scieee Open visual document viewer

Impact of material parameters on temperature field within clothing laminates

Korycki, Ryszard

Abstract

Vnitřní vrstva zajišťuje jak estetické vlastnosti, tak nemačkavost oděvních laminátů. Laminát je tvořen termoplastovým lepidlem mezi vnitřní vrstvou a oděvním materiálem, který je změkčen teplem. Stálou proměnnou je teplota. Rozložení teploty uvnitř laminátu lze určit numerickou simulací pro různé teploty topných desek. Článek analyzuje vliv různých materiálových parametrů na rozložení teploty.

Full text

49 IMPACT OF MATERIAL PARAMETERS ON TEMPERATURE FIELD WITHIN CLOTHING LAMINATES Rysza d Ko ycki1; Halina Sza anska2 1Lodz Uni e si y o Technology, Facul y o Ma e ial Technologies and Tex ile Design, Depa men o Technical Mechanics and Compu e Science, Lodz, Poland; 2Uni e si y o Technology and Humani ies, Facul y o Ma e ial Science, Technology and Design, Depa men o Shoes and Clo hing Technology, Radom, Poland e-mail: 1 ysza d.ko y[email p o ec ed] Abs ac Inlaye s secu e bo h aes he ic quali ies and s i ness agains c easing o clo hing lamina es. Lamina e is c ea ed by he moplas ic glue be ween inlaye and clo hing ma e ial which is so ened by hea . S a e a iable is empe a u e. Tempe a u e dis ibu ions wi hin lamina e can be de e mined by nume ical simula ion o di e en empe a u es o hea ing pla es. Impac o di e en ma e ial pa ame e s on empe a u e dis ibu ion is analysed. In oduc ion Inlaye s secu e aes he ic quali ies and ma e ial s i ness agains c easing o clo hing lamina es [1, 2, 3, 4]. Some pa em e s o inlaye s a e discussed by di e en au ho s [3, 4]. The subs an ial p oblem is a choice o echnology, i.e. hea ing sys em applied o so en he polyme du ing lamina ion c . S oka, Koenen [5]. The e a e some impo an echnological pa ame e s o clo hing lamina es: empe a u e, hea ing ime, p essu e applied a e hea ing, ex e nal ma e ial cha ac e is ics, kind o polyme glue, cha ac e is ics o a hea e sys em. Le us i s de e mine he physical model. S a e a iable is he empe a u e wi hin lamina e s uc u e which consis s o inlaye , ex e nal ma e ial and polyme glue poin s. I should e ec i ely desc ibe he echnological p ocess. The s uc u al shape is de ined by ec o o c ucial poin coo dina es. The mos impo an in o ma ion is he empe a u e dis ibu ion wi hin lamina e du ing he hea ing phase. The only hea sou ce a e hea e s in a hea ing de ice. Hea is anspo ed h ough inlaye , polyme glue laye and ex ile ma e ial. The e a e di e en hea loss mechanisms by adia ion, con ec ion and conduc ion on app op ia e ma e ial su aces. The nex s ep is o desc ibe he ma hema ical model. Hea ans e is desc ibed by hea anspo equa ion and se o bounda y and ini ial condi ions, c . Li [6]; Dems, Ko ycki [7]. Hea ans e equa ion is he second-o de di e en ial co ela ion wi h espec o ec o o coo dina es. The p oblem can be sol ed by using di e en me hods. The mos popula is he nume ical in eg a ion wi hin s uc u e [8, 9]. The o he me hod is o in oduce i s a ia ional o m and ind i s solu ion. The main goal is o analyze he sensi i i y o empe a u e ield o polyme glue laye wi h espec o di e en ma e ial and echnological pa ame e s. Va ious desc ip ions o polyme glue dis ibu ion can be in oduced. I can be modeled as a sepa a e laye o by means o egula o