Home > AEM > Infinity EMS > AEM Infinity Quick Start Guide NA

AEM Infinity Quick Start Guide NA

    Download as PDF Print this page Share this page

    Have a look at the manual AEM Infinity Quick Start Guide NA online for free. It’s possible to download the document as PDF or print. UserManuals.tech offer 223 AEM manuals and user’s guides for free. Share the user manual or guide on Facebook, Twitter or Google+.

    							Tunin g G uid e
    38
    © 2 015 A EM  P erfo rm ance E le ctr o nic s
    P rim ary  In je cto r F lo w  S ele ctio n
    T his  d ata base a llo w s th e u ser to  s ele ct p ro per p rim ary  in je cto r flo w  d ata . 
    I n jF lo w Rate  [c c/s ec], 1 -A xis  lo okup ta ble  o f  flo w  v s  in je cto r p re ssure .
    I n jO ffs et [u s/1 0], 2 -A xis  lo okup ta ble  o f  P W  o ffs et v s  b atte ry  v o lt a ge a nd in je cto r p re ssure
    S eco ndary  In je cto r F lo w  S ele ctio n
    I f  S econdary  In je cto rs  w ere  s ele cte d in  th e In je cto r S etu p W iz ard , th is  S econdary  In je cto r F lo w  S ele ctio n d ata base
    w ill  b e e nable d. T his  a llo w s th e u ser to  s ele ct p ro per s econdary  in je cto r flo w  d ata .
    I n jS ecF lo w Rate  [c c/s ec], 1 -A xis  lo okup ta ble  o f  flo w  v s  in je cto r p re ssure .
    I n jS ecO ffs et [u s/1 0], 2 -A xis  lo okup ta ble  o f  P W  o ffs et v s  b atte ry  v o lt a ge a nd in je cto r p re ssure 
    						
    							39
    © 2 015 A EM  P erfo rm ance E le ctr o nic s
    I
    n fin ity  Q uic k S ta rt G uid e
    N O TE : If  th e S etu p W iz ard  d oes n ot c onta in  y our s pecific  fu el  in je cto r ty pe, y ou c an m odify  th e In jF lo w Rate  ta ble
    m anually . If  y ou d o n ot k now  th e d iffe re nt flo w  ra te s a t d iffe re nt fu el  p re ssure s, c hoose a  flo w  ra te  (b ased o n
    M anufa ctu re rs  s pecs) a t a  k now n p re ssure  a nd p opula te  th e e ntir e  ro w  w it h  th at v a lu e. F or e xam ple , y ou h ave  a
    f u el  in je cto r th at is  n ot lis te d in  th e W iz ard  S ele ctio n. Y ou k now  th at it  flo w s 4 75 c c/m in  a t 4 5 p si.  S ele ct th e c ells
    i n  th e u pper ro w  o f  th e In jF lo w Rate  [c c/m in ] ta ble  a nd m anually  in put 4 75. T his  w ill  s uffic e to  g et th e c ar u p a nd
    r u nnin g, th ough p ro per flo w  d ata  is  id eal.
                
           
                      
    Set T hro ttle  R ange
    T he w iz a rd  d is p la ys a  w arn in g m essa ge to  th e u se r if th e s o ftw are  is  n ot c o nnecte d to  a  h ard w are
    t a rg et.
    L iv e  T P S V olts
    T ext a nd g ra phic al  re pre senta tio n o f  th e ra w  a nalo g v o lt a ge is  s how n. 
    						
