Bullseye S480
Got my new turbo in yesturday and this thing is huge 80mm cold side and 1.32 hot with 96mm trim . Here are a few pics. Enjoy ! The turbo next to it is a PeakBoost A/R70 with a 1.00 hot side
http://img242.imageshack.us/img242/7784/imag0163dr7.jpg http://img149.imageshack.us/img149/8684/imag0165fd8.jpg http://img246.imageshack.us/img246/6992/imag0166wq6.jpg http://img237.imageshack.us/img237/5269/imag0167hr9.jpg |
Hi,
I have one myself. I think they are a great turbo They will outflow any equivalent sized turbo on the market They (S480) has 8 compressor blades as opposed to the Garrett 80mm comp wheel which has only 6 blades, that's ~25% more airflow!! They have extended tips so they hold more air flow and boost pressure You definately made a good choice there |
That's one big boy you got there! Did it get dropped on the turbine housing?
|
bad ass turbo.
|
Originally Posted by pmr eng
(Post 8734858)
Hi,
I have one myself. I think they are a great turbo They will outflow any equivalent sized turbo on the market They (S480) has 8 compressor blades as opposed to the Garrett 80mm comp wheel which has only 6 blades, that's ~25% more airflow!! They have extended tips so they hold more air flow and boost pressure You definately made a good choice there
Originally Posted by mono4lamar
(Post 8734928)
That's one big boy you got there! Did it get dropped on the turbine housing?
Originally Posted by Turbo Tech
(Post 8734931)
bad ass turbo.
|
Another Pic
|
Seems like everyone is going with this turbo nowadays... I can't wait to see what it can do. Not sure about the 2 extra blades giving 25% more airflow though... doesn't make sense to me.
|
did you go with the standard or race comp cover? i got a 475 with race cover. i cant wait to see this thing in action.
|
Originally Posted by pmr eng
(Post 8734858)
They (S480) has 8 compressor blades as opposed to the Garrett 80mm comp wheel which has only 6 blades, that's ~25% more airflow!!
-J |
Originally Posted by dregg100
(Post 8735678)
did you go with the standard or race comp cover? i got a 475 with race cover. i cant wait to see this thing in action.
|
i paid well under that. lol
|
Originally Posted by dregg100
(Post 8736870)
i paid well under that. lol
|
Originally Posted by dregg100
(Post 8735678)
did you go with the standard or race comp cover? i got a 475 with race cover. i cant wait to see this thing in action.
Originally Posted by Turbodriven
(Post 8736634)
That is a standard cover. Should have been around 800 bucks. You can get the BW480 with the race cover direct from BW (177287). They are only around 1000 or less from a diesel shop....
|
i am really thinking of going with this turbo myself, but i am wondering if i really need the s480, as apposed to the s475. If anybody is familiar with both of these, is there any noticable increase in spool time between the two?
|
Originally Posted by Chaotic_FC
(Post 8738118)
i am really thinking of going with this turbo myself, but i am wondering if i really need the s480, as apposed to the s475. If anybody is familiar with both of these, is there any noticable increase in spool time between the two?
|
Originally Posted by 13BT_Starlet
(Post 8738211)
What are you going to use for the street racing or drag racing only ? what makes your spool up laggier or quicker is your exhaust side thats what you need to consider for the quick spooling the cold side is the amount of air you want it produce.
-J |
well, a peripheral port s475 or s480 with a 1.32 turbine housing. i would be getting the new stlye race housing. the engine is already starting its build, but i have time to think about what turbo i am using.
|
Hello pmr , from what I hear of everyone I talk to that are running this the tell me nothing but good thing about them . You have yours up and running yet ? How it spools and poweband thru the rpm's ? This is strickly for drag racing can wait till all together up and running . I just finished my studies for the year, therefore have been busy with that and have done very little on engine I have bought some parts and planning to buy some more in the coming months My engine will be ready to start probably in a year or two It's hard for me to save up money as I work part time and have no time to work any extra hours because of my studying commitments Things are looking up though, I have 3.5 months free now, to work and make money, so I like to save up the money needed, to hopefully complete a large portion of what else is required on the engine The exhaust wheel and housing is quite large on the S480, therefore I'd probably go with a smaller diameter manifold piping if you're worried about spool |
Originally Posted by DelSlow
(Post 8735354)
Not sure about the 2 extra blades giving 25% more airflow though... doesn't make sense to me.