i egula dis ibu ed poin s. Addi ionally, di e en hea -insula ing p o ec ions can be in oduced o imp o e hea ans e , c . side housings. Gene ally speaking, he analyzed p oblem has a 3D space cha ac e . To simpli y he solu ion, some cases can be educed o an op ional c oss-sec ion o s uc u e. The e o e, space 3D p oblem can be educed o i s plane 2D c oss-sec ion. The impo an ac o desc ibing he s uc u e can be he mean empe a u e in he glue laye which is assumed as a compa a i e elemen o es ima e he sensi i i y. 50 1 Desc ip ion o hea anspo Clo hing ma e ials and inlaye made o ex iles ha e pe iodically epe eable s uc u e which should be i s homogenized. The e a e a ew e ec i e homogeniza ion me hods [7, 10]. The mos applied is he ule o mix u e de ined in he ollowing o m. . VV V ξ ; VV V ξ ; ξ λ ξ λλ m m m m mmz     (1) whe e Vm is olume o ib es in m3, V is olume o in e ibe spaces illed by ai o he glue in m3, λm; λ desc ibe hea conduc i i y coe icien s o ma e ial (m) and illing ( ) in W/(m K), ξm; ξ a e olume coe icien s o ib es o olume Vm and he in e ibe spaces o olume V . Hea is anspo ed h ough polyme poin s as well as ai be ween he glue. Bo h polyme glue and ai a e homogeneous. The polyme glue laye should secu e he co ec connec ion be ween he inlaye and ex ile ma e ial. The mos e ec i e me hod is o apply he poin -wise sp ead p ocedu e o polyme . We ob ain egula and i egula polyme poin dis ibu ion o di e en scales desc ibed as “mesh” pa ame e o “compu e poin ” pa ame e . Consequen ly, he mos simple and e ec i e me hod is o de ine polyme glue as he con inuous laye . Sou ce: Meye Fig. 1: Scheme o he con inuous au oma ic usion p ess KFH 600 o shi – and blouse usion wi h p essu e cooling s a ion a he ou pu Sou ce: Meye Fig. 2: Scheme o he In e al Con ac Cooling wi h he CoolVac Sys em 51 The des ip ion o hea anspo depends on echnology and hea ing p ess applied. The e a e di e en solu ions o a ious hea ing sys ems. Le us assume he con inuous au oma ic usion p ess KFH 600 o shi – and blouse usion wi h p essu e cooling s a ion a he ou pu , c . S oka and Koenen [5], Figu e 1, Figu e 2. P ess de ice has he addi ional con ac cooling o secu e he egula hea anspo and equalized empe a u e wi hin glue laye . Le us assume he s eady hea anspo desc ibed by ime-independen hea lux densi y o hea ing de ices. Nei he inlaye no ex ile s uc u es con ain hea sou ces. The only hea sou ce a e always hea e s wi hin hea ing p ess. I means ha hea can be only los du ing hea ing p ocess by lamina e. Hea can be accumula ed by ex ile ibe s and anspo ed o su oundings h ough ex e nal s uc u al bounda y. In oducing now hea balance which is he sum o hea losses, we o mula e he hea anspo equa ion. I is he second-o de di e en ial equa ion wi h espec o ec o o coo dina es. To sol e he abo e equa ion, i is necessa y o de e mine he se o bounda y condi ions. I depends on he pa icula solu ion o hea ing p ess, c . Figu e 3. 