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Bsi bs au 050 1 6 7 1998 (iso 13327 1998)

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Tiêu đề Tyres and Wheels Part 1: Tyres — Section 6: Motorcycle Tyres — Subsection 6.7 Method of Test for Measuring Rolling Resistance
Trường học British Standards Institution
Chuyên ngành Standards
Thể loại British Standard
Năm xuất bản 1998
Thành phố London
Định dạng
Số trang 19
Dung lượng 1 MB

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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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50- 1- 6.7:1998

ISO

ICS 4 1 0; 8 1 0.1

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T 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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