Impact of material parameters on temperature field within clothing laminates
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.
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Rysza d Ko ycki; Halina Sza anska