1 – hea ing elemen s, 2, 7 – hea ing de ices, 3 – inlaye , 4 – homogenized polyme laye , 5 – side he mal housing, 6 – ou e ex ile ma e ial Sou ce: Own Fig. 3: Scheme o ma e ial laye s in hea ing de ice The uppe pa o inlaye and he lowe pa o ex ile ma e ial a e exposed o cons an empe a u e T = T0. This bounda y po ion ΓT is subjec ed o he i s -kind condi ion. The side pa s o hea ed elemen s as well as ex e nal housing a e subjec ed o con ec i e and adia i e hea anspo . The e a e bounda y pa s ΓC and Γ loaded by con ec ional and adia ional hea lux densi ies i.e. he hi d-kind and adia ion condi ions. We assume on in e nal bounda ies Γi he same hea lux densi ies, i.e. he ou h-kind condi ions. Hea anspo equa ion o (i)- h laye supplemen ed by se o condi ions is shown in Figu e 4 and desc ibed by Eq. (2). Sou ce: Own Fig. 4: Bounda y condi ions o sys em inlaye – polyme glue – ex ile ma e ial 1 2 3 4 6 7 5 ΓC: qn=qn con Γ : qn=qn ΓT T=T0 Γi ΓT T=T0 ΓC: qn=qn con Γ : qn=qn Γi qn (i)=qn (i+1) 52           ; y x ; T 0di i *iii i              xx qAq q                                 . qq ; Tσq ; T-Thq ; TT i 1i n i n 4i n C i nC T 0i       xxx xxx xxxx xxx (2) whe e q is ec o o hea lux densi y, q* is ec o o ini ial hea lux densi y, qn=n·q deno es ec o o hea lux densi y no mal o su ace de ined by uni ec o n, A is ma ix o hea conduc ion coe icien s, T is empe a u e, is eal ime, T0 deno es p esc ibed empe a u e, h is su ace ilm conduc ance, T is su ounding empe a u e, σ is S e an-Bol zmann cons an . 2 Impac o ma e ial pa ame e s on empe a u e ield The e a e some basic pa ame e s which can in luence he clo hing lamina e. The mos impo an a e he ollowing:  Type o lamina e. Inlaye can be made o di e en ex iles: ab ics, kni ed ab ics and non-wo ens which depends on p edic ed applica ions. Thus, su ace mass and in e nal po osi y a e also impo an and limi ed o he speci ic lamina e.  Type o ibe s wi hin inlaye ; he mos popula a e: polyes e , polyamide, co on, iscose, Lyc a- ibe s and bamboo ibe s.  Place and a ea o applica ion which de e mines s i o he mo e lexible connec ion.  Finishing p ocedu e which secu es s abili y and aes he ic quali ies o ex ile lamina e.  Lamina ion echnology de ined by hea sou ce pa ame e s, loca ion o hea ing de ices, ime o hea ing and ime o p essu e, o ce wi hin he p essu e olle e c. Le us analyze he sensi i i y i.e. he impac o he abo e men ioned pa ame e s on empe a u e dis ibu ion wi hin polyme glue laye . To de e mine empe a u e ields in ex ile lamina e, i is con enien o assume he same hea lux densi y o he hea e . The homogenized polyme laye has he same geome y and hea anspo condi ions wi hin he hea ing de ice. The hea desc ip ion is consequen ly simpli ied o he 2D plane p oblem. 2.1 Impac o ma e ial po osi y on empe a u e ield We assume he ou e ex ile made o wo en ab ic and he co on inlaye , bo h o iso opic hea ans e p ope ies. Ma e ial pa ame e s can be de ined acco ding o [6,11,12]. Iso opic ma e ial has he single-componen ma ix o hea ans e coe icien s de ined o i- h laye     λλ ii A ; i=1,2,3; ( o inlaye , polyme laye , ou e ex ile ma e ial). Hea ans e coe icien o co on ib e be o e homogeniza ion is cons an λ=0,072W/(mK) whe eas o polyme glue empe a u e-dependen : λ=0,08W/(mK) o T<115°C, λ=0,10W/(mK) o 116°C<T<125°C; λ=0,11W/(mK) o 126°C<T<135°C; λ=0,12W/(mK) o 136°C<T<145°C. The hea ans e capaci y o co on is c=1320J/(kgK); polyme c=1200J/(kgK). The po osi y o co on ab ic is assumed as cons an ε=0,350. The ai con en wi hin he laye o polyme is also de ined as cons an ε=0,450. F ee spaces a e illed by ai o he cons an hea ans e coe icien λ=0,028W/(mK) and cons an hea ans e capaci y c=1005J/(kgK). The