    							Tunin g G uid e
    40
    © 2 015 A EM  P erfo rm ance E le ctr o nic s
    S te ps
    S et T P S V olts  M in
    P re ss th is  b utto n w hen th e th ro ttle  p edal  is  fu lly  re le ased. T his  w ill  w rit e  th e c urre nt v a lu e o f  A nalo g7 [V ] to
    t h e T hro ttle _ra w  [% ] A nalo g In  c ondit io ner a nd d is pla y th e re sult a nt v a lu e o n th e T P S M in  V olt s : X .X X
    d is pla y.
    S et T P S V olts  M ax
    P re ss th is  b utto n a ft e r th e th ro ttle  p edal  is  fu lly  d epre sses. T his  w ill  w rit e  th e c urre nt v a lu e o f  A nalo g7 [V ] to
    t h e T hro ttle _ra w  [% ] A nalo g In  c ondit io ner a nd d is pla y th e re sult a nt v a lu e o n th e T P S M ax V olt s : X .X X
    d is pla y.
    Ig nitio n S yn c
    T he e ngin es  ig nit io n tim in g m ust b e s ynchro niz ed w it h  th e In fin it y  T uners  ig nit io n tim in g d is pla y. T his  is  c ru cia l
    w it h  o ld er v e hic le s th at h ave  a dju sta ble  d is trib uto rs , a dju sta ble  c am  a ngle  s ensors , e tc . M ost m odern  e ngin es d o
    n ot u tiliz e a  m anual  a dju stm ent fo r ig nit io n tim in g. H ow eve r, th is  w iz ard  s hould  a lw ays b e u sed fo r v e rific atio n a s
    s ensors  c an b e fr e quently  in sta lle d b ackw ard s o r u psid e d ow n. T his  c an c atc h a  p ro ble m  b efo re  d am age o ccurs .
    N ote : T his  w iz a rd  c a n o nly  b e u se d w hen th e e ngin e s p eed is  g re ate r th an 5 0 R PM .  T he ig nitio n tim in g
    w ill a uto m atic a lly  u nlo ck w hen th e w in dow  is  c lo se d r e ve rtin g b ack to  th e n orm al c a lc u la te d v a lu e.  
    						
    							41
    © 2 015 A EM  P erfo rm ance E le ctr o nic s
    I
    n fin ity  Q uic k S ta rt G uid e
    I g nitio n T im in g
    F or s ynchro niz in g, th e ig nit io n tim in g c an b e lo cked b y c heckin g th e b ox. 
    A llo w able  v a lu es: M in  v a lu e =  0 , M ax v a lu e =  4 5
    S yn c A dju stm ent
    T he w in dow  in clu des 4  b utto ns. T w o b utto ns a re  u sed to  A dva nce T im in g a nd T W O b utto ns a re  u sed to
    R eta rd  T im in g.
    T he b utto n la bele d L arg e e dit s  th e C am SyncA dju stm ent T rig O ffs et [d egB TD C] c hannel  in  1 .0  d eg s te ps. T he
    r a nge is  0  to  7 19 d egre es. T he b utto n la bele d S m all  e dit s  th e T rig O ffs et [d egB TD C] c hannel  in  0 .1  d eg
    s te ps. 
    T he T rig O ffs et [d egB TD C] is  a dju sta ble  b y R esolu tio n. T he R esolu tio n s ettin g h as a  ra nge o f  0 .2 5 d eg to  2 .0
    d egre es in  0 .2 5 d egre e in cre m ents . T his  “s te ppin g” fu nctio n a llo w s th e u ser to  m ake T rig O ffs et [d egB TD C]
    a dju stm ents  w it h  th e S m all  b utto n u p to  th e ra nge lim it .
    A dva nce d S etu p
    P ic ku p s e nso r d ela y
    T he M ore  a nd L ess b utto ns in cre ase/d ecre ase th e S pkD ela yC om p [u s] v a lu e in  in cre m ents /d ecre m ents  o f
    5 . 
    M in  v a lu e =  0 , M ax v a lu e =  5 00
    T w o s epara te  p ro cedure s a re  re quir e d d ependin g o n th e In fin it y  a pplic atio n: P lu g a nd P la y o r U niv e rs al  A pplic atio n.
    P lu g a nd P la y
    a . In  th e Ig nit io n S ync w iz ard , s ele ct th e c heckbox “L ock ig nit io n tim in g a t” a nd s et th e “d egre es B TD C” (1 0.0  d eg
    B TD C is  th e d efa ult ). 
    b . Sta rt th e e ngin e a nd u se a  tim in g lig ht to  v e rify  th at th e c ra nkshaft  tim in g m atc hes th e lo cked ig nit io n tim in g
    s et p oin t (1 0.0  d eg B TD C if  u sin g th e d efa ult  s ettin g). 
    c . If  th ere  is  a  d evia tio n b etw een th e lo cked s et p oin t a nd th e a ctu al  tim in g o bserv e d w it h  th e tim in g lig ht, u se th e
    S ync A dju stm ent a rro w s to  m atc h th e w iz ard -d is pla yed v a lu e w it h  th e a ctu al  v a lu e. A s th e S ync A dju stm ent
    a rro w s a re  a dva nced o r re ta rd ed, th e tim in g o bserv e d o n th e c ra nkshaft  w ill  c hange, w hile  th e “L ock ig nit io n
    t im in g a t 1 0.0  d egre es B TD C” w ill  re m ain  c onsta nt.
    U niv e rs a l A pplic a tio n
    a . In  th e Ig nit io n S ync w iz ard , s ele ct th e c heckbox “L ock ig nit io n tim in g a t” a nd s et th e “d egre es B TD C” (1 0.0  d eg
    B TD C is  th e d efa ult ). 
    b . Do N O T a tte m pt to  s ta rt th e e ngin e. D is able  (u nplu g) th e fu el  in je cto rs  a nd/o r fu el  p um p. 
    c . While  c ra nkin g th e e ngin e, u se a  tim in g lig ht to  v e rify  th at th e c ra nkshaft  tim in g m atc hes th e lo cked ig nit io n
    t im in g s et p oin t (1 0.0  d eg B TD C if  u sin g th e d efa ult  s ettin g). 
    d . If  th ere  is  a  d evia tio n b etw een th e lo cked s et p oin t a nd th e a ctu al  tim in g o bserv e d w it h  th e tim in g lig ht, u se th e
    S ync A dju stm ent a rro w s to  m atc h th e w iz ard -d is pla yed v a lu e w it h  th e a ctu al  v a lu e. A s th e S ync A dju stm ent
    a rro w s a re  a dva nced o r re ta rd ed, th e tim in g o bserv e d o n th e c ra nkshaft  w ill  c hange, w hile  th e “L ock ig nit io n
    t im in g a t 1 0.0  d egre es B TD C” w ill  re m ain  c onsta nt.
    e . Reconnect th e fu el  in je cto rs  a nd fu el  p um p.
    f . Once th e re m ain in g S etu p W iz ard s h ave  b een c onfig ure d, re peat th e Ig nit io n S ync p ro cess w it h  th e e ngin e
    r u nnin g to  e nsure  th at th e c ra nkshaft  tim in g m atc hes th e lo cked ig nit io n tim in g s et p oin t. 
    						
