,x a ‘3.“ umaafia i. . o. .1599 v: Inn-w. $3? «Egg if : . g 2? . , . ‘ufififfi... . lal".‘.. |t| A*F Large Hot-Melt 31.3506 0.8154 524 38.45 <.0001 A*F Large Pre-Applied 31.1255 0.8087 524 38.49 ‘ <.0001 A*F Small 1 Hot-Melt 28.6849 1.7783 524 I 16.13 1 <.0001 A*F Small LPre-Applied 23.6219 0.7830 524 1 30.17 I<.0001 47 Q)_Adhesive on Comer-Mid flap; Hot Melt and Pre-applied adhesive variable: Looking at the graph below, we can say that Hot-Melt adhesive performed better than pre-applied on the midflap location of the boxes. But on the other side pre- applied performed better than hot melt on the corner location of the box. By this reulst we can infer that midflap was good for hot melt and corner location was better for pre-applied. c 32 32 a, 0 0 .2 31 31 .2 ‘ .5 30 .5 g‘ 29 28 g 0 U ‘5 28 27 s s 26 a E 27 25 E A 26 . ‘ _ 24 3 Hot Melt Pre-Applied Figure35. Interaction between adhesive location and adhesive type Table 6. Least square means for adhesive location and adhesive type Least Squares Means Standard Effect c F Estimate Error DF tVaIue Pr>|tI c*F Corner Hot-Melt 29.0250 1.2338 524 23.53 <.0001 c*F Corner Pre-Applied 28.2931 0.7830 524 36.131<.0001 c*F Mid-flap Hot-Melt 31.0105 1.1808 524 26.26 ‘<.0001 c*F Mid-flap Pre-Applied 26.4542 0.8087 524 32.711<.0001 48 c) Box with Full and Half flap; Adhesive pattern long- short: The figure below explains that there long adhesive pattern was better than short for the full flaps. And in both the cases the full flap was significantly better than the half flap boxes. 10' 5 10 -.- .~ 5 7 :I—iLong , 1 e 50 ' - V “l—o—ShortI"~ 50 9 45 . . CW __ .1 _ 45 g “9 40 40 9 C c .9 35 35 .Q 3 a e 30 30 9 Q. g 25 25 g o 20 20 o '9 15 15 .91 “5 (u E .E 175 773' “J u.l Full Flap Ha” Flap Figure 36. Interaction between flap style and adhesive length Table 7. Least square means for flap style and adhesive length Least Squares Means 1 Standard 1 Effect B l D Estimate Error DF tVaIue 1 Pr>1t1 I B*D Full ‘Short 36.3939‘ 0.7964 524 45.70 <.0001 B*D Full Long 43.2494 0.7830 524 55.23 <.0001 13*1) Half Short 17.1203 1.1808 524 14.50 <.0001 13*!) Half Long 18.0187 1.2329 524 14.62 <.0001 d) Large and small box size; Adhesive pattern long- short Graph below states that there was significant decrease in the compressive force for the long length of adhesive with the box size. Large box with long length was 49 found to be the best combination. For the short length of adhesive there was no difference observed with the change of box size. 40' 35 30 30 Estimate of compression force 25 25 20 20 15 10 Estimate of Compression Force U1 5 0 Large Box ~ 0 Small Box Flgure37. Interaction between box size and adhesive length. Table 8. Least square means for box size and adhesive length. Least Squares Means I Standard 1 Effect A D Estimate Error DF tVaIue ; Pr>1t| A*D Large Short 26.85701 0.7964 1524 33.721<.0001 A*D Large long I 35.61901 0.8278 5241 43.703 I<.0001 A*D Small Short 26.6577 1 1.1808 5245 22.58 <.0001 A*D Small1 Long 25.6491 1 1.1914 5241 21.53 <.0001 e) Box with Full and Half flap; Adhesive location on corner and midflap The figure below explains that there was no difference found in the pattern of flap design with change of adhesive location. The full flap box design performed 50 better in both the adhesive location compare to half flap design. Also there was no significant difference observed with the adhesive location within full or half flap design. 17 7 * 7 7 7 7 *‘+* Cornér W 45 . . ~J—Q—Mid Fla l- 45 I” p .. o J 8 40 - PW 1» 4o 8 . I L1. 