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MIT 2.810 Fall 2016 Homework 5 Solutions 1 MIT 2.810 Manufacturing Processes and Systems Homework 5 Solutions Sheet Metal Forming Revised October 7, 2015 Problem 1. Springback Rank the metals in Table 2.2 (Kalpakjian, all editions) in terms of springback, listing those with the largest springback first. Answer: Springback is larger for materials with larger values of Y/E. Materials ranked in terms of their springback behavior E [GPa] Y [MPa] Y/E Ti 105 862 8.2 x 10 -3 Mg 43 218 5.1 x 10 -3 Steel 195 965 5.0 x 10 -3 Cu 128 588 4.6 x 10 -3 Al 74 293 4.0 x 10 -3 Ni 197 653 3.3 x 10 -3 Mo 345 1075 3.1 x 10 -3 W 375 620 1.7 x 10 -3 Pb 14 14 1.0 x 10 -3 Note: The values in this Table are averaged and therefore can deviate considerably. Example: Mild steel can have a yield strength of approximately 350 MPa, which leads to a Y/E ratio of 1.53 x 10 -3 , a value even smaller than the one for Tungsten (W).

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Page 1: MIT 2.810 Manufacturing Processes and Systems Homework ...web.mit.edu/.../hw5-sheet-forming-solutions-2016.pdfMIT 2.810 Fall 2016 Homework 5 Solutions 1 MIT 2.810 Manufacturing Processes

MIT2.810Fall2016 Homework5Solutions

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MIT2.810ManufacturingProcessesandSystemsHomework5SolutionsSheetMetalForming

RevisedOctober7,2015

Problem1.SpringbackRankthemetalsinTable2.2(Kalpakjian,alleditions)intermsofspringback,listingthosewiththelargestspringbackfirst.Answer:SpringbackislargerformaterialswithlargervaluesofY/E.

Materialsrankedintermsoftheirspringbackbehavior E[GPa] Y[MPa] Y/ETi 105 862 8.2x10-3Mg 43 218 5.1x10-3Steel 195 965 5.0x10-3Cu 128 588 4.6x10-3Al 74 293 4.0x10-3Ni 197 653 3.3x10-3Mo 345 1075 3.1x10-3W 375 620 1.7x10-3Pb 14 14 1.0x10-3

Note:ThevaluesinthisTableareaveragedandthereforecandeviateconsiderably.Example:Mildsteelcanhaveayieldstrengthofapproximately350MPa,whichleadstoaY/Eratioof1.53x10-3,avalueevensmallerthantheoneforTungsten(W).

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Problem2.ConsiderthemanufactureofthebracketshowninFigure1fromsheetsteel(availablein4in.widestrips) using a manual brake press or presses. Assume UTS = 70,710 psi. We are interested inestimatingtheunitcosttomakethesebrackets.PleaseuseinformationfromBoothroyd’s“DesignforSheetMetalworking”andthefollowingassumptions:

1. Thesheetmaterialcosts$0.25/lb.2. Thecostofapressis:Presscost[$]=2[$/lb]×forcecapacity[lb].3. All operations take the same length of time, with no breakdowns or unusual delays

betweensteps.4. Laborcosts$30/hr.5. Equipmenthasalifeof10years,tools—of1year.

(a) Describe the sequence operations needed to make this bracket, including materials, tools,

machinesandoperators.(b) Estimatethesizeandcostoftheequipmentneededtomakethispart.(c) Estimatethetimerequiredtomakeoneofthese(ignorewaitingtime).(d) Estimate the cost per bracket (materials, labor, and equipment) assuming 106 parts are

produced.Stateanyassumptions,beyondthosegiven,explicitly.(e) Estimatetheminimumbendradiusforthepart.(f) If thepart is formed to90±,makea roughestimateof the resultingangledue to the spring

back.Use1.5x(yourminimumbendradius).Howwouldthischangeifthebracketmaterialwasaluminumortitanium(roughanswerisOK)?Howwouldyoucompensateforspringback(listatleast3ways)?

Figure1:Sheetsteelbracket.

