Sunday, 3 May 2026

KTT 581: Engine Rebuild – Part 2 – Completing the Build

The engine rebuild is now complete

and it looks a bit happier than when I first received it a bit over a year ago.

A few more details below of the top-end rebuild and final assembly.

The Cylinder Head

The bronze cylinder heads - part number K-1/6 - fitted to the Mk IV and V KTTs really are a work of art. This is the 2nd one that has come into my possession and when cleaned up and vapour blasted it could be mistaken for gold.


I had cleaned up the springs, the inlet valve and the other bits and pieces in the tumbler some time ago

and bought a new exhaust valve from G&S valves. However, the eagle-eyed might have spotted that there is one part missing in the last picture above, namely a top collar that holds the collets – only one was present in the parts that I had acquired.

Luckily, this is a straightforward component to make and so a new one was turned from a piece of O1 tool steel and heat treated. New one on the right in the pictures below.


For the record, the internal hole that supports the collets has a half-angle of 60 and although I have a carbide cutter of this angle it is more accurate and the surface finish is better if it is machined using a small boring bar.

New collets were fitted to both valves which were lightly ground before reassembling into the head.

With the valves in place, I could now measure the TDC combustion chamber volume and check the compression ratio,

The volume of oil required to fill the combustion chamber up to the bottom of the spark plug hole with the piston at TDC was found to be 57cc. With a bore and stroke of 74mm x 81mm this gives a compression ratio of 7.1:1.

As I mentioned in my last blog, I have used 2x paper gaskets to sandwich 2x shims between the base of the cylinder barrel and the crankcase (this engine did not have these when originally built – I believe that something such as shellac was used as a sealant). I estimate that, when compressed, the addition of these gaskets has added a volume of ~2cc to the TDC volume – ie without the gaskets the volume would be 55cc. This would give a compression ratio of 7.33:1.

The value quoted for the compression ratio of a Mk V KTT is 7.75:1 (see eg. Ivan Rhodes Passion of a Lifetime, page 265) and whilst I can account for a 0.2 difference I cannot see where another 0.4 of a ratio comes from …not that it really matters.

Cylinder Head Sealing

I am quite familiar with the fine/coarse grinding paste procedure for fitting iron heads onto iron barrels – see here, for example, which describes the process for the heads/barrels on the V-Twin. However, neither the bronze head nor the iron barrel on KTT 581 show any witness marks from applying such a method. Measurements of the height of the spigot on the barrel (0.370”) and the depth of the recess in the head (0.374”) indicate that either the head sealed directly onto the main top surface of the barrel or there was a very thin gasket (that disappeared long ago) between either the top of the spigot and the bottom of the head recess or the main flat surfaces of each component. I can find no mention of any cylinder head gasket in the Mk IV parts book, which has the same bronze head.

As measured, there is a 0.004” gap between the top of the spigot and the head recess. I decided that I would apply the seal to these surfaces using a very thin circular copper gasket. A quick search showed that I could get copper foil in a variety of thicknesses from 0.01mm to 1mm from a Chinese-based vendor on eBay. I ordered a 12cm x 1m long roll of 0.15mm (0.006”) thick foil and 2 ½ weeks later this arrived in the post.

It could have been packaged a bit better for its 6000-mile trip but there was plenty of unbent foil to use. It is not so easy to make a thin circular gasket from this material! I tried various combinations of scalpel, scissors, tin cutters, sharpened point of dividers and with both “as-received” (hard – combination of age and work hardened from the manufacturing process) and annealed pieces of the sheet but was unable to make a satisfactory gasket.

In the end, I clamped a small piece of the copper sheet to the rotary table and with a 1/8” diameter long end-mill used the milling machine to cut out the centre first

and then the outside.

This worked pretty well - the gasket was made much more accurately and it fits into the recess perfectly. After annealing, the head was fitted.

The Cambox

Although I had taken a brief look inside the cambox when I first received the engine, I had done nothing further with it until now. The 3 pictures below are of the “as-received” cambox.


As a restorer, this is exactly how I like to find parts – covered in oily grime and oily inside – because everything will have been preserved without deteriorating.

The cambox was stripped and all of the parts were cleaned.

A few observations:

The rockers have been highly polished.

There are aluminium quills in both the top cover

and the cover for the bevel drive

with 1mm diameter holes to provide oil to the cams and upper bevel gears.

A K-17/6 cam is fitted

 


and which shows little signs of wear. The rocker skids were also OK and were left in place.

The original SKF bearing on the oil pump end of the shaft was as-new and was refitted.

The oil pump assembly has 3x 0.008” brass shims (K-109/6 in the Mk IV parts list) which have been inserted to get the correct axial positioning of the pump relative to the end of the camshaft.

The cambox was reassembled with new felts to help keep the oil inside and was now ready to fit.

The cylinder head nuts/pillars on which the cambox is seated were missing and new ones were made, together with the cambox retaining bolts, using ETG 100 steel bar.

This is not a steel that I have ever used before and I don’t know if it is even available in the UK. A few lengths of this were given to me by a buddy from Sweden (Thank you Christer) and it turns out to be a high tensile steel with excellent machining characteristics and I have to agree that it is a very straightforward steel to machine.

The cylinder head nuts/cambox pillars were initially made around 0.050” longer than required to check that the cambox would “sit” on the 4 pillars without rocking (it does). The thickness of the washers beneath the nuts/pillars were checked to ensure they were exactly the same size. The nuts/pillars were then reduced in length to give an exhaust tappet clearance of 0.025”. The resulting inlet clearance was 0.015”. This is a few thou more than the recommended 0.020”/0.012” but I’ll leave it like this for the moment until the engine has run a while and settled down before resetting. The pillars all have the same dimension of 0.75” +/- 0.0005” and were chemically blacked prior to assembly.