35 ' ‘ - 35 LL ‘ .5 30 30 .5 g 25 g 25 g E- 20 20 '5. o 15 15 g Q 10 » 10 U E 5 5 E I. 1 Full Flap Half Flap Figure38. Interaction between flap style and adhesive location Table 9. Least square means for flap style and adhesive location Least Squares Means I I Standard Effect 1 B C Estimate Error DF t Value Pr > 1t| B*c Full Comer 40.9794 0.7830 524 52.33 <.0001 B*c Full Mid-flap 38.6639 0.7964 5247754855 <.0001 B*c Half Comer 16.3388 1.2338 524 13.24 1 <.00015 B*c Half Mid-flap 18.8008 1.1807 524 15.92 1 <.0001 f) Large and small box size; Adhesive location on corner and midflap The graph below shows that there was significant difference between large and small box size with the corner adhesive location. Corner location was found to be higher for the large boxes; this can be explained due to the distance between the force applied and adhesive location. For mid flap the adhesive was far away from 51 the compression platen and hence took less force by torque principle. But the mid flap adhesive location there is very small difference observed between the compressive for box sizes. I -l— I 7 7 corner . 35 ._._ -_ 35 1 5 30 , . - , ' 30.9 I C . l .2 25 » ‘ ’ ' 25 '3 I 3 . g a 20 . ' 20 o. o 15 ' 15 o '6 ‘5 o 1 — I” 1 a, 0 10,2, in" m 0 - 0 Large BOX Small Box Figure 39. Interaction between box size and adhesive location Table 10. Least square means for box size and adhesive location Least Squares Means Standard Effect A C Estimate Error. DF tVaIue Pr>|t1 A*c Large Comer 33.1203 0.8084 524 40.97 <.0001 A*c Large Mid-flap 29.3558 0.8165 524 35.95 <.0001 A*c Small Comer 24.1978 1.1914 524 20.31 <.0001 A*c Small Mid-flap 28.1090 1.1808 15241 23.81 1<.0001 9) Large and small box size; with full and Half Flap design From the figure below we can inference that full flap boxes performed way better than the half flap boxes despite box size i.e. is large or small. In full flap design the large size box was better than a small size box. In the half flap design there 52 was no difference observed in the compression strength with the change in box size. 50 1 1 j..." VFuIIFIapL 50 Estimate of Compression force Estimate of Compression force 1 Large Box Small Box Figure 40. Interaction between box size and flap style. Table 11. Least square means for box size and flap style. Least Squares Means Standard Effect A B Estimate Error DF tVaIue Pr>|t| A*B Large Full 44.3864 07964 524 55.73 <.0001 A*B Large Half 18.0897 0.8278 524’ 21.85 <.0001 A*B Small iFull 353569 0.7830 5241 45.03 1<.0001! A*B Small Half 17.0499 1.7783 5241 9.59 1<.0001 4.2.2. Analysis on the Basis of Adhesive Failure: Here the analysis was done by only considering the main effect and ignoring the interaction between the various variables. As closure system was important variable for this project, so percentage of adhesive failure was taken into account 53 for analysis. Critical combinations were studied and average of the adhesive failures. a) If we look at the plot below, we can see that in the large boxes, Hot Melt observed least adhesive failure and tape was the worst closure system having maximum adhesive failure. 100 90 80 * 7O - 60 Adhesive Failure % 01 O PRE-APPLIED HOT MELT . TAPE Figure41 Adhesive Failures in Large Box Size b) The graph below for small boxes explains similar adhesive failure pattern among the three adhesives as shown by large boxes. Hot melt was the best among three closures systems. Although here as well tape closure was found with maximum adhesive failure, but it was better than large size boxes. This trend is also supported by drop data where small taped box performed better than large tape box. 54 Adhesive Failure % 0| 0 l PRE-APPLIED HOT MELT Figure 42 Adhesive Failure in Small Box 0) The chart below shows that pre-applied adhesive found lower adhesive failure than hot melt adhesive in large full flap boxes. Whereas in case of large half flap boxes hot melt was better. 20 Half Flap 1 Full Flap Half Flap Adhesive Failure % I PRE-APPLIED HOT MELT Figure 43 Comparison of Adhesives within Large Boxes 55 d) In the graph below is shown the comparison of two types of application method used for pre-applied adhesive on the corrugated boxes. The slot coat was better application method as it gave less adhesive failure. Adhesive Failure % Slot Coat MMB Figure 44 Comparison of Application method within Pro-Applied adhesive e) In the figure below, we can see comparison of adhesive length pattern on basis of adhesive failure percentage. The Short adhesive pattern was found to be better than long adhesive pattern. This can explained on the basis of force required per unit of adhesive length. 