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Answer:

(a) Sequenceofoperations:1. Cuttingandholepunching:

Material:sheetmetalstrip,4”wideMachine:stampingpressTool:compounddieset(withcuttingandpunchingdies)(asinFig16.11,Kalpakjian,7thed)Operator:1

2. Bending:Material:sheetmetalstripforeachbracketMachine:pressbrakeTool:V-dieOperator:1

Note:AnalternativeforStep1canbeaprogressivediewith2stations,punchingandcut-off.Inthiscase,thesheetmetalstripwouldneedtobesuppliedcontinuouslyasacoil.)

(b) Machineforcecapacities:

L=perimeterofcutorbend(varies)T=thickness=0.1inUTS=ultimatetensilestrength=70,710psiW=V-dieopening≈2in

1. Cutting:maximumshearingforce(equation16.1inKalpakjian,7thed.)

𝐹! = 0.7 𝑇𝐿(𝑈𝑇𝑆) = 0.7 0.1 𝑖𝑛 4 𝑖𝑛 70,710 𝑝𝑠𝑖 =

= 19799 𝑙𝑏𝑠 4.448𝑁𝑙𝑏

= 88 𝑘𝑁

2. Holepunching:maximumshearingforce

𝐹!,!!"# = 0.7 𝑇(𝜋𝑑)(𝑈𝑇𝑆) = 0.7 0.1 𝑖𝑛 𝜋 0.25 𝑖𝑛 70,710 𝑝𝑠𝑖 = 3887 𝑙𝑏𝑠 = 17.3 𝑘𝑁 𝐹!,!"!#$ = 17.3 𝑘𝑁 × 4 = 15548 𝑙𝑏𝑠 = 69 𝑘𝑁

3. Bending:maximumbendingforce(equation16.8inKalpakjian,7thed.)

𝐹! =𝑈𝑇𝑆 𝐿𝑇!

𝑊=

70,710 𝑝𝑠𝑖 (1 𝑖𝑛) (0.1 𝑖𝑛)!

(2 𝑖𝑛)= 354 𝑙𝑏𝑠 = 1573 𝑁

Presscosts:1. Stampingpress:

𝐶!"#"$%& ≈$2𝑙𝑏

𝑙𝑏𝑠 𝑓𝑜𝑟𝑐𝑒 𝑐𝑎𝑝𝑎𝑐𝑖𝑡𝑦 = $2 19799 + 15548 lbs ≈ $70,700

2. Pressbrake:𝐶!"#$%& ≈ $2 354 lbs ≈ $708

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Diecosts:1. Cuttingand4-holepunchdieset:

Usablearea:𝐴! = 4 𝑖𝑛 2.5 !"!"

1 𝑖𝑛 2.5 !"!"

= 25 𝑐𝑚!

Diesetmaterialcost:𝐶!" = $120 + 0.36𝐴! ≈ $130 Timefordiemaking:Basetime:𝑀!" = 23 + 0.03𝑏𝑤 = 23 + 0.03 4 𝑖𝑛 2.5 !"

!"1 𝑖𝑛 2.5 !"

!"≈ 24 ℎ𝑟

Standardpunchshapetime:𝑀!" = 𝐾𝑁! + 0.4𝑁! = 2 4 + 0.4(1) = 8.4 ℎ𝑟 Totalcostforblankingandpunchingdieset:𝐶!"#$ = $130 + 24 + 8.4 ℎ𝑟 $"#

!!= $1102

2. BendingV-die:

Diesetmaterialcost:𝐶!" = $120 + 0.36𝐴! ≈ $130(asabove)Timefordiemaking:Basetime:𝑀!" = 18 + 0.023𝑏𝑤 0.9 + 0.02𝐷 =

= 18 + 0.023 4 𝑖𝑛 2.5𝑐𝑚𝑖𝑛

1 𝑖𝑛 2.5𝑐𝑚𝑖𝑛

0.9 + 0.02 2 𝑖𝑛 2.5𝑐𝑚𝑖𝑛

≈ 19 ℎ𝑟

Bendlengthtime:𝑀!" = 0.68𝐿! + 5.8 𝑁! = 0.68 1 𝑖𝑛 2.5 !"!"