8 vs 6 blades, 2 blades difference = 25% |
Originally Posted by internal comsucktion engi
(Post 8735687)
It doesn't work that way my friend....
-J |
Originally Posted by pmr eng
(Post 8738538)
Yeah it does...
-J |
Originally Posted by internal comsucktion engi
(Post 8738566)
Oh Awsome..... Im having the CNC machine cut me a compressor wheel with 657 blades on it so I can make 38,964hp!!! Thank you for your help bud :icon_tup:
-J ~25% is pretty high but can we agree that the increase airflow will be quite signifiicant? |
Originally Posted by internal comsucktion engi
(Post 8738566)
Oh Awsome..... Im having the CNC machine cut me a compressor wheel with 657 blades on it so I can make 38,964hp!!! Thank you for your help bud :icon_tup:
-J |
Originally Posted by pmr eng
(Post 8738640)
Lol ok, without the airflow data (I can't find any S480 data) it would be hard to figure out the exact difference
~25% is pretty high but can we agree that the increase airflow will be quite signifiicant? -J |
Originally Posted by internal comsucktion engi
(Post 8738566)
Oh Awsome..... Im having the CNC machine cut me a compressor wheel with 657 blades on it so I can make 38,964hp!!! Thank you for your help bud :icon_tup:
-J There is no way in hell just adding additional compressor blades is going to linearly increase airflow like that. |
so does anybody know if there would be an noticeable increase in spool between the s475 and s480 in my application?
|
as far as i know they are identical turbos except the 480 has a 5mm bigger comp wheel. so a 480 would spool just a tad slower, but probably not enough to notice.
|
Originally Posted by dregg100
(Post 8739905)
as far as i know they are identical turbos except the 480 has a 5mm bigger comp wheel. so a 480 would spool just a tad slower, but probably not enough to notice.
|
Originally Posted by internal comsucktion engi
(Post 8738284)
Correction: A properly sized "exhaust side" can and will help with the "spool up". But it has more to do with the balance between the wheels.
I agree with you on the balance in between , I've seen ppl go with a good size A/R and the hot side small it spool at a really low rpm by mid rpm band it stop producing viseversa to big exhaust no low end only at top end of the rpm's -J
Originally Posted by Chaotic_FC
(Post 8740332)
it is a $200 difference, and i think that the s475 is enough for my application, but i am not sure.
|
Originally Posted by internal comsucktion engi
(Post 8738704)
I can't tell you the exact % of increase, but I will say that I'm sure I know why BW did it and IN THIS CASE it probably is more efficiant. But, just because a compressor has more blades doesn't make it better. In a lot of cases it makes it worse. It has to do more with the shape, pitch and angle of the blades and how they work together not only with one another but also with the housing/inlet.
-J Consider the BW 80mm comp wheel, if the blade had the same blade cross sectional area as the Garrett (80mm comp wheel) blade and the compressor wheels were rotating at the same speed the flow (from each blade) would be the same (if they both have the same inducer and exducer diameters). Therefore if additional blades were added the flow would increase (this is a fact). But, this all changes with the efficiency of the compressor wheel at the determined rotational speed. Increasing comp wheel rotation reduces efficiency! Changing the blade configurations (as you mentioned) may or may not increase efficiency (depends on the initial design, at what speed you want it to be most efficient). Additional blades reduce efficiency at higher rotational speeds. At some particular speed (most probably at lower rotational speeds, where there would have the greatest flow difference, to mid range speeds), the S480 comp wheel would have ~25% more flow because of the additional blades. If you don't believe me please speak to an engineer at garrett and they will tell you the same thing |
Originally Posted by dregg100
(Post 8739905)
as far as i know they are identical turbos except the 480 has a 5mm bigger comp wheel. so a 480 would spool just a tad slower, but probably not enough to notice.
