User s of Br itish Stand ar ds a re resp nsible for their corr ect a pl ica tion.. Amendment s is ued sinc p blcation í±Đ đãạ áơ ịơã-á Íơ¿ẳ¿đ ẳ- ì²-ơãơôơã±... ISO col la ora tes cl osely
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ISO
ICS 4 1 0; 8 1 0.1
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Trang 2T is British Stand rd, ha ing
be n prep r d u de the
dire ctionof the Enginee ring
Se cto Board,was publshed
u de the autho ity of the
Stand rds Board and c me s
into efet on
15 N ovembe 19 8
â BSI 0 -19 9
ISBN 0 5 0 3 6 1 9
This Br iti sh Stand ar d r eprod ces v er ba tim ISO1 3 7:1 9 an i mpl ements it
as the UK national stan a rd
The UK p r ti cip tion i n its pr ep r ation w as entrusted to Tech i cal Comm it e
AUE/4, Ty r es and w he ls for motor v ehicl es, w hich ha s the r esp nsi bii ty to:
— ai d en u ir er s to u d er stan the te t;
— present to the resp nsible interna tional/ Eur op a n commi tte any
enquiri es on the i nter pr etati on, or pr op sal s for chang e, an ke p the UK
inter ests informed;
— monitor r el ated i nter national an Euro e n d ev elo ments an
promulg a te them in the UK
A l ist oforg a nizations re r esented on thi s commit e ca n b o tai ned on
r eq est to its secr etar y
Cros - re e enc s
The Br i tish Standar d s whi ch impl ement intern ational or Euro e n
publcations refer red to in this d ocument ma b fou d in the BSI Stand ar ds
Catal og ue u d er the secti on entitled “ Inter nati onal Stand ar ds Cor resp nd en ce
Ind ex”, or b using the “ Find ” faci ty ofthe BSI Stand ard s Electr oni c
Catal og ue
A Bri tish Stan a rd d oes n ot pur por t to includ e al l the neces ary pr ov i sions of
a contr act User s of Br itish Stand ar ds a re resp nsible for their corr ect
a pl ica tion
Com planc wit h a Brit ish Stan ard does not ofit self c onf r imm unity
f om leg al o lg ations
S mmary of pag es
This docum ent comprises a font cov er , an i nside font cov er , p g es i an i,
the ISO title p g e, p g es i to i v , p g es 1 to 8, an insid e b ck cov er an
a ba ck cov er
This sta ndar d has b en upda ted (se co y r ig ht d ate) and ma y hav e had
amen ments incorp r ated Thi s wil l b i ndicated in the amend ment ta l e on
the i nsi de font cov er
Amendment s is ued sinc p blcation
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Pag e
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Contents
Pag e
An e B ( i nfor ma ti v e) Me sur ement methods ofmoment of
i ner ti a for dr um a nd ty r e a ssembl y — Deceler ation method 7
Fig ure 1 — Fr ee-b d y diag r am of ty re/ d rum sy stem,
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Foreword
ISO (the Interna tional Or g ani zation for Stan a rd ization) i s a world wide
fed er ation of nati onal stand ard s b di es ( ISO memb r b d i es) The work of
pre ar i ng Interna ti onal Stand ar ds i s normally car r ied out throug h ISO tech i ca l
commit e s Ea ch memb r b d y i nter ested in a subject for which a tech i cal
comm it e has b en esta bli shed ha s the rig ht to b r epresented on tha t
commit e Inter national or g anizati ons, g ov er nmenta l a nd non-g ov ernmental,
i n laison wi th ISO, also take p r t in the work ISO col la ora tes cl osely wi th the
Inter nati ona l Electr otechnical Commi ssi on ( IEC) on a ll mater s of