su ounding empe a u e wi hin he housing is assumed T∞=25°C. The su ace ilm conduc ance has he cons an alue h=0,1 W/(m2 K). The p oblem was sol ed be means o ADINA-so wa e. The s uc u e is app oxima ed by 3D space Fini e Elemen Ne made o 4-nodal elemen s because con ec ion and adia ion a e de ined by ADINA-p og am as he spa ial unc ion, Figu e 5a. Hea ans e equa ion is 53 in eg a ed using he Gauss me hod [9]. The ob ained empe a u e dis ibu ion is shown in Figu e 5b. The side su aces ha e complica ed shapes subjec ed o hea con ec ion and hea adia ion. Consequen ly, he cen al polyme laye has unequal empe a u e dis ibu ion which can in luence he s abili y o lamina e c ea ed. Tempe a u e maps a e always symme ic ela i e o e ical plane o symme y which con i ms he co ec calcula ions. F ee spaces wi hin polyme laye illed by ai a e hea isola o s and p e en he hea ans e . Tempe a u e maps enable o c ea e he mean empe a u e wi hin he polyme glue laye s. empe a u e o he pla e wi hin hea ing de ice. The mean alue o he empe a u e in he homogenized laye made o polyme and ai is de e mined in 27 poin s loca ed symme ically wi hin his laye . In enginee ing p ac ice, alues o po osi y o co on ab ic can change signi ican ly and i is now assumed a bi a y om he ange 0,250≤ε≤0,450. These wo alues can help o de e mine he mean empe a u e o he polyme laye by means o empe a u e maps by means o he abo e desc ibed p ocedu e. Di e en po osi ies de e mine a ious hea ans e coe icien s and hea ans e condi ions. The ob ained mean empe a u es a e shown in Figu e 6. a) Fini e Elemen Ne o homogenized laye o polyme , b) homogenized laye o polyme , empe a u e o uppe and lowe su aces T = 110 °C; empe a u e in housing T∞ = 25 °C Sou ce: [13] Fig. 5: Fini e Elemen Ne and example o empe a u e dis ibu ion 54 Sou ce: Own Fig. 6: Mean empe a u e o polyme laye o di e en co on po osi ies The ob ained dis ibu ions o mean empe a u es s. empe a u e o pla e in hea ing de ice a e simila . The cou ses can be app oxima ed linea ly. I is e iden ha he highe he po osi y, he be e isola ion o polyme glue laye . Thus, he change o po osi y can in luence he mean empe a u e o he polyme laye . 2.2 Impac o su ace masses on empe a u e ield Change in mass in ac de e mines a ious hea ans e coe icien s. Calcula ions a e de e mined simila ly o p e ious case o he po osi y o he co on ab ic ε=0,350. We can de e mine a e homogeniza ion ha he hea ans e coe icien s can now change wi hin he ange 0,048W/(mK)≤ε≤0,055W/(mK). The ob ained empe a u e maps ha e analogical dis ibu ion o he shown in Figu e 5b. Mean empe a u es a e conside ably close as shown in Figu e 6 o he po osi y ε=0,350. The di e ences a e no g ea e han 2%. Thus, he pa ame e is de e mined now in Figu e 6. Consequen ly we can conclude ha he mean empe a u e is no sensi i e o change o su ace mass o he inlaye ma e ial. 2.3 Impac o ype o ibe s wi hin inlaye on empe a u e ield The nex p oblem is o de e mine he sensi i i y o lamina e wi h espec o di e en ibe s applied. The mos popula a e: polyes e , polyamide, co on, iscose, Lyc a- ibe s, bamboo ibe s ec . The choice o ibe s de e mines hea ans e coe icien o he inlaye ma e ial. Simila ly o subclause 2.1, iso opic ma e ial has he single-componen ma ix o hea ans e coe icien s     λλ ii A ; i=1,2,3. Hea ans