The Bevel Drive

Now having the fasteners to actually bolt down the cambox it was time to set up the bevel drive. This has to be the last task because the distance between the upper and lower bevels depends on everything that has preceded – cylinder base gaskets, cylinder head gaskets, cambox mounting etc.

With all the main engine components bolted in place the vertical shaft (K-49/X) can be put in position without any Oldham couplings and the distance between the end of the shaft and the bottom bevel pinion (K-33) can be measured.

The screwdriver is simply to hold the shaft hard up against the upper bevel to enable the feeler gauge to be inserted. This dimension is to be filled by the flanges of both Oldham couplings + clearance.

Now, I seem to have acquired plenty of Oldham couples over the years

but I never seem to have ones with the flange thickness that I need. I also prefer to distribute the available space for the flanges as equally as possible rather than having one thick and one thin. As a consequence, I invariable end up making new ones and I now have an established process for this.

New Oldham couplings were machined in O1 tool steel to within a couple of thou on the milling machine

before finishing/fitting by hand with emery cloth,

coating with “KEEPBRYTE” anti-scale compound and heating to 8200C in the furnace,

oil quenching and tempering at 2600C

and cleaning up before final checking and fitting.

I checked the clearance of the vertical shaft again before final assembly and it was 0.012” - about the minimum acceptable value.

I have used the nitrile O-rings and PTFE rings that I described for building the engine of KTT 305 for sealing the cover for the vertical shaft (K-50/3).

It is important when fitting the vertical shaft that the positions of both the crankshaft and the cam are in the right places. If the crankshaft is positioned so that the piston is at TDC and the orientation of the slot in the lower bevel gear is aligned parallel to the axis of the bike (ie, orthogonal to the crankshaft – it might take a few rotations of the crankshaft to achieve this because of the hunting tooth) and the upper bevel slot has the same orientation (ie the slots are mirror images of each other) with both valves closed (which would correspond to TDC firing – again, a few rotations may be required) then the vertical shaft can be fitted in place.

After assembly and before tightening the gland nuts (K-52) the valve timing was checked. The “book” values for a Mk V engine with the K-17/6 cam (see Ivan Rhodes Passion of a Lifetime page 265) are:

IVO: 510 BTDC

IVC: 570 ATDC

EVO: 710 BBDC

EVC: 430 ATDC

and checked with a 0.012” valve/tappet clearance. I have made allowance for the checking clearance by using appropriate thickness feeler gauges but without physically changing the clearances with the resulting valve timings of:

IVO: 550 BTDC

IVC: 680 ATDC

EVO: 700 BBDC

EVC: 500 ATDC

These are in pretty reasonable agreement with the book values and I’m quite happy that the setup is good.

The gland nuts were tightened and it was now time to set up the ignition timing.

The BTH TT magneto has been overhauled as I mentioned in a previous blog and it has also been set up with a locked advance/retard, ie the timing is fixed. As it was like this when I received the engine, I assume this was done at the factory to avoid the possibility of either a broken cable messing up the timing or the timing being inadvertently retarded during the race. I have retained this setup and the timing has been set to 350 BTDC which should be an adequate level of advance without being over-advanced.   

Carburettor

The carb is a 1 1/16” 10 TT 34 AMAL instrument – 10 denotes the body size and 34 the year of manufacture. This is the correct (see Ivans book) and almost certainly the original carb for the bike

It was stripped in its entirety

to clean, check for any damage and to replace the fibre washers with new ones from AMAL

All the parts were in excellent condition however the main jet that was fitted was a #210 rather than a #360 that would have been fitted to a Mk V engine (see Ivans book). Now, I can imagine that some tuning/fettling on the dyno or the track could easily have resulted in a different jet size from a published value but this jet is too small for a 350cc engine and the difference is too great to be accounted for in this way.

A clue to the reason for the small main jet lies in the history of the bike. As I mentioned in a previous blog, Geoff Monty acquired the original complete bike around 1950 and used the chassis for a 250cc racer. And, guess what, a #210 main jet is perfect for the smaller capacity engine. So, my instinct is that the carb was “borrowed” for another, smaller engine and subsequently reunited with KTT 581 when Geoff sold it.

Anyway, I don’t have a #360 main jet in my stock of jets (I’ll get one when I next put in an order to AMAL) so have inserted a #380 in the meantime.

The last little job before completing the engine build was to strip and clean the 1:1 rev counter drive.

After repainting and repacking with fresh grease it was reattached to the engine.

And that concludes the engine rebuild. The engine is now on the bench and I’ll get back to this project later in the year when I have completed the final builds of both KTT 55, 305 and the DOHC 250.

A final couple of observations about this engine:

Having now seen the engine in its entirety, I can honestly say that I don’t believe it has done more than 500 miles in its life – practice laps plus the 7-lap Junior race (37.73 miles/lap) back in 1935. There is minimal wear for any of the major parts – crankshaft/big-end, small-end, piston-bore, cams and followers. It is also clear that this was built as a race engine judging by the amount of careful polishing of the con-rod and rockers.

From necessity I have had to replace a few bits – piston rings, make new cylinder head nuts/cambox bolts and Oldham couplings, replace a few 3/16” BSW screws and repair some damage to the piston that was caused by a careless stripper (that could be misinterpreted!) in the past. But to all intents and purposes the engine is pretty well exactly as it left the factory 91 years ago.





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