    							Tunin g G uid e
    42
    © 2 015 A EM  P erfo rm ance E le ctr o nic s
    M
    odifie d V alu es
    C alib ra tio n ta ble  c hanges th at h ave nt  b een c om mit te d to  fla sh m em ory  a re  h ig hlig hte d a s s how n b elo w . C ondit io ns
    t h at w ill  re set th e d is pla y a re  a s fo llo w s:
    1 . M anually  c om mit tin g c hanges th ro ugh th e T arg et >  C om mit  m odific atio ns m enu c om mand
    2 . M anually  c om mit tin g c hanges u sin g th e h ot k ey c om bin atio n [C trl  S hift  C ]
    3 . O penin g a nd c lo sin g th e S etu p W iz ard .  N ote  th e S etu p W iz ard  a uto m atic ally  c om mit s  A LL c hanges to  m em ory
    e ve ry  tim e it  is  c lo sed.
    4 . T urn in g th e ig nit io n s w it c h o ff  w hen th e tu nin g p re fe re nce K ey O ff  C om mit  is  s ele cte d      
    						
    							43
    © 2 015 A EM  P erfo rm ance E le ctr o nic s
    I
    n fin ity  Q uic k S ta rt G uid e
    R ig ht C lic k E ditin g
    T o u se th e rig ht c lic k m enu fo r e dit in g ta ble  v a lu es, s ele ct a  p ortio n o f  th e ta ble  a nd rig ht c lic k.  C hoose fr o m
    a va ila ble  o ptio ns.
    VE &  A ir flo w  B ase d T unin g
    T he In fin it y  E CU u ses s ig nific antly  d iffe re nt m eth ods o f  c alc ula tin g th e fu el  d eliv e ry  re quir e m ents  a nd o utp uts  th an
    p re vio us A EM  p ro ducts . 
    M easure d d ata  fr o m  s ensors , i. e ., M anifo ld  A bsolu te  P re ssure  (M AP [k P a]), A ir  T em pera tu re , C oola nt
    T em pera tu re , a nd E ngin e R PM , a re  a cquir e d. T he E CU u ses th is  s ensor d ata  in  c om bin atio n w it h  V olu m etric
    E ffic ie ncy (V E% ) to  e stim ate  a ir flo w . 
    T he V olu m etric  E ffic ie ncy is  a  p erc enta ge o f  a ir  a nd fu el  th at a ctu ally  e nte rs  th e c ylin der d urin g in ductio n re la tiv e  to
    t h e v o lu m etric  c apacit y  (ra te d d is pla cem ent) o f  th e c ylin der u nder s ta tic  c ondit io ns. T he V E lo okup ta ble  is  a  2 -a xis
    l o okup ta ble , w it h  lo ad v a lu es (ty pic ally  M AP [k P a]) v e rs us E ngin e R PM . In  e ach ta ble  c ell,  th e E ngin e R PM
    c orre sponds w it h  a  s pecific  M AP [k P a], a nd a  V olu m etric  E ffic ie ncy is  d efin ed fo r th at c ell.   
    						
