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Over-design or poor design (more protection than is required or materials being incorrectly used ) results in excessive material cost. The procedure can be broken down into seven basic steps. @>: Introduction(1Determine Product Fragility Determine the amount of mechanical shock the product can survive on its own by evaluating  fragility or  g-factor  . 2. Determine Conditions Consider the handling and transportation environment the product will face and establish the amount of shock the product may encounter ( drop height ). 3. Calculate Cushion Requirements Use dynamic cushioning curves to determine thickness, static loading and bearing area. ZZz$Z$ Introduction(4. Recognizing Design Constraints Check for important problems including compressive creep, cushion buckling and extreme temperature effects. 5. Design Prototypes and Test Build a prototype and determine its actual performance. 6. Consider Vibration Effects Determine the natural frequency of any component which is prone to vibration damage, and compare it against the vibration characteristics of your package design. rZZ#o ;  Introduction(7. Monitor Performance Monitor the performance of your design to determine when internal changes in the design might alter the requirements for package performance. B % Step 1 Determine Product Fragility"&$%" Fragility is normally expressed in units of  g s and indicates the maximum deceleration the product can withstand without being damaged. The more fragile a product is, the lower its g-factorTable 15.1 . (4  % Step 1 Determine Product Fragility&&"Table 15.1 Approximate fragility of typical packaged Articles Extremely Fragile Aircraft altimeters, gyroscopes, items with delicate mechanical alignments Very Delicate Medical diagnostic apparatus, X-ray equipment Delicate Display terminals, printers, test instruments, hard disk drives Moderately Delicate Stereos and television receivers, floppy disk drives Moderately Rugged Major appliances, furniture Rugged Table saws, sewing machines, machine toolsP>  } g % Step 1 Determine Product Fragility&&"RThe highest deceleration, which did not cause damage, is then known to be the product s g-factor. It may be necessary to determine fragility levels for a product in various orientations. If the g-factor is estimated too high, and the product is unable to survive as much shock as anticipated, the packaging will be underdesigned and significant shipping damage is likely to occur. If the g-factor is estimated too low, and the product can actually withstand more shock than anticipated, the packaging will be overdesigned and unnecessarily expensive. *Z*,<     Step 2 Determine Conditions( Drop heights are generally established by the product's weight, which usually reflect how the product will be handled(Table 15.2). $$n     Step 2 Determine Conditions( Table 15.2 Typical drop heights Weight Range Type of Handling Drop Height Gross Weight in lbs. in inches 0-10 1 person throwing 42 10-20 1 person carrying 36 20-50 1 person carrying 30 50-100 2 person carrying 24 100-250 Light equipment 18 250+ Heavy equipment handling 12+ Note: Palletized products may receive drops of up to six inches.pP6; ' Step 3 Calculate Cushion Requirements"( 'To determine the amount of functional cushioning material which will provide adequate protection for the packaged item. By functional cushioning material, we mean that portion of the design which directly supports the load and functions to absorb shock during impacts. ' Step 3 Calculate Cushion Requirements(( ' Step 3 Calculate Cushion Requirements((' Step 3 Calculate Cushion Requirements((' Step 3 Calculate Cushion Requirements((GUsing Dynamic Cushioning Curves (Figure 15.1) An Overview Curves are generated by dropping a series of known weights onto a cushion sample from a specified height and measuring the amount of shock experienced by the weights as they impact the foam. In simple terms, this testing represents a product dropping on a cushion from a height likely to be encountered during shipment. The horizontal axis represents a range of static loadings that packaged items might apply to the cushioning material. The vertical axis represents the shock experienced as the cushion is impacted. F;P P   ' Step 3 Calculate Cushion Requirements((Curves are often presented for both first impact and multiple impact (average of drops 2-5) data. An Example [Given] An object to be packaged is a 10-inch cube weighing 60 pounds with a fragility of 50 g's. [Solution] 1. Since a product typically faces repeated impacts during shipment, you will probably wish to use multiple-impact data. 2.The typical drop height for a product of this weight may be estimated from the chart below as 24 inches. TcP PoPPb f' Step 3 Calculate Cushion Requirements(( 3. Obtain the cushioning curves for the cushioning material you wish to use. Locate curves that represent multiple impact data from a drop height of 24 inches. 4. Determining Thickness locate our product's fragility level (50 g's) on the vertical axis of the figure, and draw an imaginary horizontal line across the chart at this level. This separates the chart into two sections: our fragility line and lower, where the packaged item will be able to survive the anticipated shock level, and the section above our line where the shock levels are high enough to damage the product PZZ' Step 3 Calculate Cushion Requirements((Uchoose a thickness of 2 inches for the thinnest cushion thickness. 