electr otech i cal stan a rd i zation
Draft Internationa l Stan a rd s ad opted by the tech i ca l commit e s ar e
cir cu lated to the memb r b d ies for v oti ng Publcati on a s an Inter national
Stand ar d r eq ir es a pr ov al b a t l east 7 % of the memb r b d ies castin a v ote
Inter nati onal Stand ar d ISO1 3 7 was pre a red by Technical Commit e
ISO/ TC3 ,Tyre s, rims and valve , S bcommi tte SC1 ,Cyc le, mo e d ,
motorc ycle tyr s a d rims
An e A forms an integ r al p r t of thi s Inter national Stand ar d An e B an
An e C a re for information only
Desc ipto s:Roa vehicle , motocycle , tyr s, pneumatic tyr s, te ts,la oato y te ts, physical
te ts, rl ng te ts
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Thi s Inter national Stand ar d sp ci fies methods for
me sur in r ol l in g resistance, u nder contr oll ed
la oratory condi tions, for new pneumatic ty res
d esig ned pr im ar ily for use on motor cy cl es The
r el ationshi p b twe n v alues o tai ned an the fuel
econ omy ofthe v ehicl e is u d eter mined , an such
v alues are not inten ed to b used to ind icate lev el s
of p r for man ce or q al i ty
Thi s Inter nati onal Standar d is a pli ca l e to a ll
motor cy cl e ty res
I ena bl es comp r isons to b mad e b twe n the
r ol ling r esista nce ofnew ty r es when they a re
fr ee-r ol ling str aig ht ahea d, in a p sition
p r pen icu lar to the dr um outer sur face, an in
ste d y -sta te cond iti ons
In me sur ing ty r e roll i g resistance, it i s neces ar y
to me sur e sma ll for es i n the pr esence of much
lar g er for ces I is, ther efor e, es enti al that
equipment an i nstr umentati on of a pr opri ate
ac ura cy b used
The fol lowi ng stand ard contains pr ov i si ons which,
thr oug h r efer ence in thi s te t, constitute pr ov i sions
of this Inter nati onal Standar d At the time of
publcati on, the ed ition i nd icated was v al i d Al
stan a rd s ar e subject to r ev i sion an p r ti es to
ag r eements ba sed on thi s Inter national Stand ar d
ar e encour ag ed to i nv esti g ate the p s i bi lity of
a pl y i ng the most recent ed ition ofthe stand ard
in i cated b l ow Memb r s ofIEC an ISOmaintain
r eg i ster of curr entl y v a li d Internationa l Stand ar ds
ISO 4 2 -1:1 8 , Deinitions ofsome te rms us d in
the ty re ind ustry — Part 1: Pne umatic t yr s
For the pu rp ses ofthis Inter national Stand ar d, the
d efi nitions g i v en i n ISO4 2 -1 a nd the fol lowi ng
d efi nitions a ply
3.1
roling r sist anc
F
r
los ofener g y ( or ener g y consumed) p r u i t of
d istance
NOTE T e SI u it cnventionaly usd fo the ol ng rsistanc
is the newton m etr pe r metre (Nãm/ m)
this is eq i v alent to the dr ag for ce in newtons ( N)
3.2
roling r sist anc coe fic ient
C
r
r atio ofthe r ol ling resistance, in newtons, to the lo d
on th e ty re, i n newtons
NOTE T is quantity is dimensionle s
3.3
capped inflat ion
proces of infla ti ng the ty r e an al lowi ng the
i nfla ti on pr es ur e to bu d up, as the ty re i s wa rmed
up while r un ing
3.4
r g ulated inflation
proces of inflatin the ty re to the r equ ir ed pr es ur e
i nde en ent ofits temp r ature, an ma intai ni ng
this infl ation pres ur e whil e the ty r e ru s u nder
l oad
NOTE T is is mot c m only done b using a r gulated