80 in the small length pattern, the force required was more and thus lower adhesive failure. 17 7- 77 7 _7-77 1 25 20 15 10 Adhesive Failure % Figure 45 Comparison of Adhesive Length Pattern 56 f) Comparison of adhesive location is shown below. There were two adhesive locations selected for this study, one at comer and other at mid flap of the box flaps. The Corner location observed lower adhesive failure as comparison to mid— flap. This can be explained on principle of torque. Torque is rotational force measured in Newton-meter. The longer the distance lesser the force is required to move the object. Here midflap is farther than corner location from the platen (acting force). 80 for corner higher force was applied resulting in better adhesive strength. 1 .7 7 7 Adhesive Location Pattern Adhesive Failure % Midflap Corner Figure 46 Comparison of Adhesive location on Box Flap 57 4.3 Analysis of Drop Test Results In drop testing we did a drop test for 5 samples for each design and each box was dropped repeatedly till failure. $0 for 5 samples numbers of drops were recorded and were analyzed for adhesive closure system. The below table shows all the box configuration which took more than 5 drops in total for 5 samples. Table 12. Drop test analysis :- Ngmbeg Of Fagtges 4m 5‘" T t l GI : o a . ue . Type drop drop drop drop drop Drops Box Deslgn Location ; SF-33 2 3 23 Small Box Tape FL-16 3 2 12 Large Full Hot Melt Corner FL-32 1 2 11 Large Full Pro-Applied Corner I FL-08 2 1 1 9 Large Full Pre-Applied Corner 1— HMF-10 1 4 9 Large Half Hot Melt Mid Flap LF-34 2 3 8 Large Tape HL-14 3 2 7 Large Half Pre-Applied Corner MFL-11 4 1 6 Small Full Hot Melt Mid Flap Looking at the table above we can say that small box with tape took maximum number of drops for 5 boxes and was contradicting with the compression data results. This trend is also supported by adhesive failure percentage data where there was less failure as compare to large box with tape. By analyzing the table we also can say that hot melt adhesive took more number of drops for Large Half and Full flap boxes as compare to pre-applied adhesive. The comer location was found to be better than midflap, as there were 4 boxes with having adhesives on corner location as compare to only one in case of midflap. Summary of Key Findings: 58 Compression force data shows: — No Significant difference observed between the Hot melt and Pre- applied (IR) for large size box. — In small case size Hot melt was better than Pre-applied. — For hot-Melt adhesive midflap was better location than corner flap. — Full flap was significantly better than the half flap boxes. — Significant difference between large and small box size with comer flap adhesive location. — Long adhesive length gave higher compression strength than small for large box. Adhesive Failure data:- — Tape was found to have maximum adhesive failure. — For Large Full Flap boxes Pre-applied was found to better than Hot- Melt. — For Half Flap box design, more failures were observed in Pre- applied as compare to Hot Melt. — Short adhesive length was better than long length in terms of adhesive failure. — Slot coat was found to be better application method as compare to MMB. — Comer flap location found less adhesive failure as comparison to Mid Flap. 59 Drop testing results shows — Small box with tape withstood maximum number of drops before failure. — Large hot melt boxes were better than pre-applied for both full and half flap design. — Corner flap location for adhesive application was found to be better than mid-flap. . Box Design: Half Flap box is a promising design for Packaging Industry as it reduces corrugated cost. . The new closure strength test does not correlate with drop test results. - Additional testing on other box sizes, weights and closures needs to be done. 5.0 CONCLUSIONS This study reached the following conclusions based on the different materials and boxes tested: 1. The tape closures show the best closure performance for containment of products during drops followed by hot melt adhesives and IR activated adhesives. 