|
Originally Posted by pmr eng
(Post 8740854)
Ultimately flow is governed by the cross sectional area of the blades (nothing else)
Consider the BW 80mm comp wheel, if the blade had the same blade cross sectional area as the Garrett (80mm comp wheel) blade and the compressor wheels were rotating at the same speed the flow (from each blade) would be the same (if they both have the same inducer and exducer diameters). Therefore if additional blades were added the flow would increase (this is a fact). But, this all changes with the efficiency of the compressor wheel at the determined rotational speed. Increasing comp wheel rotation reduces efficiency! Changing the blade configurations (as you mentioned) may or may not increase efficiency (depends on the initial design, at what speed you want it to be most efficient). Additional blades reduce efficiency at higher rotational speeds. At some particular speed (most probably at lower rotational speeds, where there would have the greatest flow difference, to mid range speeds), the S480 comp wheel would have ~25% more flow because of the additional blades. If you don't believe me please speak to an engineer at garrett and they will tell you the same thing Let me ask you this: At what comressor speed do the added blades make the unit "25%" more efficient? Are you running that boost level? Are you even going to be at the place in the comp. map that you'll benifit from this amazing "25%" gain? I highly doubt it. Also, "increasing comp wheel rotation" does NOT reduce efficiency. It does past a point but that statment can't be an absolute. Haha no need for me to call garrett bud, I know..... |
Originally Posted by internal comsucktion engi
(Post 8741098)
Let me ask you this: At what comressor speed do the added blades make the unit "25%" more efficient? Are you running that boost level? Are you even going to be at the place in the comp. map that you'll benifit from this amazing "25%" gain? I highly doubt it.
Also, "increasing comp wheel rotation" does NOT reduce efficiency. It does past a point but that statment can't be an absolute. Haha no need for me to call garrett bud, I know..... Have you ever seen a centrifugal belt driven supercharger and the amount of blades the impeller has? Well I can tell you they have alot >8 why, because their rotational speed is much less then a turbocharger http://www.turbobygarrett.com/turbob...pmap_large.gif Ok, see the speeds, 84000, 91000, 100000rpm and the efficiency, 79%-70% You can see an deduction in efficiency with an increase in speed |
Originally Posted by DelSlow
(Post 8739100)
+1
There is no way in hell just adding additional compressor blades is going to linearly increase airflow like that. blades. You see 2 or 3 usually. Also think @ a boat prop. I think the high speed boats use fewer blades, more for low end pull. I have no data and am just contemplating. Another thing that comes into play is pitch- I mean are the blades the same pitch on these two turbos?- unlikely. |
I agree, think about an airplane prop- if this is true, you would have 8 or 10 blades. You see 2 or 3 usually. Also think @ a boat prop. I think the high speed boats use fewer blades, more for low end pull. I have no data and am just contemplating. Another thing that comes into play is pitch- I mean are the blades the same pitch on these two turbos?- unlikely. |
Originally Posted by Xcentric
(Post 8741742)
I agree, think about an airplane prop- if this is true, you would have 8 or 10
blades. You see 2 or 3 usually. Also think @ a boat prop. I think the high speed boats use fewer blades, more for low end pull. I have no data and am just contemplating. Another thing that comes into play is pitch- I mean are the blades the same pitch on these two turbos?- unlikely. Must impellers are very similar in their configurations |
Originally Posted by pmr eng
(Post 8742846)
If you want to compare apples with oranges then what about the plane jet engine, have you seen how many blades they have?