pr sur s ur e atac hed to the tyr thro ugh a r tating u ion
3.5
parasitic los
l os of ener g y ( or ener g y consumed) p r u it
d istance ex clud ing ty r e l os es, an at ri buta l e to
a rody na mic los , b ar i ng ficti on an other sour ces
ofsy stematic l os w hich ma y b in er ent i n the
3.6
skim r ading
ty pe of p r asiti c los mea sur em ent, in which the
ty re is ke t r ol ling ,withou t sli pp g e, wh e r ed uci ng
the ty r e loa d to a l ev el a t whi ch energ y l os w ithin
the ty r e itsel f i sv ir tual l zer o
3.7
m ac hin e r ading
ty pe of p r asiti c los me surement, inv olv i ng los es
ofthe test machi ne, e clusi v e of l os es i n the
r otatin spi ndl e whi ch ca rr ies the ty r e a nd r im
4 T est methods
The folowi ng al ter nati v e me sur ement methods
ar e g i v en in this Internationa l Stan a rd :
a) For e method : the re ction for ce at the ty r e
spind l e
b) Torque method : the tor que input to the test
d rum
c) Power method: the p w er input to the test
d rum
d ) Decelera tion method: the deceler ation of the
test dr um an ty r e a ssembly
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5.1 Drum spec ific ation s
5.1.1Diameter
The test dy nam ometer shal ha v e a cy lindr ical
fly whe l ( dr um) w i th a d iameter of b twe n 1,5m
an 3m i nclu si v e ( refer ence d r um
d iameter : 1,7 m) I t shoul d b noted tha t the
r esults a re di ffer ent; se 9.3 for d r um d ia meter
cor recti on for compa risons, i f neces a ry
5.1.2Surfac
The su rface of the d r um shal b smo th ste l or
tex tur ed an shal l b ke t cl ean ( se cla useA 6)
5.1.3Width
The w id th of the dr um test su rface shal l e ce d th e
wid th of the test ty re tre d
5.2 Tes rim
The ty re shal b mou ted on a test r im, as sp cified
in An e A
5.3 Lo d, al gnm ent, con trol an
in strument ation ac uracy
Me surement of these p r ameter s shal l b
sufici ently ac ur ate an pr ecise to prov id e the
r eq ir ed test da ta The sp ci fic an r esp cti v e
v alues a re show n i nAn e A
5.4 The m al environ men t
5.4.1Re erenc conditions
The r efer ence ambi ent temp r atur e, a s me su red
on the rotati onal ax is ofthe ty re,1m aw ay fr om the
plan e touchin the ne r est ty re sid ewall , shal
5.4.2Alternativ conditions
Ifthe r efer en ce temp r atur e cannot b o tained , the
r ol ling resistance me sur ement shall b cor rected to
stand ard temp r atur e cond itions in a ccor da nce
with9.2
5.4.3Drum surfac temperature
Car e should b ta ken to ensur e that the
temp r atur e of the test d rum sura ce is
a pr oxi mately the same as the a mbi ent
temp r atur e a t the b g in in of the test
6 T est conditions
The test consists of a measurement ofr oli ng
r esista nce in whi ch the ty r e is infla ted a nd the
infla tion pr es ur e a ll owed to buid up (i “ ca pp d
ai r ”)
6.1 Tes spe ds
The v alu e shal l b o tai ned at a dr um v eloci ty of
8 km/ h for ty res mar ked wi th a sp ed sy mb l
a ov e “L”;
5 km/ h for ty res mar ked with a sp ed sy mb l
“ L” an b low
6.2 Tes lo d
The standar d test lo d sha ll b computed fom
6 % ofthe ma x imu m lo d ca pa ci ty of the ty r e
for l ig ht a nd stand ar d lo d v er sions;
8 % ofthe ma x imu m lo d ca pa ci ty of the ty r e
for r ei nfor ced v er sion