    							Tunin g G uid e
    44
    © 2 015 A EM  P erfo rm ance E le ctr o nic s
    T he V olu m etric  E ffic ie ncy is  c om bin ed w it h  te m pera tu re  s ensor d ata  to  e stim ate  a  c om pensate d M ass A ir flo w . T he
    C harg eTem pB le nd ta ble  d ic ta te s w hat ra tio  o f  a ir  te m pera tu re  to  c oola nt te m pera tu re  is  u sed a t s pecific  E ngin e
    R PM  to  a dju st th e d ensit y  o f  th e in ducte d a ir . A  h ig her n um ber g iv e s p rio rit y  to  C oola nt T em pera tu re , a nd is  s een
    a t lo w er E ngin e R PM .
    O nce M ass A ir flo w  h as b een c alc ula te d u sin g th e ta ble s a bove , th e In fin it y  E CU w ill  lo ok u p th e T arg et L am bda
    ( A FR ) a nd th en c alc ula te  th e fu el  re quir e m ents . T arg et A FR  w ill  b e u sed a s a  m ain  p ara m ete r in  d ete rm in in g fu el
    i n je cto r flo w  ra te . T he L am bdaTarg etT able  (b elo w  L eft ) a nd A FR  T arg et T able  c onve rs io n ta ble  (b elo w  R ig ht) w ill
    h ave  d efa ult  v a lu es. B ased o n th e c alc ula te d M ass A ir flo w , th e In fin it y  E CU w ill  a tte m pt to  a dd e nough fu el  to  h it
    t h e ta rg et A FR . 
    N ote : T he c alc ula te d L am bdaTarg et in flu ences th e fu el  d eliv e re d to  th e e ngin e a t a ll  tim es, e ve n w hen c lo sed-lo op
    0 2 fe edback is  d is able d. 
      
    						
    							45
    © 2 015 A EM  P erfo rm ance E le ctr o nic s
    I
    n fin ity  Q uic k S ta rt G uid e
            
    T he s uggeste d tu nin g m eth od is  to  s et th e A FR  u sin g th e L am bdaTarg etT able  o r A FR  T arg et T able  to  a  v a lu e s afe
    a nd s uit a ble  fo r th e e ngin e. F or n orm ally  a spir a te d e ngin es a  v a lu e o f  1 3.0 :1  o r 0 .8 87 la m bda is  u sually  s uffic ie nt a t
    a ll  o pera tin g c ondit io ns. F or b ooste d a pplic atio ns, th e o pera tin g c ondit io ns d ic ta te  a  s afe  A FR . P le ase c onsult  a
    t u ner k now le dgeable  in  y our e ngin e’s  re quir e m ents  fo r h elp . O nce th e ta rg et la m bda (A FR ) v a lu es a re  c hosen, ru n
    t h e e ngin e a t a s m any o pera tin g c ondit io ns a s p ossib le  a nd a dju st th e V E T able  to  re ach th e A FR  T arg et T able
    v a lu es. O nce th e V E T able  h as b een tu ned to  a ccura te ly  re ach th e A FR  T arg et T able  v a lu es a t a ll  o pera tin g
    r a nges, th en y ou c an c hange th e A FR  T arg et T able  to  u se d iffe re nt A FR  s ettin gs la te r. N eve r a dju st V ETable  to  ru n
    a  d iffe re nt A FR , o nly  to  a chie ve  th e L am bdaTarg et v a lu e.
    T he In je cto r F lo w ra te  is  v e ry  im porta nt in  d ete rm in in g th e fu el  re quir e m ents . T he In fin it y  E CU u ses a ctu al  In je cto r
    F lo w ra te  [c c/m in ] to  d ete rm in e th e p ro per in je cto r p uls e w id th . T he In jF lo w Rate  [c c/m in ] ta ble  is  c alib ra te d fr o m  th e
    S etu p W iz ard : In je cto r F lo w , h ow eve r th e ta ble  c an b e m odifie d m anually  fo r u nlis te d in je cto rs .  
    						