Must impellers are very similar in their configurations |
Originally Posted by Xcentric
(Post 8743284)
Good point! I think a jet engine would be a better comparison and they do have alot of blades. Do we have any nasa engineers on this site to chime in?:Wconfused
Plain and simple answer is the more blades a comp wheel has and the thicker the blades, the less a wheel will flow. So a 6 blade versus a 8 blade wheel of the same design the 6 blade will outflow the 8 blade counterpart. Only thing is the 8 blade design will move the air sooner per 1 rev of the shaft up to a certain X shaft speed. Their is a reason why the Formula 1 turbos of the 80's ran 3 and 4 blade design and not 8-10 blades. They were limited to a certain inducer size and had to design a charger to move the most amount of air with that limited inducer size. The only problem with less blades, is that it will make a compressor map more narrow, but a formula 1 car operated at a very high rpm and narrow range during racing that the limited blade count did not effect driveability. |
^^^Take notes folks.....
-J |
Originally Posted by Turbodriven
(Post 8751836)
Plain and simple answer is the more blades a comp wheel has and the thicker the blades, the less a wheel will flow. So a 6 blade versus a 8 blade wheel of the same design the 6 blade will outflow the 8 blade counterpart.
Only thing is the 8 blade design will move the air sooner per 1 rev of the shaft up to a certain X shaft speed. Their is a reason why the Formula 1 turbos of the 80's ran 3 and 4 blade design and not 8-10 blades. They were limited to a certain inducer size and had to design a charger to move the most amount of air with that limited inducer size. The only problem with less blades, is that it will make a compressor map more narrow, but a formula 1 car operated at a very high rpm and narrow range during racing that the limited blade count did not effect driveability They never ran 3-4 blades (well I haven't seen any) The turbo F1 engines ran very high boost, they had 6-7 blades Here is the proof, http://blog.gtroc.com/dino/Honda-CH-159.jpg Honda 6 blades http://www.cimanet.co.uk/realhondaf1...987RA167E.jpeg http://doughy.theddrzone.com/bm1.jpg BMW 6 blades http://www.gurneyflap.com/Resources/DSCN4180a.jpg TAG- Porsche 7 blades http://www.gurneyflap.com/Resources/EngineZakspeed2.jpg For further F1 information check out this great site http://www.gurneyflap.com |
I have never found any tubo that have more compressor blades to outflow more than one with less in the same given dimension and that's not base on what I've read form the internet either. Actual testing at 50 to 70 psi most 7 blades fall short way below that and 8 blades are not even considered for that application.
It's well known fact to those who have actual experience that more blades equals more/broader airfow at lower than at higher speeds. More blades give a wider compressor map. |
Originally Posted by pmr eng
(Post 8753689)
A 8 blade compressor wheel will hold higher boost/pressure better than any 6 blade wheel period! Why because the additional blades hold the pressure better, not allowing the air to escape.
These wheels will not hold boost period. They are not airtight(or anything close to it for that matter). If they are generating pressure greater than the pressure present in the intake plenum(on the engine side of the compressor) then the boost is not leaking or going anywhere. Not to mention: more blades means more holes through which boost would "escape" (though not in any applicable anecdote). This is a very hard situation to explain but to put it simply: After a certain point additional blades will only screw themselves over. The more blades on the inducer the less opportunity each blade has to grab additional air due to the low pressure area created in the wake of the preceeding blade. More blades can only be smaller and thus cannot push the air with as much force as a wider blade. With fewer blades at any given RPM mother nature will have more time to erase the "vacuum" created by the preceeding blade. Thus there will be more air to grab and wider blades to push it harder than a design with more blades. This design fails to take advantage of a "low" rpm situation where air is abundant. |
more blades means more holes through which boost would "escape" Since the gap between each blade is larger with the 6 blade wheel, than there is a likely hood of greater chance for the air to escape with the 6 blade wheel? This is a very hard situation to explain but to put it simply: After a certain point additional blades will only screw themselves over. The more blades on the inducer the less opportunity each blade has to grab additional air due to the low pressure area created in the wake of the preceeding blade. More blades can only be smaller and thus cannot push the air with as much force as a wider blade. I mentioned that before With fewer blades at any given RPM mother nature will have more time to erase the "vacuum" created by the preceeding blade. Thus there will be more air to grab and wider blades to push it harder than a design with more blades. This design fails to take advantage of a "low" rpm situation where air is abundant. I agree the less blades are more efficient at higher speeds |
Originally Posted by crispeed
(Post 8755838)
I have never found any tubo that have more compressor blades to outflow more than one with less in the same given dimension and that's not base on what I've read form the internet either. Actual testing at 50 to 70 psi most 7 blades fall short way below that and 8 blades are not even considered for that application.