I shal b ke t withi n the tolera nce sp ci fied in
6.3 Tes infl ation pr s ur
The infl ati on pr es ure shal l b
2 0 kPa for lg ht a nd stand ar d lo d v er sions;
2 0 kPa for r ei nfor ced v er sion
The infl ati on pres ure shal l b ca p d wi th the
ac u racy sp cifi ed i nA.4.1
6.4 Durat ion an d velocity
When the deceler ation method is sel ected , the
fol low in r eq i rements a ply :
a) for d r ati on, ỷ t, the time incr ements shal not
e ce d0,5s;
b) any v ari ati on ofthe test dr um v elocity shal l not
e ce d1km/ h
7.1 G ene al
The choice of an i nd iv id ual method is l eft to the
tester For e ch method, the test measurements
shal l b conv er ted to a r oll i g resistance for ce actin
at the ty r e/ d r um i nter fa ce
The test pr oced r e ste s d es r ib d in7.2 to7.7 shal l
b foll owed in the sequence g i v en
To ensu re r ep a ta bil ity of me sur ements, a n i ni ti al
br ea k-i n an d co li ng p r iod is r equir ed pri or to the
star t of the test S ch a br ea k- n should b car ried
ou t on a test d r um ofat le st1,5m d i ameter for a
p r iod ofat l east 1h, a t a minimum v eloci ty
of8 km/ h, w i th the lo d an i nfla tion pr es ur e
g i v en in6.2 an 6.3 r esp cti v ely
7.3 The mal con ition ing
Pl ace the infl ated ty re in the therma l env i ronment
ofthe test location for at lea st3h
7.4 Pr s ur adjust men t
After ther mal cond itioni ng , the inflation pr es ur e
shal l b a djusted to the test pres u re, an
v er ified1 mi n after the adjustment w as ma de
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7.5 Warm- up
The ty r e shal b r un at constant test v eloci ty u ti
r eachin a sta i lised stea dy -state v a lue of r oll ing
r esi stance A wa rm-up p r iod ofat l eas t3 mi n at
the test sp ed i s r eq i red
7.6 Measur ment and r cordin g
The folowin shal l b me sur ed an r ecor ded
( se Fi g ure 1):
a) test v elocity ,U
n
;
b) loa d on the ty r e normal to the d ru m sur face,
L
m
;
c) t est infl ati on pr es ure:
1) i nitial, a s defined in7.4,
2) fi na for ca p d inflation;
d ) the d ri v ing torque on the dr iv e shaft, T
t , the
ty re spind le for ce, F
t , the input p wer , VI A, or
the d eceler ation of the test d rum/ ty re/ whe l
as embly ,ỷ V/ ỷt, d ep nd in on the method ;
e) distan ce, r
L ( se 8.2.1);
f) ambient temp r ature, t
amb
;
g ) test d rum rad i us, R ;
h) test method chosen;
i ) test ri m ( d esig nati on and mater ia l)
7.7 Measur ment of parasitic l os es
Deter mi ne p r asi ti c los es b one ofthe pr oced ures
g iv n in 7.7.1 to 7.7.3
7.7.1S kim rea ing
a) R ed uce the l oa d to mainta in the ty re at the test
v eloci ty wi thout sl ip a g e to, for ex ampl e, 5 N
b) R ecord the spindl e for e, F
p , i nput torque, T
p ,
or the p wer, whi chev er a pl ies
c) Recor d the lo d on the ty r e normal to the d rum
sur face,L
p
NOTE T e measur d v lue include s the bearing and
ae od namic lo s s o f the whe l,the tyr , and the drum los s
which ar als to be c nsideed
7.7.2Machine rea in
a) R emov e the ty re fr om the dr um sur face
b) At the test v el ocity ,U
n , r ecor d the i nput
tor que,T
p , the p wer , or the test dr um
d ecel er ati on, w hichev er a pl i es
NOTE T e measur d v lue include the drum lo ss to be
cnside ed
Fig ur 1 — Fr e- body diag ram oft yr /drum sys em, as umin no bearin g an d windag e los es