5. Determining Static Loading and Bearing Area The useable part of the curve is bounded by a static loading of 0.3 psi at the low end, and 1.4 psi at the high end. This tells us that, with a 2-inch cushion, we can apply a static loading anywhere within this "cushioning range" and still protect to 50 g's or lower. The highest static loading value within the cushioning range will result in the most economical design because it will use less cushioning material to provide adequate protection, thus lowering design costs. FDZ4ZZv,{' Step 3 Calculate Cushion Requirements((The cushion bearing area is easily calculated as the product weight divided by our chosen static loading. a) 60 / 0.3 = 200 square inches of foam b) 60 /1.4 = 43 square inches of foam (This is a 78.5% reduction in cushioning material) Designing to the minimum thickness is the general practice. By repeating this procedure with several materials, you can quickly generate comparisons, which will allow you to strike an economical balance between material cost and package size. 0kZZZ( Step 4 Recognizing Design Constraints")&'Y1. Consider Compressive Creep Compressive creep is the gradual loss of thickness a material may experience if placed under a constant load for an extended period of time. Significant compressive creep will result in the packaged product loosening in the cushion and becoming vulnerable to excessive movement inside the package during shipment.:;9' Step 4 Recognizing Design Constraints((As a general rule, creep of 10% is recognized as a practical upper limit. In some cases creep losses of over 10% in thickness have been shown to result in a significant loss of cushion performance. Should it be found that creep in excess of 10% is anticipated, designers should recalculate the functional foam requirement using a lower static-loading figure. Spreading the loading over a larger area will reduce compressive creep. Z' Step 4 Recognizing Design Constraints((Buckling is the non-uniform compression of a cushion. When buckling occurs, the energy of the impact is not transferred evenly throughout the cushion and more shock is transferred to the package contents. Buckling usually occurs when the cushions become too tall and thin. Figure 15.2 provides width-to-thickness coefficients for different static loading values and enable the designer to check for buckling potential. Z' Step 4 Recognizing Design Constraints((' Step 4 Recognizing Design Constraints((' Step 4 Recognizing Design Constraints((' Step 4 Recognizing Design Constraints((Example: Let's assume you plan to use a 3-inch thick pad of ETHAFOAM 220 to cushion a side of your product, which presents a static load of 1.0 psi. In this case, the coefficient is 0.7. Using the formula T x W/T = W, you can now find the minimum width: 3"x 0.7 = 2.1". Your cushion must be at least 2.1 inches wide or long to resist buckling. 3. Consider Extreme Temperature Effects 4Z)Y(' Step 4 Recognizing Design Constraints((RAs with all thermoplastic foams, when they are exposed to extremely high or low temperatures over a considerable length of time, they may be affected. The materials become stiffer at low temperatures and increasingly softer at higher temperatures. In extreme cases, it may become necessary to compensate for these effects in your design.SZS# Step 5 Design Prototypes and Test"$$##Each packaging design must be developed separately, given the large number of variables involved. It is highly recommended that you build and test a prototype of your cushion design to determine its actual performance.  # Step 6 Consider Vibration Effects"$&#$Table 15.3 Typical forcing frequencies of carriers Carrier Frequency Range Conditions Railroad 2 - 7 Hz (suspension) Moving freight car 50 - 70 Hz (structural) Truck 2 - 7 Hz (suspension) Normal highway travel 15 - 20 Hz (tires) 50 - 70 Hz (structural) Aircraft 2 - 10 Hz (propeller) On aircraft floor during flight 100  200 Hz (jet) Ships 11 Hz (on deck) Vibrations caused by 100 Hz (bulkheads) interference to the flow of water by the ship, and from imbalance and misalignment of the propeller shaft system.3PP27 h s!# Step 6 Consider Vibration Effects$$$jEvery mode of transport subjects the packages being shipped to some amount of vibration at various frequencies. In order to provide products which are prone to vibration damage with protection against such effects, it is essential to determine the natural frequency of any component which is prone to vibration damage, and compare it against the vibration characteristics of your package design. Every cushioning system has a range of vibrational frequencies in which it amplifies vibration and passes on a more severe vibration to the packaged product than it receives from the transport environment (Figure 15.3). kPk "# Step 6 Consider Vibration Effects$$$]For most vibration-sensitive products, making sure that the package design does not amplify vibration in the product's natural frequency and is enough to prevent vibrational damage from occurring during shipment. For severely vibration-sensitive products, it may be necessary for the package design to actually attenuate the frequencies of concern.