+ 5.8(1) = 7.5 ℎ𝑟TotalcostforV-die:𝐶!"#$ = $130 + 19 + 7.5 ℎ𝑟 $"#

!!= $925

(c) Timeestimateperpart:

UsingthecycletimefromBoothroyd(equation9.22),t=3.8+0.11(L+W)secondsforloadingandremovingapartmanuallyfromabrakepress.Thetimeforthestampingpressstepwillbelesssinceithasautomatedpartejection.Assuming2operatorsareoperatingthe2machinessimultaneously,thetimeforonepartwillbelimitedbythelongersteptime(bending):𝑡 = 3.8 + 0.11 𝐿 +𝑊 = 3.8 + 0.11 4 + 1 𝑖𝑛 = 4.35 𝑠 = 1.21×10!!ℎ𝑟perpart

(d) Costperbracket:

Materialcosts:𝐶!"#$ = $0.25/𝑙𝑏 0.15 𝑙𝑏𝑠 = $0.038/𝑝𝑎𝑟𝑡Laborcosts:𝐶!"#$% = $30/ℎ𝑟

𝐶!"#$ =𝐶!"#$%𝑁

+ 𝐶!"# =𝐶!"#"$%& + 𝐶!"#$%& + 𝐶!"#$ + 𝐶!"#$

𝑁+ (𝐶!"#$% + 𝐶!"#$) =

=$70,700 + $708 + $1,102 + $925

𝑁+

$30ℎ𝑟

1.21×10!! ℎ𝑟 + $0.038 =

=$73,435

𝑁+ $0.074

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If10!partsareproduced,thecostperbracketis:

𝐶!"#$ =$73,43510!

+ $0.074 ≈ $0.15

(e) Theminimumbendradiusistheradiusatwhichacrackfirstappearsattheouterfibersofasheetbeingbent(Sec.16.5,Kalpakjian,7thed).Engineeringstrainduringbending:

𝑒 =1

2𝑅𝑇 + 1

=𝑇

2𝑅 + 𝑇

2𝑅 =𝑇𝑒− 𝑇

𝑅!"# = 0.5𝑇

𝑒!"#− 𝑇

Here,T=0.1inandemax=maximumstrainatfracture=ductilityofthematerial=!!!!!!!

=

0.22forlow-carbonsteel(Boothroyd,p.403).Thus,𝑅!"# = 0.5 !.! !"

!.!!− 0.1 𝑖𝑛 = 0.18in.

(f) Fromslide64ofthesheetmetalforminglecture,theequationforspringbackradiusis:1𝑅!−1𝑅!

= 3𝑌𝐸𝑇

− 4𝑅!!𝑌𝐸𝑇

!

whereRi=1.5(0.18in)=0.27in,T=0.1inFromthediagramonthesameslide,Y/Esteel=1/909Y/EAl=1/212Y/ETi=1/188

Thenthefinalradiiwouldbe: !!!= − !

!!− 3 !

!"+ 4𝑅!!

!!"

!

Steel:𝑅! =!

0.27 − 3!

!".!+ 4 0.27 ! !

!".!

! !!= 0.2724in

Aluminum:𝑅! =!

0.27 − 3!

!".!+ 4 0.27 ! !

!".!

! !!= 0.2807in

Titanium:𝑅! =!

0.27 − 3!

!".!+ 4 0.27 ! !

!".!

! !!= 0.2822in

Estimatethefinalangleafterspringback,assumingitisinitiallybentto𝛼! = 90°:Iftheradiiaremeasuredtothecenterlineofthemetalsheet,thenthelengthofthecenterlinearcis𝑙 = 𝑅!𝛼! = 𝑅!𝛼!(Figure2).

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Figure2.Diagramofspringbackangles.

Steel:𝛼! =!!!!𝛼! =

!.!"!.!"!#

90° = 89.2°,𝜃! = 180° − 𝛼! = 90.8°

Aluminum:𝛼! =!.!"!.!"#$

90° = 86.6°,𝜃! = 180° − 𝛼! = 93.4°

Titanium:𝛼! =!.!"!.!"!!

90° = 86.1°,𝜃! = 180° − 𝛼! = 93.9°SpringbackislargestforTitanium.

Compensationmethods:1. Over-bending2. Bottoming3. Stretchbending