e coe icien be o e homogeniza ion is cons an and equal o polyes e (PES) λ=0,200W/(mK); polyamide (PA) λ=0,210W/(mK); co on λ=0,072W/(mK); iscose λ=0,063W/(mK) and Lyc a λ=0,025W/(mK). Fo simplici y, ab ic po osi y is assumed as cons an ε=0,350. All pa ame e s ch ac e izing polyme glue, ai and su ounding a e de ined in subclause 2.1. Thhe p oblem was sol ed by means o ADINA- so wa e. The s ucu e is de ined by 3D space Fini e Elemen Ne made o 4-nodal elemen s. Hea ans e equa ion is in eg a ed using he Gauss me hod [9]. The ob ained empe a u e dis ibu ion has always he same cha ac e as shown in Figu e 5b bu he alues a e now di e en . Tempe a u es on side su aces a e conside ably lowe han in he cen e o he inlaye because he shapes a e complica ed as well as subjec ed o bo h con ec ion and adia ion. The empe a u e maps a e symme ic ela i e o e ical plane which con i m he co ec calcula ions. 20 30 40 50 60 70 80 90 100 20 40 60 80 100 120 140 Mean empe a u e o polyme laye [°C] Tempe a u e o pla e in hea ing de ice [°C] 0,45 0,35 0,25 55 The empe a u e maps help us o c ea e he mean empe a u e dis ibu ion in polyme laye s. empe a u e o pla e wi hin he hea ing de ice o di e en ma e ials. The mean empe a u e wi hin he homogenized laye made o polyme and ai is de e mined in 27 poin s loca ed symme ically. The mean empe a u es a e illus a ed in Figu e 7. Sou ce: Own Fig. 7: Mean empe a u e o polyme laye o di e en inlaye ma e ials The mean empe a u es a e ela i ely close and he dis ibu ions can be app oxima ed by a s aigh line. The highe he hea ans e coe icien o inlaye ma e ial, he be e he hea anspo h ough he ex ile inlaye . Thus, he mean empe a u e wi hin polyme laye is now highe han he empe a u e o he mo e insula ing ma e ial o lowe hea ans e coe icien s. 2.4 Impac o o he ac o s on empe a u e ield The e a e some o he ac o s which can in luence he empe a u e dis ibu ion wi hin he polyme laye . Place and a ea o applica ion can c ea e a s i o mo e lexible connec ion. The main di icul y is ha he e is a p oblem o pa icula lamina e connec ion which should be analyzed indi idually. I is di icul o de e mine he gene al hea anspo model desc ibing all pa icula cases o lamina ion echnology. Finishing p ocedu e helps o secu e he s abili y and aes he ic quali ies o ex ile lamina e. The e a e di e en inishing echnologies o a ious pa ame e s. Thus, a he momen i is impossible o de ine he hea ans e coe icien p ecisely. Addi ionally, ma e ial cha ac e is ics a e inishing p ocedu e can change laye by laye wi hin ex ile ma e ial. These phenomena can be desc ibed s a is ically wi hin each laye . Lamina ion echnology is a complex p oblem de ined by hea sou ce pa ame e s, he loca ion o hea ing de ices, he ime o hea ing and he ime o p essu e, he o ce wi hin he p essu e olle e c. The exac desc ip ion wi hin subclause In oduc ion de e mines he speci ic case o lamina ion echnology. Any o he p oblems should be de ined and sol ed indi idually. Conclusion Tempe a u e maps can gi e some impo an in o ma ion conce ning maximal and minimal alues o s a e a iable wi hin ex ile lamina e. The mean empe a u e wi hin polyme laye can be u he de e mined in selec ed 27 poin s. This empe a u e is assumed as he pa ame e cha ac e izing polyme laye and consequen ly ex ile lamina e. The e a e some