^\ # # Step 6 Consider Vibration Effects$$$$!# Step 6 Consider Vibration Effects$$$%"# Step 6 Consider Vibration Effects$$$FMaterial response is often given in diagrams similar to Figure 15.4, which represent performance for a given thickness of material. Note that for any frequency, one can estimate whether the package will perform in direct coupling, amplification, or attenuation mode as a function of the static loading applied to the cushion. GZG&#F Step 7 Monitor Performance If it works, question itGGThere are many assumptions that went into your design development. It is a good practice to monitor the performance of your design in actual use. This will help you to determine if your design is providing more real-world performance than is actually required, or not enough. Monitoring of packaging performance on an ongoing basis can also help determine if further economies can be achieved without sacrificing protection. }  ` fffff` ?̙ffE` ff333` C3ff3` &u3` ffff` **@fff̙fl` +3[Xd` 333f` 5D`|f>?" dd@*?lPd@ `F `A@`<``( n?" dd@   @@``PP   @ ` `.p>>  @6(  @6T ``` @ "```" @ BCG p"P`` F 0C B @ C FBCE6FGIQSTUV.WX@` B C "`` D0C hB @ s *DԔ" @ 0XI "{4  LUSQdkYkHrh7h_    @ 08L "  8USQdkYkHre,g7h_ ,{N~ ,{ N~ ,{V~ ,{N~   @ 6Q #" `` `  X*   @ 6U #" ``   Z*   @ 6Z #" `` `  \* H @ 0޽h ? fffff___PPT10i. +D=' = @B +  Radial    t l  D (  D:T H X  D "H X " D <`p"X  F 0C  D Bh>"H0 F 0C B D C BCE6FGIQSTUV.WX@` B C "h  D0C B D s *Dp"p,$ 0 D 0 "py  LUSQdkYkHrh7h_   D 0 "x   NUSQdkYkHroRh7h_   D 6t #" `` `  X*   D 6 #" `c   Z*   D 6؛ #" `` `  \* H D 0޽h ? fffff80___PPT10. 0   0(  x  c $4Dpy  x  c $Dp   H  0޽h ? 3380___PPT10.Vd`;$   0L$(  Lr L S @{4   r L S @  H L 0޽h ? fffff80___PPT10.Wdu4$   @P$(  Pr P S 0@{4   r P S @1@  H P 0޽h ? fffff80___PPT10.Wdq$   PT$(  Tr T S (6@{4   r T S 6@  H T 0޽h ? fffff80___PPT10.Wd0$   `X$(  Xr X S `E@{4   r X S 4F@  H X 0޽h ? fffff80___PPT10.Wd`ak$   p\$(  \r \ S X@{4   r \ S 7@  H \ 0޽h ? fffff80___PPT10.Wd    F> `(  `r ` S  h@{4   r ` S y@%   ` Bd  15-25 g's  ` Bt\C  25-40 g's  ` BWk  < 40-60 g's  ` BF x-   85-115 g's ` Bb p   60-85 g's  ` Bg F  #115 g's and up H ` 0޽h ? fffff80___PPT10.Xd$   d$(  dr d S H@{4   r d S @  H d 0޽h ? fffff80___PPT10.YdЯy$   l$(  lr l S 4Y@{4  Y r l S Y@&Y Y H l 0޽h ? fffff80___PPT10.Yd0$   p$(  pr p S 0Y@{4  Y r p S ОY@ Y H p 0޽h ? fffff80___PPT10.Ydǯ$   t$(  tr t S  @{4   r t S ̚ @   H t 0޽h ? fffff80___PPT10.Zd%   91x(  xr x S q @{4  q  ( x AX  @.http://www.dow.com/perffoam/images/fig1.gifcushioning curve graph"`  q  x < {ADetermining Cushion Thickness 24" drop height, 2-5 drop average B?H x 0޽h ? fffff80___PPT10.Zd`   WO(  r  S @{4   *  AX  @0http://www.dow.com/perffoam/images/fig2.gifcushion thickness graph"`z    << ' C Determining Static Loading Range 24" drop height, 2-5 drop averageDCCH  0޽h ? fffff80___PPT10.Zd   C; (  r  S L}@{4   0  AX  @6http://www.dow.com/perffoam/images/fig3.gifstatic loading range graph"`{    B t w-Figure 15.1 Typical dynamic cushioning curve ..  H  0޽h ? fffff80___PPT10.Zd$   @$(  r  S |۝@{4   r  S  ܝ@  H  0޽h ? fffff80___PPT10.Zd$   P$(  r  S @{4   r  S @  H  0޽h ? fffff80___PPT10.Zd$   `$(  r  S ם@{4   r  S ԝ@  H  0޽h ? fffff80___PPT10.[dl$   p$(  r  S @{4   r  S D@  H  0޽h ? fffff80___PPT10.[dp`*8$   $(  r  S @{4   r  S @  H  0޽h ? fffff80___PPT10.[dL$   $(  r  S  x@{4  x r  S  x@ x H  0޽h ? fffff80___PPT10.[d0y[$   $(  r  S x@{4  x r  S x@ x H  0޽h ? fffff80___PPT10.[dn   `X(  r  S (x@{4  x r  S )x@ x   6*x tVj  ^.Figure 15.2 Buckling coefficients for ETHAFOAM//H  0޽h ? fffff80___PPT10.[dPN   aY (  r  S @{4   T  AX  @Zhttp://www.dow.com/perffoam/images/fig5.gifbuckling coefficients for ETHAFOAM 220 graph"` \    BܿZ z qABuckling Coefficients for ETHAFOAM 220 at Various Static LoadingsBBH  0޽h ? fffff80___PPT10.[d`    |t (  r  S Ox@{4  x Z  AX  @`http://www.dow.com/perffoam/images/fig5.gifbuckling coefficients for ETHAFOAM select graph"`  x  B\9   DBuckling Coefficients for ETHAFOAM Select at Various Static Loadings&E+H  0޽h ? fffff80___PPT10.\d    me(  r  S `Ax@{4  x V  AX  @\http://www.dow.com/perffoam/images/fig6.gifbuckling coefficients for ETHAFOAM nova graph"`   x  BtMx 8 {CBuckling Coefficients for ETHAFOAM Nova at Various Static Loadings DBH  0޽h ? fffff80___PPT10.\d78$    $(  r  S \x@{4  x r  S \x@ x H  0޽h ? fffff80___PPT10.\d0G$   0$(  r  S ix@{4  x r  S tjx@ x H  0޽h ? fffff80___PPT10.]dx$   @$(  r  S yx@{4  x r  S zx@ x H  0޽h ? fffff80___PPT10.]d>2$   P$(  r  S x@{4  x r  S tx@ x H  0޽h ? fffff80___PPT10.]dJ$   `$(  r  S x@{4  x r  S șx@ x H  0޽h ? fffff80___PPT10.^d_$   p$(  r  S pGx@{4  x r  S  x@ x H  0޽h ? fffff80___PPT10.^dP{    zr (  r  S hx@{4  x N  AX  @Thttp://www.dow.com/perffoam/images/fig7.giftypical vibrational response of a package"`F  x  B  6Figure 15.3 Typical vibrational response of a package 75 H  0޽h ? fffff80___PPT10.^dE%   %(  r  S DPx@{4  x R  AX  @Xhttp://www.dow.com/perffoam/images/fig8.gifvibration response of a cushioning material"`z  x  B@- ; Figure 15.4 Vibrational response of a cushioning material $<9$ $H  0޽h ? fffff80___PPT10.^d@1$   $(  r  S xY@{4  x r  S $Y@ Y H  0޽h ? fffff80___PPT10.^dߒ$   $(  r  S Px@{  x r  S $x@ x H  0޽h ? fffff80___PPT10.