Before instructing the machine shop to remove material from the top of the block surface, I measured the 'actual' capacity of the combustion chamber in the cylinder head. This was previously original, and has only had a light skim (3 thou). 'The internet' says this should be 36cc, when in fact, its actually 33cc.
This then allowed for an actual calculation for static compression, considering I already know every other component spec.
Standard deck height is 210mm, mine was slightly under this already from previous skims, but to maximize the compression with the components I am going to be using I worked out it would be possible to drop the deck height to 209mm. All things considered, this will net an effective static compression ratio of 12.45:1 using a standard headgasket with enough clearance between piston and head. Stock compression ratio would normally be 10.2:1.
The machine shop removed the material, along with the boring/honing to suit the new pistons.
I am using 'Maxpeedingrods' connecting rods in this build, as they are well used and reviewed across the board now and offer ridiculous value in reality. In the mean time of the machine work being done I had torqued up the H-beam connecting rods to spec (with ARPs) and checked them for roundness. No issue with any of them, and all perfectly round, within 0.004mm. Some of the standard M54 rods were up to 0.030mm out of round!
The block was then collected...
Before beginning to assemble it I wanted to drill and tap an area near the oil pump chain, allowing me to use an oil pump chain tensioner from now on as they do not have one from factory. The chain runs fairly slack normally, and can generate strange vibrations if you push through to higher RPM. It may not be nessecary, but when the BMW part is only £12, I decided to do it for peace of mind this time.
To ensure the holes were drilled in the correct place (and square) I drew up and 3D printed a small jig based from the existing holes in the block, so I could bolt it on and drill through in one go.
After drilling for the tensioner, the whole block was scrubbed and jet washed to ensure any left over debris/dirt was removed. After drying with an airline the bores/surfaces were oiled.
This then allowed for an actual calculation for static compression, considering I already know every other component spec.
Standard deck height is 210mm, mine was slightly under this already from previous skims, but to maximize the compression with the components I am going to be using I worked out it would be possible to drop the deck height to 209mm. All things considered, this will net an effective static compression ratio of 12.45:1 using a standard headgasket with enough clearance between piston and head. Stock compression ratio would normally be 10.2:1.
The machine shop removed the material, along with the boring/honing to suit the new pistons.
I am using 'Maxpeedingrods' connecting rods in this build, as they are well used and reviewed across the board now and offer ridiculous value in reality. In the mean time of the machine work being done I had torqued up the H-beam connecting rods to spec (with ARPs) and checked them for roundness. No issue with any of them, and all perfectly round, within 0.004mm. Some of the standard M54 rods were up to 0.030mm out of round!
The block was then collected...
Before beginning to assemble it I wanted to drill and tap an area near the oil pump chain, allowing me to use an oil pump chain tensioner from now on as they do not have one from factory. The chain runs fairly slack normally, and can generate strange vibrations if you push through to higher RPM. It may not be nessecary, but when the BMW part is only £12, I decided to do it for peace of mind this time.
To ensure the holes were drilled in the correct place (and square) I drew up and 3D printed a small jig based from the existing holes in the block, so I could bolt it on and drill through in one go.
After drilling for the tensioner, the whole block was scrubbed and jet washed to ensure any left over debris/dirt was removed. After drying with an airline the bores/surfaces were oiled.