12"x2" FLAT BAR *** 12"X12"X0.1" SHEET **** PER LB @ 12"X12"X0.09" SHEET + 12"X4"X3/4" FLAT BAR

DESIGN OPTIONS

INNOVATIVE BICYCLE WHEEL http://www.bikerumor.com/2013/04/14/loopwheels-curl-carbon-fiber-loops-into-suspensioninside-the-wheels/

CONSIDERATIONS PROS CONS Unique elliptical pattern Utilized series of ellipses to allow for equal deflection around circumference of wheel Offset connection Frequency of ellipses not suitable for rumored load of 5000 lbs Overly simplistic for competitive purposes

WIRED PATTERN http://www.googlelunarxprize.org/teams /frednet/blog/scaled-wrv1-wheeldesign-for-the-jaluro-lunar-rover http://lh3.ggpht.com/- tnjxyjkuu0w/tvtb284poqi/aaaaaaaaaaa/ilij_ky0ubc/ s400/wrv1_wheel_evolution-1.jpg

CONSIDERATIONS PROS Aesthetically unique for competitive purposes Outer hinged plates allow for single point deflection Isolated failure Wire design promotes deflection even deflection around circumference CONS Individual components subjected to large stress values Unlikely for thin, flexible wire with circular cross section to support rumored load of 5000 lbs Large multitude of independent components presents higher risk of failure

MICHELIN TWEEL http://www.frc.ri.cmu.edu/project/lri/scarab/fieldn otes_mk.html

CONSIDERATIONS PROS Introduced an alternative spring design Inspired use of leaf springs and increased frequency of springs CONS Relatively new technology Extremely complex design Expensive and unknown material

DOWN SELECT

PRELIMINARY DESIGN

WEIGHING THE OPTION CHARACTERISTICS Large inner hub Large quantity of holes to decrease waste material and cost Series of ellipses on outer layer to allow for deflection Flat sheet of aluminum on outermost layer for stability WEAKNESSES TO MODIFY Immense size of hub Absence of bolt pattern Single layer of springs to support deflection

SECOND DESIGN

WEIGHING THE OPTION CHARACTERISTICS WEAKNESSES TO MODIFY Smaller hub with realistic design and bolt pattern Second deflective layer added utilizing leaf springs A) Diamond-shaped treads placed on outermost layer of aluminum B) Chevron based tread pattern Tread designs and patterns allows vehicle to traverse radially and laterally 10 ellipses and leaf springs total Single row of ellipses and leaf springs could compromise entire structure if single component fails Bolt Pattern may not be correctly designed A) Diamond treads could result in excessive build up of soil Increase number of springs within structure

FINAL DESIGN

CHARACTERISTICS Bolt Pattern based upon actual pictures of LRV Three series of springs for each layer Rows of springs offset to decrease torsional stresses Offset springs also reduces risk of compromising entire structure if single component fails 16 ellipses and leaf springs in each series and 3 within each row

FABRICATION

HUB CNC MACHINING 6 EVENLY SPACED BOLT HOLES CAST ALUMINUM

LEAF SPRINGS 48 leaf springs Allow the outer rim to deform Welded to center hub Bolted to middle rim

ELLIPSE 48 Ellipses Connects outer rim to middle rim Overlapped and bolted to inner rim

TREADS VERTICAL CHEVRONS DIAMOND VERTICAL CHEVRONS

GOALS FINITE ELEMENT METHOD ANALYSIS BUDGET PROPOSAL PROTOTYPE 3D PRINT OF TREADS TO TEST MINIATURE PROTOTYPE A WHOLE WHEEL--TENTATIVE

QUESTIONS, COMMENTS, AND CONCERNS