^dr`1Zgqs&vRx~z|~ 8d5$+Wۣ3+$8=iEW? &Z( D/ 0|  ĻʾuFACULTY OF DESIGNi#A *ArialTimes New Roman Wingdings Arial BlackRadial Lesson 15 Introduction Introduction Introduction Introduction& Step 1 Determine Product Fragility& Step 1 Determine Product Fragility& Step 1 Determine Product Fragility Step 2 Determine Conditions Step 2 Determine Conditions( Step 3 Calculate Cushion Requirements( Step 3 Calculate Cushion Requirements( Step 3 Calculate Cushion Requirements( Step 3 Calculate Cushion Requirements( Step 3 Calculate Cushion Requirements( Step 3 Calculate Cushion Requirements( Step 3 Calculate Cushion Requirements( Step 3 Calculate Cushion Requirements( Step 3 Calculate Cushion Requirements) Step 4 Recognizing Design Constraints( Step 4 Recognizing Design Constraints( Step 4 Recognizing Design Constraints( Step 4 Recognizing Design Constraints( Step 4 Recognizing Design Constraints( Step 4 Recognizing Design Constraints( Step 4 Recognizing Design Constraints( Step 4 Recognizing Design Constraints$ Step 5 Design Prototypes and Test$ Step 6 Consider Vibration Effects$ Step 6 Consider Vibration Effects$ Step 6 Consider Vibration Effects$ Step 6 Consider Vibration Effects$ Step 6 Consider Vibration Effects$ Step 6 Consider Vibration EffectsG Step 7 Monitor Performance If it works, question it  õʾĸģ õƬ_xTOADTOAD# 8@ _PID_HLINKSA+../jiaoxueluxiang/flash/15-1 five step.exe[ 00"D[SOalBlact+8 08z[ 00 DTimes New Roman8 08z[ 000DWingdingsRoman8 08z[ 00@DArial Blackman8 08z[ 00"PDўSOal Blackman8 08z[ 00@ .  @n?" dd@  @@`` >%       "$%&'()*+,.02345678:<=4b$^Qb#"t?~1b$M (}|%3,R1b$P?hjxd\l.3bEb$ 2v!Sqs]}E4b$ü:4lTGb$S5c+']6'b$#XΝIR 0AA@8  yʚ;ʚ;g4KdKdPz[ 0ppp@ <4dddd| 0L+ ~0___PPT10 pp>___PPT9 T Lesson 15 zSeven Steps for Cushioned Package Development ,{15 QSňNekl .>.$(,.  Introduction(1Packaging can be unnecessarily expensive in a couple of ways: 1. Inadequate design results in shipment damage 2. Over-design or poor design (more protection than is required or materials being incorrectly used ) results in excessive material cost. The procedure can be broken down into seven basic steps. @>: Introduction(1Determine Product Fragility Determine the amount of mechanical shock the product can survive on its own by evaluating  fragility or  g-factor  . 2. Determine Conditions Consider the handling and transportation environment the product will face and establish the amount of shock the product may encounter ( drop height ). 3. Calculate Cushion Requirements Use dynamic cushioning curves to determine thickness, static loading and bearing area. ZZz$Z$ Introduction(4. Recognizing Design Constraints Check for important problems including compressive creep, cushion buckling and extreme temperature effects. 5. Design Prototypes and Test Build a prototype and determine its actual performance. 6. Consider Vibration Effects Determine the natural frequency of any component which is prone to vibration damage, and compare it against the vibration characteristics of your package design. rZZ#o ;  Introduction(7. Monitor Performance Monitor the performance of your design to determine when internal changes in the design might alter the requirements for package performance. ( Another way for cushion design: Five steps for package cushion design ) R;u F" U 0 % Step 1 Determine Product Fragility"&$%" Fragility is normally expressed in units of  g s and indicates the maximum deceleration the product can withstand without being damaged. The more fragile a product is, the lower its g-factorTable 15.1 . (4  % Step 1 Determine Product Fragility&&"Table 15.1 Approximate fragility of typical packaged Articles Extremely Fragile Aircraft altimeters, gyroscopes, items with delicate mechanical alignments Very Delicate Medical diagnostic apparatus, X-ray equipment Delicate Display terminals, printers, test instruments, hard disk drives Moderately Delicate Stereos and television receivers, floppy disk drives Moderately Rugged Major appliances, furniture Rugged Table saws, sewing machines, machine toolsP>  } g % Step 1 Determine Product Fragility&&"RThe highest deceleration, which did not cause damage, is then known to be the product s g-factor. It may be necessary to determine fragility levels for a product in various orientations. If the g-factor is estimated too high, and the product is unable to survive as much shock as anticipated, the packaging will be underdesigned and significant shipping damage is likely to occur. If the g-factor is estimated too low, and the product can actually withstand more shock than anticipated, the packaging will be overdesigned and unnecessarily expensive. *Z*,<     Step 2 Determine Conditions( Drop heights are generally established by the product's weight, which usually reflect how the product will be handled(Table 15.2). $$n     Step 2 Determine Conditions( Table 15.2 Typical drop heights Weight Range Type of Handling Drop Height Gross Weight in lbs. in inches 0-10 1 person throwing 42 10-20 1 person carrying 36 20-50 1 person carrying 30 50-100 2 person carrying 24 100-250 Light equipment 18 250+ Heavy equipment handling 12+ Note: Palletized products may receive drops of up to six inches.pP6; ' Step 3 Calculate Cushion Requirements"(  !"#$%&'()*+,-./0123456789:;<=>?@ABCDEFGHIJKLMNOPQRSTUVWXYZ[\]^_`abcdefghijklmnopqrstuvwxyz{|}~      >"#$&'()*+,-./012345678s=?