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Titanium connecting rods forged aluminum pistons
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the big end diameter is 2.225 the rod journal diameter is 2.100 the difference is the bearing look at clevite master bearing catalog (http://mahleclevite.com/pubs_detail.asp?c=1&id=24) go into the PDF file to the right on page 83 to the right it will say brg O.D. 2.2247-2.2252 and then you use a h series bearing from king bearing to go to the 2.0 rod journal of the stock 3.1L but you must mill the side of the rod down to the same thickness as the stock rod which is .843
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Your "standard" SBC has 2.2, 2.1, or 2.0, but there are aftermarket rod/crank combinations
Either way, the small journal big ends are an exact fit for the 660 (diameter, width has the be shaved).
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asfar as I am aware, the 350 only had 2.0 and 2.1 rod big ends. the 4.3 is the only motor i know of that has a 5.7 length rod and 2.25 main.
Please prove me wrong.
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the main girdle is set up for a Gen 2 but i will let you later next week i have a 2003 3400 block that i can check and make sure it works for you, i think it would work on any of that style blocks, and the 350 have two different sized big ends 2.100 and 2.250 just call a part supplier and they should be able to get the rods that you need
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where are you finding 350 rods that are 2.25 journal diameter on the big end?
as far as i know the 4.3 is the only engine that used this size other than the 3500, and the 4.3 big end is offset.
please elaborate.
also will your main girdle fit the gen3 3x00 engines?
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Ok, try this one then...
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Originally posted by bszopi View Post
Without putting too fine a point on it... as an aviation mechanic who flew in every plane (helicopter) he worked on in the military for post-mechanical work Test Flights as well as a SAR Crewman... understanding the basic principles of flight and the actions of fluid air on lift surfaces was crucial during Aviation Machinist School and while flying in and repairing these complicated machines. The author of that article would have you believe that when constricting an airway for an engine... or as he puts it ..."Like putting your finger on a garden hose..." that air pressure would INCREASE as a result of the Venturi shaping the air column. This is completely wrong.
The whole idea of any Venturi shaped intake passage is that by narrowing the inlet with a curve...the velocity of the air moving in the column entering the gradually narrowing tube will increase...but Bernouilli's Principle posits that the AIR PRESSURE within that moving column of air will DECREASE when passing over any curved surfaces...simply because the molecules of gas making up the atmospheric stream separate and thereby cause a substantial drop in air pressure.
You can prove this right now... right where you sit. Just take a sheet of paper 8.5" X 11" and tear off about a 1" strip... Now ...while holding one end of the strip between your index finger and thumb...allow the strip to drape over the back of your hand...Gravity will fold the strip over into a curve that in this case emulates either the curved surface of a wing structure...or in this example...the curvature of the inner surface of a Venturi Tube on an intake manifold.
Now if you slowly blow air over the surface of that strip of paper, you will gradually see the paper rise straight out in front of you. If the air comes too fast...it will cause turbulence on the trailing edge of the paper and it will flap up and down...like the stall of a wing with too much of an angle of attack on an air column. This phenomena is caused by and called the Differential Pressure between the normal room PSI around you of approximately 14.7 PSI... versus the reduction in the air pressure you have created by blowing a small column of air over the curved paper "wing".
The results of this simple experiment will prove my point. The real reason for the shape of a Venturi intake is so that the placement of the fuel vacuum in-port where fuel is taken in on a carburetor style engine will flow best at the point where the vacuum is the highest possible...because the partial vacuum present inside the Venturi chamber allows the normal air pressure present inside the fuel float chamber to push down on the fuel and force it into the intake via... Differential Pressure.
When it comes to learning anything new...I'm like Fox Mulder on "The X-Files"..."I want to believe..." But if I see something this egregiously wrong... I might have to challenge the source of this information. I'd better be right about what I have just suggested... because the millions of people who will fly around America in airplanes for this Thanksgiving Holiday...are counting on it!
Please know that my criticism is with the author of that entire article and that everyone should know that you are without fault in this situation. I'm glad to look at any other source of information on the Runner Length vs. Torque Topic if you can recommend them. I really want to know why this is true from someone who gets it right.Last edited by 60dgrzbelow0; 11-26-2009, 12:07 AM.
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Originally posted by 60dgrzbelow0 View Post...and why is it that "Long Runners" allow the engine to develop more torque?
Scroll down to the intake manifold section.
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...and why is it that "Long Runners" allow the engine to develop more torque?
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Originally posted by IsaacHayes View PostWould you hack up the existing one and weld up stuff to it? The LIM covers more than just the intake ports... coolant, valley, valve train... makes it more of a PITA to make one from scratch..
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We will be building a custom lower for the Mustang project. It will all be designed in CAD, therefore all the parts will be able to be replicated at a later date. This will potentially allow for much more options for the 3x00 engines.
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Would you hack up the existing one and weld up stuff to it? The LIM covers more than just the intake ports... coolant, valley, valve train... makes it more of a PITA to make one from scratch..
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Not hard to build a decent flowing LIM. All in how you want it too look though. I scrapped my g2 lim plans so no more of that.
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Yeah the lower intake is going to bottle neck your ported heads...
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