It's well known fact to those who have actual experience that more blades equals more/broader airfow at lower than at higher speeds. More blades give a wider compressor map. Your practical experience can't be questioned If that's the case then I take your word for it, that is if the inducer and exducer dimensions were the same The larger the difference between the inducer and exducer diameters, the greater the ability for the compressor wheel to hold more pressure more efficiently |
Originally Posted by crispeed
(Post 8755838)
I have never found any tubo that have more compressor blades to outflow more than one with less in the same given dimension and that's not base on what I've read form the internet either. Actual testing at 50 to 70 psi most 7 blades fall short way below that and 8 blades are not even considered for that application.
It's well known fact to those who have actual experience that more blades equals more/broader airfow at lower than at higher speeds. More blades give a wider compressor map. all the info i needed |
Originally Posted by pmr eng
(Post 8753689)
A 8 blade compressor wheel will hold higher boost/pressure better than any 6 blade wheel period! Why because the additional blades hold the pressure better, not allowing the air to escape. A 6 blade wheel may or may not outflow a 8 blades depends on the circumstances, comp wheel speed the biggest factor
I agree! You are wrong there! They never ran 3-4 blades (well I haven't seen any) The turbo F1 engines ran very high boost, they had 6-7 blades Here is the proof, http://blog.gtroc.com/dino/Honda-CH-159.jpg Honda 6 blades http://www.cimanet.co.uk/realhondaf1...987RA167E.jpeg http://doughy.theddrzone.com/bm1.jpg BMW 6 blades http://www.gurneyflap.com/Resources/DSCN4180a.jpg TAG- Porsche 7 blades http://www.gurneyflap.com/Resources/EngineZakspeed2.jpg For further F1 information check out this great site http://www.gurneyflap.com |
I don't know why ppl are concern about the wheel having 6 ,7 blades and the 8 blade this that . I dont see anything bad about the Borgwarner desing at all its been proven on many cars .
Here are some Dyno vids of car running the S480 ! http://www.grs-motorsports.com/notic...carolina/3.wmv http://www.grs-motorsports.com/notic...carolina/4.wmv http://www.grs-motorsports.com/notic...carolina/6.wmv http://www.grs-motorsports.com/notic...carolina/5.wmv |
Originally Posted by Turbodriven
(Post 8763619)
Check some of the turbos they used in qualifying trim (Keke Rossberg,Mansell and Piquet) and later banned to 6-7 blade design. Shortly after that turbos were then banned all together.
and I'd appreciate some new additions |
Originally Posted by 13BT_Starlet
(Post 8764315)
I don't know why ppl are concern about the wheel having 6 ,7 blades and the 8 blade this that . I dont see anything bad about the Borgwarner desing at all its been proven on many cars .
Here are some Dyno vids of car running the S480 ! http://www.grs-motorsports.com/notic...carolina/3.wmv http://www.grs-motorsports.com/notic...carolina/4.wmv http://www.grs-motorsports.com/notic...carolina/6.wmv http://www.grs-motorsports.com/notic...carolina/5.wmv For what I payed and the power I'm after, the turbo is more than adequate I will definately be looking to upgrade the turbo to a much larger one, when funds become available and I start chasing the need for more power I wish 13BT_Starlet all the best and success with his S480 8 blade turbocharger! |
All times are GMT -5. The time now is 02:15 AM. |
© 2024 MH Sub I, LLC dba Internet Brands