@ABCDEFGHIJKLMNOPQRSTUVWXYZ[\]^_`abcdefghijkl%opqr!tuvwxyz{|}~Root EntrydO)`|4_nPictures/oCurrent UserC,SummaryInformation($ PowerPoint Document(DocumentSummaryInformation8%dDArialBlact+8 08z[ 00"D[SOalBlact+8 08z[ 00 DTimes New Roman8 08z[ 000DWingdingsRoman8 08z[ 00@DArial Blackman8 08z[ 00"@ .  @n?" dd@  @@`` >%       "$%&'()*+,.02345678:<=4b$^Qb#"t?~1b$M (}|%3,R1b$P?hjxd\l.3bEb$ 2v!Sqs]}E4b$ü:4lTGb$S5c+']6'b$#XΝIR 0AA@8  3ʚ;ʚ;g4KdKdPz[ 0ppp@ <4dddd| 0L+ 80___PPT10 ppS Lesson 15 zSeven Steps for Cushioned Package Development ,{15 QSňNekl .>.$(,.  Introduction(1Packaging can be unnecessarily expensive in a couple of ways: 1. Inadequate design results in shipment damage 2. Over-design or poor design (more protection than is required or materials being incorrectly used ) results in excessive material cost. The procedure can be broken down into seven basic steps. @>: Introduction(1Determine Product Fragility Determine the amount of mechanical shock the product can survive on its own by evaluating  fragility or  g-factor  . 2. Determine Conditions Consider the handling and transportation environment the product will face and establish the amount of shock the product may encounter ( drop height ). 3. Calculate Cushion Requirements Use dynamic cushioning curves to determine thickness, static loading and bearing area. ZZz$Z$ Introduction(4. Recognizing Design Constraints Check for important problems including compressive creep, cushion buckling and extreme temperature effects. 5. Design Prototypes and Test Build a prototype and determine its actual performance. 6. Consider Vibration Effects Determine the natural frequency of any component which is prone to vibration damage, and compare it against the vibration characteristics of your package design. rZZ#o ;  Introduction(7. Monitor Performance Monitor the performance of your design to determine when internal changes in the design might alter the requirements for package performance. B % Step 1 Determine Product Fragility"&$%" Fragility is normally expressed in units of  g s and indicates the maximum deceleration the product can withstand without being damaged. The more fragile a product is, the lower its g-factorTable 15.1 . (4  % Step 1 Determine Product Fragility&&"Table 15.1 Approximate fragility of typical packaged Articles Extremely Fragile Aircraft altimeters, gyroscopes, items with delicate mechanical alignments Very Delicate Medical diagnostic apparatus, X-ray equipment Delicate Display terminals, printers, test instruments, hard disk drives Moderately Delicate Stereos and television receivers, floppy disk drives Moderately Rugged Major appliances, furniture Rugged Table saws, sewing machines, machine toolsP>  } g % Step 1 Determine Product Fragility&&"RThe highest deceleration, which did not cause damage, is then known to be the product s g-factor. It may be necessary to determine fragility levels for a product in various orientations. If the g-factor is estimated too high, and the product is unable to survive as much shock as anticipated, the packaging will be underdesigned and significant shipping damage is likely to occur. If the g-factor is estimated too low, and the product can actually withstand more shock than anticipated, the packaging will be overdesigned and unnecessarily expensive. *Z*,<     Step 2 Determine Conditions( Drop heights are generally established by the product's weight, which usually reflect how the product will be handled(Table 15.2). $$n     Step 2 Determine Conditions( Table 15.2 Typical drop heights Weight Range Type of Handling Drop Height Gross Weight in lbs. in inches 0-10 1 person throwing 42 10-20 1 person carrying 36 20-50 1 person carrying 30 50-100 2 person carrying 24 100-250 Light equipment 18 250+ Heavy equipment handling 12+ Note: Palletized products may receive drops of up to six inches.pP6; ' Step 3 Calculate Cushion Requirements"( 'To determine the amount of functional cushioning material which will provide adequate protection for the packaged item. By functional cushioning material, we mean that portion of the design which directly supports the load and functions to absorb shock during impacts. ' Step 3 Calculate Cushion Requirements(( ' Step 3 Calculate Cushion Requirements((' Step 3 Calculate Cushion Requirements((' Step 3 Calculate Cushion Requirements((GUsing Dynamic Cushioning Curves (Figure 15.1) An Overview Curves are generated by dropping a series of known weights onto a cushion sample from a specified height and measuring the amount of shock experienced by the weights as they impact the foam. In simple terms, this testing represents a product dropping on a cushion from a height likely to be encountered during shipment. The horizontal axis represents a range of static loadings that packaged items might apply to the cushioning material. The vertical axis represents the shock experienced as the cushion is impacted. F;P P   ' Step 3 Calculate Cushion Requirements((Curves are often presented for both first impact and multiple impact (average of drops 2-5) data. An Example [Given] An object to be packaged is a 10-inch cube weighing 60 pounds with a fragility of 50 g's. [Solution] 1. Since a product typically faces repeated impacts during shipment, you will probably wish to use multiple-impact data. 2.The typical drop height for a product of this weight may be estimated from the chart below as 24 inches. TcP PoPPb f' Step 3 Calculate Cushion Requirements(( 3. Obtain the cushioning curves for the cushioning material you wish to use. Locate curves that represent multiple impact data from a drop height of 24 inches. 