    							Tunin g G uid e
    46
    © 2 015 A EM  P erfo rm ance E le ctr o nic s
    N ow  th at th e b ase in je cto r flo w  ra te  h as b een d ete rm in ed, th e In fin it y  E CU a pplie s a  fe w  m ore  c om pensatin g
    f a cto rs . W all  W ettin g is  a  fu nctio n o f  fu el  c ondensin g in  th e in ta ke m anifo ld  a t th e in je ctio n p oin t. A t d iffe re nt ra te s
    o f  c hange in  th e M AP [k P a] v a lu es, a nd a t d iffe re nt C oola nt T em pera tu re s, fu el  e nric hm ent c om pensatio ns a re
    u sed to  p re ve nt le an a nd ric h c ondit io ns d urin g ra pid  m anifo ld  p re ssure  c hanges. N ote  th at th is  ta ble  h as s eve ra l
    d iffe re nt fu nctio ns. It  c an b e u sed fo r d ynam ic  tra nsie nts  b y n atu re  o f  it s  “M AP R ate ” x -a xis . It  c an a ls o b e u sed fo r
    m ore  s te ady s ta te  c om pensatio ns b y a dju stin g th e v a lu es in  th e “m id dle  b and” o f  th e ta ble  w here  M AP ra te
    c hanges a re  v e ry  s m all.   P osit iv e  n um bers  in  th is  ta ble  w ill  e ffe ctiv e ly  a dd fu el  to  e nric hen th e m ix tu re . N egativ e
    n um bers  h ave  th e o pposit e  e ffe ct.    
    T he X  a nd Y  a xis  in puts  o f  th e W allW ettin g ta ble  c an b e s et to  s eve ra l  d iffe re nt v a ria ble s. T hese s ettin gs a re  fo und
    i n  th e S etu p W iz ard  p age fo r A ccel  a nd D ecel  F uel.  A xis  s ele ctio ns in clu de:
    M ap R ate
    T hro ttle  R ate
    C oola nt T em p
    M AP [k P a]
    E ngin eS peed [R PM ]
    D BW _A PP R ate 
    						
    							47
    © 2 015 A EM  P erfo rm ance E le ctr o nic s
    I
    n fin ity  Q uic k S ta rt G uid e
    L am daA fte rS ta rtT rim  is  a  2 -a xis  ta ble  th at is  u sed to  m odify  th e L am bda (A FR ) fo r s pecifie d tim e a ft e r s ta rtin g
    t h e e ngin e. T his  ta ble  a dds a  la m bda o ffs et fo r a  s m all  p erio d o f  tim e a ft e r th e e ngin e is  s ta rte d. B y a llo w in g a
    s lig htly  ric her m ix tu re  ta rg et, it  w ill  k eep th e e ngin e fr o m  s ta llin g o r ru nnin g ro ugh im media te ly  a ft e r s ta rtin g a nd th e
    l a m bda c orre ctio n to  a  m in im um . T he la st c olu m n s hould  b e p opula te d w it h  “0 ” trim  a t o pera tin g te m pera tu re s to
    p re ve nt a  c ontin uous la m bda o ffs et.
    Targ et L am bda
    T o c ontro l  th e e ngin es  fu el  d eliv e ry  s yste m , th e In fin it y  c an b e p ro gra m med to  ru n o pen lo op a nd/o r c lo sed lo op O 2
    f e edback. C lo sed lo op u ses fe edback fr o m  th e o xygen s ensor to  m ake te m pora ry , b ut im media te , c orre ctio ns to
    t h e in je ctio n to  m ain ta in  a  ta rg et a ir  fu el  ra tio  (A FR ) o r la m bda. T he ty pe o f  th e O 2 s ensor w ill  d ete rm in e h ow
    l a m bda ta rg et c an b e c ontro lle d. D ue to  th e n atu re  o f  s ta ndard  n arro w  b and O 2 s ensors , th e o nly  a ccura te
    m easure m ent th at c an b e m ain ta in ed in  c lo sed lo op is  L am bda 1 .0 . H ow eve r, w id eband O 2 s ensors  c an b e u sed in
    a lm ost e ve ry  fe edback c ondit io n.  
    						
    All AEM manuals Comments (0)

    Related Manuals for AEM Infinity Quick Start Guide NA