2. The newly developed IR activated adhesive can provide corrugated material savings between 5 to 10%. 6O . The new test method measuring compression strength of an empty corrugated box with closure in a diagonal configuration does not show correlation with performance testing based on edge drop tests. . The boxes with large flap showed better results than half flaps. 61 Appendix 62 Compression Testing Results A.1 Data 8. Figure of HL-2 Force: Deviation: IFAILURETYPEI A | B 1 c I D l E I F I |PERCENTAGEI 65 1 20 1 5 1 1o 1 1 | to to to tear not at 63 A.2 Data & Figure of FS-03 FAILURE TYPE E F to tear at 64 A.3 Data & Figure of FMFS-4 65 A.4 Data & Figure of FS-05 FAILURE TYPE A B C D E F PERCENTAGE 70 20 10 t0 66 A.5 Data & Figure of HS-06 ype Peak load failure 7 5.7 FAILURE TYPE A B C D E F PERCENTAGE 80 5 10 5 67 A.6 Data & Figure of PCS-07 FAILURE TYPE A B C D E F E PERCENTAG 90 5 5 to to 68 A.7 Data & Figure of FL-08 FAILURE TYPE A B C D E F PERCENTAGE 80 20 to to to tear not at 69 A.8 Data & Figure of HS-09 HS-9 ype Peak load failure PERCENTAG 30 40 10 20 FAILURE TYPE A B C D E F E 70 A.9 Data & Figure of HMF-10 HMF-10 FAILURE TYPE A B C D E F PERCENTAGE 25 35 40 to to to tear not at 71 A.10 Data 8: Figure of MFL-11 FAILURE TYPE A B C D E F PERCENTAGE 85 15 to to 72 A.11 Data & Figure of FL-12 FAILURE TYPE A B C D E PERCENTAGE 65 20 15 to 73 A.12 Data & Figure of HL-14 HL-14 Peak load FAILURE TYPE A B C D E PERCENTAGE 45 30 20 to to U'I'TI 74 A.13 Data & Figure of FS-15 FS-15 ype Peak load failure FAILURE TYPE A B C D E F PERCENTAGE 25 55 10 10 to to 75 A.14 Data 8. Figure of FL-16 ype Peak load failure FAILURE TYPE A B C D E F PERCENTAGEI 60 40 to to 76 A.15 Data & Figure of HS-17 FAILURE TYPE A B C D E F PERCENTAGE 55 45 to to 77 A.16 Data & Figure of MFS-18 MFS-18 YPe S.no. Peak load failure 1 FAILURE TYPE A B c p E F PERCENTAGEI 80 20 to to 78 A.17 Data & Figure of FMF-19 FMF-19 Peak load FAILURE TYPE A B C E F PERCENTAGE 75 20 to UIU to to tear not at uncovered 79 A.18 Data & Figure of FL-20 ype S.no. Peak load failure 1 3 5 FAILURE TYPE A B C D E F PERCENTAGE 61.11 38.89 to to to tear not at 80 A.19 Data 8: Figure of HL-22 HL-22 Peak load IFAILURETYPEI A I B I c 1 D I E 1 fl [fERCENTAGEI 50 1 35 I | 5 | 1 1T] to to tear not at 81 A.20 Data & Figure of FS-23 ype Peak load failure A FAILURE TYPE A B C D E F PERCENTAGE 100 to to 82 A.21 Data 8: Figure of FMF-24 ype failure FAILURE TYPE A B C D E F PERCENTAGE 65 5 30 to to tear not at 83 A.22 Data & Figure of HL-26 HL-26 YPe Peak load failure FAILURE TYPE A B C D E F PERCENTAGE 38.46 23.07 7.69 30.76 to not 84 A.23 Data 8. Figure of FS-27 ype failure FAILURE TYPE A B C D E F PERCENTAGE 30 65 5 to to to tear not at uncovered 85 A.24 Data & Figure of FMFL-28 FMFL-28 Peak load FAILURE TYPE A B C D E F PERCENTAGE 60 40 WHERE to to to at 86 A.25 Data 8. Figure of HS-29 HS-29 Peak load FAILURE TYPE A B C D E F PERCENTAGE 30 1O 35 25 87 A.26 Data & Figure of HL-30 HL-30 ype S.no. Peak load failure FAILURE TYPE A B C D E F PERCENTAGE 25 50 8.33 16.67 to to to tear not at 88 A.27 Data & Figure of FCL-31 FCL-31 ype Peak load failure FAILURE TYPE A B C D E F PERCENTAGE 6O 20 10 10 89 A.28 Data & Figure of FL-32 FL-32 S.no. Peak load FAILURE TYPE A B C D E F PERCENTAGE 55 5 20 20 I to to to tear not at 90 A.29 Data & Figure of SF-33 Peak load FAILURE TYPE A B C D E F PERCENTAGE 50 45 5 to to 91 A.30 Data 