4. Determining Thickness locate our product's fragility level (50 g's) on the vertical axis of the figure, and draw an imaginary horizontal line across the chart at this level. This separates the chart into two sections: our fragility line and lower, where the packaged item will be able to survive the anticipated shock level, and the section above our line where the shock levels are high enough to damage the product PZZ' Step 3 Calculate Cushion Requirements((Uchoose a thickness of 2 inches for the thinnest cushion thickness. 5. Determining Static Loading and Bearing Area The useable part of the curve is bounded by a static loading of 0.3 psi at the low end, and 1.4 psi at the high end. This tells us that, with a 2-inch cushion, we can apply a static loading anywhere within this "cushioning range" and still protect to 50 g's or lower. The highest static loading value within the cushioning range will result in the most economical design because it will use less cushioning material to provide adequate protection, thus lowering design costs. FDZ4ZZv,{' Step 3 Calculate Cushion Requirements((The cushion bearing area is easily calculated as the product weight divided by our chosen static loading. a) 60 / 0.3 = 200 square inches of foam b) 60 /1.4 = 43 square inches of foam (This is a 78.5% reduction in cushioning material) Designing to the minimum thickness is the general practice. By repeating this procedure with several materials, you can quickly generate comparisons, which will allow you to strike an economical balance between material cost and package size. 0kZZZ( Step 4 Recognizing Design Constraints")&'Y1. Consider Compressive Creep Compressive creep is the gradual loss of thickness a material may experience if placed under a constant load for an extended period of time. Significant compressive creep will result in the packaged product loosening in the cushion and becoming vulnerable to excessive movement inside the package during shipment.:;9' Step 4 Recognizing Design Constraints((As a general rule, creep of 10% is recognized as a practical upper limit. In some cases creep losses of over 10% in thickness have been shown to result in a significant loss of cushion performance. Should it be found that creep in excess of 10% is anticipated, designers should recalculate the functional foam requirement using a lower static-loading figure. Spreading the loading over a larger area will reduce compressive creep. Z' Step 4 Recognizing Design Constraints((Buckling is the non-uniform compression of a cushion. When buckling occurs, the energy of the impact is not transferred evenly throughout the cushion and more shock is transferred to the package contents. Buckling usually occurs when the cushions become too tall and thin. Figure 15.2 provides width-to-thickness coefficients for different static loading values and enable the designer to check for buckling potential. Z' Step 4 Recognizing Design Constraints((' Step 4 Recognizing Design Constraints((' Step 4 Recognizing Design Constraints((' Step 4 Recognizing Design Constraints((Example: Let's assume you plan to use a 3-inch thick pad of ETHAFOAM 220 to cushion a side of your product, which presents a static load of 1.0 psi. In this case, the coefficient is 0.7. Using the formula T x W/T = W, you can now find the minimum width: 3"x 0.7 = 2.1". Your cushion must be at least 2.1 inches wide or long to resist buckling. 3. Consider Extreme Temperature Effects 4Z)Y(' Step 4 Recognizing Design Constraints((RAs with all thermoplastic foams, when they are exposed to extremely high or low temperatures over a considerable length of time, they may be affected. The materials become stiffer at low temperatures and increasingly softer at higher temperatures. In extreme cases, it may become necessary to compensate for these effects in your design.SZS# Step 5 Design Prototypes and Test"$$##Each packaging design must be developed separately, given the large number of variables involved. It is highly recommended that you build and test a prototype of your cushion design to determine its actual performance.  # Step 6 Consider Vibration Effects"$&#$Table 15.3 Typical forcing frequencies of carriers Carrier Frequency Range Conditions Railroad 2 - 7 Hz (suspension) Moving freight car 50 - 70 Hz (structural) Truck 2 - 7 Hz (suspension) Normal highway travel 15 - 20 Hz (tires) 50 - 70 Hz (structural) Aircraft 2 - 10 Hz (propeller) On aircraft floor during flight 100  200 Hz (jet) Ships 11 Hz (on deck) Vibrations caused by 100 Hz (bulkheads) interference to the flow of water by the ship, and from imbalance and misalignment of the propeller shaft system.3PP27 h s!