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7.7.3De elerat ion method
a) Remov e the ty r e fr om the test sur fa ce
b) Record the d eceler ation ofthe test
d rum,ỷ V
o /ỷ t and that of the u l oa ded
ty re,ỷ V
po
/ ỷ t
NOTE T e measure d v lue include the bearing a nd
ae od na mic lo s s of the whe l, the tyr , and the drum lo s s
which ar a ls to be c nside e d
8.1 S btraction of parasit ic los es
The p r asi tic los es shal l b subtr acted as shown
in8.1.1,8.1.2 or 8.1.3
8.1.1Skim rea ing
S btr act the skim re d ing fr om the test
me sur ement
8.1.2Machine rea ing
S btr act the ma chi ne re din fr om the test
me sur ement
NOTE When the machine r a ing method is us d to dete mine
pa rasitic los s fo the to que o powe method,the rsulting
r l ng r sistanc include aeod namic lo se s o f the tyr and
whe l as wel as the tyr-spindle friction
8.1.3Parasitic losses fo the de eleration
method
Cal culate the p ra si tic l os es F
pl
i n newtons as
w her e
I
D
i s the test d ru m i ner tia in r ota tion, in
kil og ram metr es sq a red;
R i s the test d rum surace ra dius, in metr es;
V
vo
is the test d rum ang ul ar v el oci ty , wi thout
ty re, in ra dians p r second ;
ỷ t
o
is the time inc ement chosen for the
me surement of the p r asiti c los es withou t
ty re, in second s;
I is the ty r e an w he l i nerti a i n r otation, i n
kil og ram metr es sq ared;
R
r
i s the ty r e r ol lin r ad iu s, in metr es;
V
po
is the ty r e ang ul ar v el ocity , u loa ded ty re, in
r adians p r secon
8.2 Roll ing r sis anc calc ulation
The net v al ues of d ri v in torque, spindl e for e,
p wer or deceler ation ar e to b conv er ted to roli ng
r esistance,F
r , ex pr es ed in newton s, usin the
a pr opri ate method, a ssh ow n in 8.2.1 to 8.2.4
8.2.1Fo c method at ty re spindle
The roll i g r esi sta nce, F
r , in newtons, is cal cula ted
w ith the eq a ti on:
F
r
= F
t [ 1 + (r
L /R )]
w her e
F
t
i s the ty r e spind l e for e, in newtons;
r
L
i s the d istance fr om the ty r e ax is to the dr um
outer sur face u nder stea dy -state cond i ti ons, in
metres;
R is the test dr um r ad iu s, in metres
8.2.2To que method at drum axis
The roll i ng r esi sta nce, F
r , in newtons, is cal cula ted
w ith the eq a ti on
w her e
Tis the i npu t torqu e, i n newton metr es;
R is the test dr um r ad iu s, in metres
8.2.3Power method at d rum axis
The roll i g r esi sta nce, F
r , in newtons, is cal cula ted
w ith the eq a ti on
w her e
Vis the electr ical p tential a pl ied to the
ma chi ne dr iv e, in v olts;
A is the electr ic curr ent d ra wn by the machi ne
d riv e, in a mp res;
U
n
i s th e test d rum v el oci ty , i n kiometr es p r
hour
8.2.4De eleration method
The roll i g r esi sta nce, F
r , in newtons, is cal cula ted
w ith the eq a ti on
w her e
I
D
is the test d rum inerti a in r otati on, in
kil og r am metr es sq a red;
R i s the test dr um sur face r ad iu s, in metr es;
ỷ t
v
i s the ti me i nc ement chosen for
me surement, in secon s;
V
v
i s the test dr um ang ular v eloci ty, lo ded ty r e,
i n r adi ans p r second ;
I i s the ty r e an whe l inerti a in r otation, in
kil og r am metr es sq a red;
F
r T
R
-=
F
r
3,6VìA
U
n
=
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