pa ame e s 20 30 40 50 60 70 80 90 100 20 40 60 80 100 120 140 Mean empe a u e o polyme laye [°C] Tempe a u e o pla e in hea ing de ice [°C] Lyc a iscose co on PES / PA 56 which can in luence he mean empe a u e. We can also desc ibe he sensi i i y o he mean empe a u e o hese pa ame e s. We ha e p o ed ha he ma e ial po osi y and ype o ib es wi hin inalye can in luence he empe a u e ield o polyme glue. Mo eo e , he su ace mass is no sensi i e in ela ion o he mean empe a u e. O cou se, a ew addi ional pa ame e s can be deeply analyzed, c . he place and he a ea o applica ion, inishing p ocedu e, lamina ion echnology e c. The pe o med analysis can be also applied o shape op imiza ion wi hin he inlaye ma e ial. We can in oduce he space 3D s uc u e wi h espec o di e en pa ame e s. The p oblem should be sol ed nume ically because only he basic cases can be calcula ed analy ically. The nex impo an p oblem is o in oduce he co ec physical and ma hema ical models o hea ans e wi hin ex ile lamina e. The simples solu ion is always he only homogenized polyme laye bu i can lead o some impo an and in e es ing conclusions. The mo e complica ed shape app oxima ion can in oduce he poin wise glue poin s as well as de ailed analysis o glue poin s / ee spaces be ween hese poin s. Li e a u e [1] KORYCKI, R.; SZAFRANSKA, H.: Modeling o hea ans e wi hin clo hing lamina es, P oceedings o Au ex 2011, 11 h Wo ld Tex ile Con e ence, 08-10 June 2011 Mulhouse, F ance, 2011, 598 – 603. [2] KORYCKI, R.; SZAFRANSKA, H.: Modelling o hea ans e in clo hing lamina es wi h espec o glue poin pa ame e s, P oceedings o Au ex 2012, 12 h Wo ld Tex ile Con e ence, 13-15 June 2012 Zada , C oa ia, 2012. [3] PAWŁOWA, M.; SZAFRANSKA, H.: Fo m Du abili y o Clo hing Lamina es om he S andpoin o Main enance P ocedu es, Fib es and Tex iles in Eas e n Eu ope, Vol. 62 (2007) No.3, 97-101. [4] SZAFRANSKA, H.; PAWŁOWA, M.: Aes he ic Aspec s o Clo hing P oduc s in he Con ex o Main enance P ocedu es, Fib es and Tex iles in Eas e n Eu ope, Vol. 64-65 (2007) No.5-6, 109-112. [5] SROKA, P.; KOENEN, K.: Handbook o Fusible In e linings o Tex iles. Ha ung – Goo e Ve lag Cons ance, English– language, 1997. [6] LI, Y.: The science o clo hing com o , Tex ile P og ess, Vol. 15, No. 1,2; 2001. [7] DEMS, K.; KORYCKI, R.: Sensi i i y analysis and op imal design o s eady conduc ion p oblem wi h adia i e hea ans e , Jou nal o The mal S esses, 28, 213- 232, 2005. [8] KOSMA, Z.: Nume ical me hods o enginee ing applica ions (in Polish), Technical Uni e si y o Radom, Radom, Poland, 2008. [9] KACKI, E.; MALOLEPSZY, A.; ROMANOWICZ, A.: Nume ical me hods o enginee s (in Polish), Technical Uni e si y o Lodz, Lodz, Poland, 1997. [10] KORYCKI, R.: Sensi i i y analysis and shape op imiza ion o ansien hea conduc ion wi h adia ion, In e na ional Jou nal o Hea and Mass T ans e , 49, 2033 – 2043, 2006. [11] HAGHI, A. K.: Mechanism o hea and mass ans e in mois po ous ma e ials, Ju nal Teknologi, Vol. 36(F), 1-14, 2002. 57 [12] URBAŃCZYK, G.: Physics o ib es (in Polish), Technical Uni e si y o Lodz, Lodz, Poland, 2002. [13] KORYCKI, R.; SZAFRANSKA, H.: Modelling o he Tempe a u e Field wi hin Tex ile Inlaye s o Clo hing Lamina es, Fib es and Tex iles in Eas e n Eu ope, Vol. 21(2013) No.4, 118-122. Rysza d Ko ycki; Halina Sza anska