# Step 6 Consider Vibration Effects$$$jEvery mode of transport subjects the packages being shipped to some amount of vibration at various frequencies. In order to provide products which are prone to vibration damage with protection against such effects, it is essential to determine the natural frequency of any component which is prone to vibration damage, and compare it against the vibration characteristics of your package design. Every cushioning system has a range of vibrational frequencies in which it amplifies vibration and passes on a more severe vibration to the packaged product than it receives from the transport environment (Figure 15.3). kPk "# Step 6 Consider Vibration Effects$$$]For most vibration-sensitive products, making sure that the package design does not amplify vibration in the product's natural frequency and is enough to prevent vibrational damage from occurring during shipment. For severely vibration-sensitive products, it may be necessary for the package design to actually attenuate the frequencies of concern.^\ # # Step 6 Consider Vibration Effects$$$$!# Step 6 Consider Vibration Effects$$$%"# Step 6 Consider Vibration Effects$$$FMaterial response is often given in diagrams similar to Figure 15.4, which represent performance for a given thickness of material. Note that for any frequency, one can estimate whether the package will perform in direct coupling, amplification, or attenuation mode as a function of the static loading applied to the cushion. GZG&#F Step 7 Monitor Performance If it works, question itGGThere are many assumptions that went into your design development. It is a good practice to monitor the performance of your design in actual use. This will help you to determine if your design is providing more real-world performance than is actually required, or not enough. Monitoring of packaging performance on an ongoing basis can also help determine if further economies can be achieved without sacrificing protection. 0   0(  x  c $cDpy  x  c $dDp   H  0޽h ? 3380___PPT10.Vd`;r_,? .&xY](   tR;uT../jiaoxueluxiang/flash/15-1 five step.exe/ 0DArialBlact+8 08z  !"#$&'()*+,-./0123456789:;<=>?@ABDEFGOh+'0 hp   Lesson 15oTOADssoRadialoTOADlo5ADMicrosoft PowerPointP@0@@DVd@`/_bGg  N  y-- @ !y--'f--N%%$$%%' ( * , . U W X Z\]^^^^^^]\ZXWU.,*('%%$$$--'-- @ !}--f-- $!!--'ff--,$"%(+.1357788--'--%55--'@Arial-. 2 + Lesson 15."System-@Arial-. .2 DSeven Steps for Cushioned .-@Arial-. $2 NPackage Development.--.  2 X.-@Arial-.  2 X%15.--.  2 X,.--. "2 X5װ߲.-՜.+,D՜.+,H    'To determine the amount of functional cushioning material which will provide adequate protection for the packaged item. By functional cushioning material, we mean that portion of the design which directly supports the load and functions to absorb shock during impacts. ' Step 3 Calculate Cushion Requirements(( ' Step 3 Calculate Cushion Requirements((' Step 3 Calculate Cushion Requirements((' Step 3 Calculate Cushion Requirements((GUsing Dynamic Cushioning Curves (Figure 15.1) An Overview Curves are generated by dropping a series of known weights onto a cushion sample from a specified height and measuring the amount of shock experienced by the weights as they impact the foam. In simple terms, this testing represents a product dropping on a cushion from a height likely to be encountered during shipment. The horizontal axis represents a range of static loadings that packaged items might apply to the cushioning material. The vertical axis represents the shock experienced as the cushion is impacted. F;P P   ' Step 3 Calculate Cushion Requirements((Curves are often presented for both first impact and multiple impact (average of drops 2-5) data. An Example [Given] An object to be packaged is a 10-inch cube weighing 60 pounds with a fragility of 50 g's. [Solution] 1. Since a product typically faces repeated impacts during shipment, you will probably wish to use multiple-impact data. 2.The typical drop height for a product of this weight may be estimated from the chart below as 24 inches. TcP PoPPb f' Step 3 Calculate Cushion Requirements(( 3. Obtain the cushioning curves for the cushioning material you wish to use. Locate curves that represent multiple impact data from a drop height of 24 inches. 4. Determining Thickness locate our product's fragility level (50 g's) on the vertical axis of the figure, and draw an imaginary horizontal line across the chart at this level. This separates the chart into two sections: our fragility line and lower, where the packaged item will be able to survive the anticipated shock level, and the section above our line where the shock levels are high enough to damage the product PZZ' Step 3 Calculate Cushion Requirements((Uchoose a thickness of 2 inches for the thinnest cushion thickness. 5. Determining Static Loading and Bearing Area The useable part of the curve is bounded by a static loading of 0.3 psi at the low end, and 1.4 psi at the high end. This tells us that, with a 2-inch cushion, we can apply a static loading anywhere within this "cushioning range" and still protect to 50 g's or lower. The highest static loading value within the cushioning range will result in the most economical design because it will use less cushioning material to provide adequate protection, thus lowering design costs. FDZ4ZZv,{' Step 3 Calculate Cushion Requirements((The cushion bearing area is easily calculated as the product weight divided by our chosen static loading. a) 60 / 0.3 = 200 square inches of foam b) 60 /1.4 = 43 square inches of foam (This is a 78.5% reduction in cushioning material) Designing to the minimum thickness is the general practice. By repeating this