8: Figure of LF-34 LF-34 ype Peak load failure FAILURE TYPE A B C D E F PERCENTAGE 45 5 50 92 1) 2) Drop Testing Results 3.1 Data & Figure of HL-2 Results of the Drop Testing Hl—2 before drop After drop 82 Data & Figure of FS-03 Fs-03 before drop I ‘ aft drop 93 3) 4) 3.3 Data & Figure of FMFS-4 »‘o_:," F mfs-O4 before drop Afterdrop 3.4 Data & Figure of FS-05 Hs-05 Before drop After drop 94 3.5 Data 8. Figure of HS-06 5) Hs-06 before drop r drop 3.6 Data & Figure of PCS-07 6) FCS 07 before drop After drop 95 3.7 Data & Figure of FL-08 7) Fl-8 before drop After drop 8.8 Data & Figure of HS-09 96 3.9 Data & Figure of HMF-10 Hmf—1 0 before drop 3.10 Data & Figure of MFL-11 MfI-11 before drop After drop 97 3.11 Data & Figure of FL-12 11) Fl-12beforedrop If ‘ Afterdrop 8.12 Data & Figure of HL-14 12) HI-14 before drop After drop 98 B.13Data & Figure of FS-15 Fs-15 before drop After drop 3.14 Data & Figure of FL-16 F L-1 6 before drop After drop 99 3.15 Data & Figure of HS-17 of HS—17 before drop V I After rop 8.16 Data & Figure of MFS-18 16) MFS-18 before drop M After drop 100 3.17 Data & Figure of FMF-19 FMF-19 before drop After drop 3.18 Data & Figure of FL-20 Fl-20 Before drop After drop 101 3.19 Data & Figure of HL-22 19) HL-22 before drop After drop 3.20 Data & Figure of FS-23 20) . FS-23 before drop After drop 102 3.21 Data 8. Figure of FMF-24 FMF-24 before drop After drop B22 There were no samples left for the HL-26 for drop testing. 103 8.23 Data 8- Figure of FS-27 23) meI-BB Before drop After drop 3.24 Data & Figure of FMFL-28 Fmfl-28 Before drop 9 A drop 104 3.25 Data & Figure of HS-29 25) Hs-29 Before drop Aftr drop 8.26 Data & Figure of HL-30 HL-3O before drop after drop 105 3.27 Data & Figure of FCL-31 27) FOL-31 before drop Afterrop 3.28 Data & Figure of FL-32 28) Fl-32 before drop After drop 106 3.29 Data & Figure of SF-33 29) SF-33 before drop After drop 3.30 Data & Figure of LF-34 LF-34 before drop After drop I 107 WHERE Due to delamination of fibers Due to adhesive failure Due to tear in flap Did not failed at 50% yield. Tape uncovered and flap open Fail below preload 'nrnUOCD> 108 9. 5.0 REFERENCES . George G. Maltenfort, Performance and evaluation of shipping containers, Jelmar Publications Inc, 1989. George G. Maltenfort, Corrugated Shipping containers- An engineering approach, Jelmar Publications Inc, April 1990. Diana Twede and Susan E.M. Selke, Handbook of paper and wood packaging technologY; DEStech Publications, Lancaster, Pa., USA 02005. Edited by Frank Kreith and Yogi Goswami; The CRC Handbook of Mechanical Engineering, Chapter 12, Materials- Adhesives by Lehman Richard L. Malcolmson, J.D. The Value of the compression test for corrugated boxes. Fiber Containers 21, no. 4:14, 16 (April, 1936) Grundy, A.V. Engineering aspects of corrugated container purchasing. Fiber Container 25, no. 7:16, 20-1 (July, 1940). Edward M. Petrie, Handbook of Adhesives and sealants, McGraw-Hill, 2000 Pizzi & Mittal, Handbook of Adhesive Technology, Marcel dekker,lnc.,2003 www.specialchem4adhesivescom assessed on 27th April 2006. 10.Schaepe. M, The influence of pin adhesion on edge crush and box compression strength, Corrugating lnt., vol. 2, no. 2, Apr. 2000, pp 35-39 11.http://www.pprc.org/pubs/techreviews/hotmelt/ assessed on 15th April 27, 2006. 12.This “Educational Materials” series textbook entitled “Bonding/Adhesives”. 13. Forsyth, RS; Packaging and case and carton hot melts: fifty years of change and progress, 2001 Hot melt symposium, Hilton Head Island, SC, USA, 10-13 June 2001, 14pp [Atlanta, GA, USA: TAPPI Press, 2001. 14.Sheehan, RL; Box and Closure: Partners in performance; Journal of Packaging Technology; v-2, no.4; 1988 109 15. Bacior L. Michael, Package Closure/Containment Analysis; Dimensions Conference 2006. 16. Brody Marsh, The Wily Encyclopedia of Packaging Technology second edition 1997. 110 lllllllllljllllllflillllllljllllll