procedure with several materials, you can quickly generate comparisons, which will allow you to strike an economical balance between material cost and package size. 0kZZZ( Step 4 Recognizing Design Constraints")&'Y1. Consider Compressive Creep Compressive creep is the gradual loss of thickness a material may experience if placed under a constant load for an extended period of time. Significant compressive creep will result in the packaged product loosening in the cushion and becoming vulnerable to excessive movement inside the package during shipment.:;9' Step 4 Recognizing Design Constraints((As a general rule, creep of 10% is recognized as a practical upper limit. In some cases creep losses of over 10% in thickness have been shown to result in a significant loss of cushion performance. Should it be found that creep in excess of 10% is anticipated, designers should recalculate the functional foam requirement using a lower static-loading figure. Spreading the loading over a larger area will reduce compressive creep. Z' Step 4 Recognizing Design Constraints((Buckling is the non-uniform compression of a cushion. When buckling occurs, the energy of the impact is not transferred evenly throughout the cushion and more shock is transferred to the package contents. Buckling usually occurs when the cushions become too tall and thin. Figure 15.2 provides width-to-thickness coefficients for different static loading values and enable the designer to check for buckling potential. Z' Step 4 Recognizing Design Constraints((' Step 4 Recognizing Design Constraints((' Step 4 Recognizing Design Constraints((' Step 4 Recognizing Design Constraints((Example: Let's assume you plan to use a 3-inch thick pad of ETHAFOAM 220 to cushion a side of your product, which presents a static load of 1.0 psi. In this case, the coefficient is 0.7. Using the formula T x W/T = W, you can now find the minimum width: 3"x 0.7 = 2.1". Your cushion must be at least 2.1 inches wide or long to resist buckling. 3. Consider Extreme Temperature Effects 4Z)Y(' Step 4 Recognizing Design Constraints((RAs with all thermoplastic foams, when they are exposed to extremely high or low temperatures over a considerable length of time, they may be affected. The materials become stiffer at low temperatures and increasingly softer at higher temperatures. In extreme cases, it may become necessary to compensate for these effects in your design.SZS# Step 5 Design Prototypes and Test"$$##Each packaging design must be developed separately, given the large number of variables involved. It is highly recommended that you build and test a prototype of your cushion design to determine its actual performance.  # Step 6 Consider Vibration Effects"$&#$Table 15.3 Typical forcing frequencies of carriers Carrier Frequency Range Conditions Railroad 2 - 7 Hz (suspension) Moving freight car 50 - 70 Hz (structural) Truck 2 - 7 Hz (suspension) Normal highway travel 15 - 20 Hz (tires) 50 - 70 Hz (structural) Aircraft 2 - 10 Hz (propeller) On aircraft floor during flight 100  200 Hz (jet) Ships 11 Hz (on deck) Vibrations caused by 100 Hz (bulkheads) interference to the flow of water by the ship, and from imbalance and misalignment of the propeller shaft system.3PP27 h s!# Step 6 Consider Vibration Effects$$$jEvery mode of transport subjects the packages being shipped to some amount of vibration at various frequencies. In order to provide products which are prone to vibration damage with protection against such effects, it is essential to determine the natural frequency of any component which is prone to vibration damage, and compare it against the vibration characteristics of your package design. Every cushioning system has a range of vibrational frequencies in which it amplifies vibration and passes on a more severe vibration to the packaged product than it receives from the transport environment (Figure 15.3). kPk "# Step 6 Consider Vibration Effects$$$]For most vibration-sensitive products, making sure that the package design does not amplify vibration in the product's natural frequency and is enough to prevent vibrational damage from occurring during shipment. For severely vibration-sensitive products, it may be necessary for the package design to actually attenuate the frequencies of concern.^\ # # Step 6 Consider Vibration Effects$$$$!# Step 6 Consider Vibration Effects$$$%"# Step 6 Consider Vibration Effects$$$FMaterial response is often given in diagrams similar to Figure 15.4, which represent performance for a given thickness of material. Note that for any frequency, one can estimate whether the package will perform in direct coupling, amplification, or attenuation mode as a function of the static loading applied to the cushion. GZG&#F Step 7 Monitor Performance If it works, question itGGThere are many assumptions that went into your design development. It is a good practice to monitor the performance of your design in actual use. This will help you to determine if your design is providing more real-world performance than is actually required, or not enough. Monitoring of packaging performance on an ongoing basis can also help determine if further economies can be achieved without sacrificing protection. $   `X$(  Xr X S k@{4  k r X S tk@ k H X 0޽h ? fffff80___PPT10.Wd`akr.4? .`&