- Joined
- Apr 22, 2020
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Many birds of a feather are present here.The money I have burned bringing my commando up to an early 80s average bike specs is unbelievable
Many birds of a feather are present here.The money I have burned bringing my commando up to an early 80s average bike specs is unbelievable
From talking to someone who built a couple of featherlastics a while ago, I learnt that the issue of the rear wheel yanking the powertrain backwards in the frame (when the rear wheel is NOT also isolated) is a real issue and not one that’s easily resolved.After reading through a lot of this info I'll be maybe considering incorporating ISOs into frame
I don't know if there's enough room yet but it's only metal!
My only concern would be not having the swing arm attached to the engine/gearbox cradle the chain alignment
IE the motor trying to tear itself backwards and to the left
The chain would become slack
Could probably solve this with some links /rose joints at the expense of some vibration
The reason I moved away from triumph twins was the sheer amount of vibration I find a triumph t140 intolerable after riding a commando for example
I should be picking my new project up this week so I shall have a measure up to see if ISOs are possible
I'm also wondering if the ISOs only really work well with the swinging transmitting the vibes away through the wheel,tyre , using the road as a damper?
Anyone have any experience of running a commando on its ISOs in a different frame without the swinging arm fitted?
I disagree on the "bearing" theory here. Mounting plates are only properly installed when the studs and nuts are properly torqued to bring them into intimate unmoving contact with the cases they're bolted to. It's the friction between the surfaces, amplified by the normal force of the torqued fasteners, that is the bearing, not the radial forces inside in the holes. If the fasteners come loose, of course tighter diametrical clearances provide a better last resort, but that is past the point of failure of the engineered design.(bolt holes are considered to be "bearings" for the bolts), thus plate thickness have to be substantially increased over steel plates. Thereby some or all of the weight advantage is lost. AMC increased alloy plates for the P11, but not enough. Used engine plates usually exhibit ovalized holes. Another drawback is compressibility due to the low Young's modulus. Engine/frame bolts will come loose much sooner than when using steel plates. Loose bolts amplify bearing wear of course.
- Knut
Yes - now there are lightweight pistons for stock rods (lighter than stock pistons). This is a recent development. But they are not as light as the pistons for longer rods.20 years ago Ken Armann balanced my Atlas crank to 65%, do not know if that was wet or dry. It runs very well in town or at freeway speeds. I rarely take it over 5000 rpm and it is very good to ride. Single 34 Mikuni and a Boyer.
It was balanced for 10-1 forged pistons which were very heavy lumps. I could never stop it from pinging so I went back to stock Commando pistons. To keep the balance It was necessary to have heavier wrist pins made. This arrangement worked very well. However, during the 20 years the heavy wrist pins got lost and I had to use the stock Commando pins. I noticed a slight difference for the worse though it is still very rideable. JS claims a key factor is reducing reciprocating weight and I discovered RGM has tapered wrist pins which are lighter than the stock ones. Also very inexpensive. My plan this winter when the weather gets bad is to have the crank rebalanced using the RGM pins. I REALLY WISH there were lightweight pistons ( just like the JS pistons ) I could use in a stock motor. Comstock has recommended MARINE CRANKSHAFT in southern California.
To sum up, before balancing, the Atlas was a vicious shaker. Balancing really tamed it.
The stock rods are very light.Yes - now there are lightweight pistons for stock rods (lighter than stock pistons). This is a recent development. But they are not as light as the pistons for longer rods.
As a Principal and Chief Stress Engineer (long since retired) in the Aviation industry I have to rule in favour of mdt-son on the issue of bolts taking the bearing (and shear also) loads in bolted joint. Whilst there is undoubtedly a friction force between the clamped faces of a bolted joint, it is never included in the joint analysis. If the bearing area of the bolt is too small, then one uses more bolts, a larger bolt, stronger material, or incorporates a hollow dowel into the joint. The friction clamping force is only ever a guess and cannot be assumed to remain constant during the service life of the component, factors which the Aviation Authorities find quite unacceptable for use in service life calculations.I disagree on the "bearing" theory here. Mounting plates are only properly installed when the studs and nuts are properly torqued to bring them into intimate unmoving contact with the cases they're bolted to. It's the friction between the surfaces, amplified by the normal force of the torqued fasteners, that is the bearing, not the radial forces inside in the holes. If the fasteners come loose, of course tighter diametrical clearances provide a better last resort, but that is past the point of failure of the engineered design.
The mounting plates are shear joints with rather generous clearance to accommodate tolerance build-up and to allow easy assembly and disassembly. If the joint were to rely on the stud to hole fit, and not friction from clamping force, then every mount on a motorcycle would be rapidly progressing towards failure from first use. I don't see any need for constant friction at the plate to case interface, just that the clamping force be maintained sufficiently for it to be above the minimum required to prevent relative movement in use. If the stud in a shear joint is receiving shear force instead of only tensile force, then the joint is already failing. As stated here: https://www.theautopian.com/a-suspe...ratcheting-agony-goes-into-fighting-friction/As a Principal and Chief Stress Engineer (long since retired) in the Aviation industry I have to rule in favour of mdt-son on the issue of bolts taking the bearing (and shear also) loads in bolted joint. Whilst there is undoubtedly a friction force between the clamped faces of a bolted joint, it is never included in the joint analysis. If the bearing area of the bolt is too small, then one uses more bolts, a larger bolt, stronger material, or incorporates a hollow dowel into the joint. The friction clamping force is only ever a guess and cannot be assumed to remain constant during the service life of the component, factors which the Aviation Authorities find quite unacceptable for use in service life calculations.
Friction provides an additional load transfer (in addition to bolt bearing) between overlapping plates when there are many bolts or rivets, this is called a bolt group. The prerequisite is metal to metal contact over a large area. See for example old truss bridges, the Eifel tower, etc. These conditions are not fulfilled for engine plates. Sorry, but no text book will back up your theory.I disagree on the "bearing" theory here. Mounting plates are only properly installed when the studs and nuts are properly torqued to bring them into intimate unmoving contact with the cases they're bolted to. It's the friction between the surfaces, amplified by the normal force of the torqued fasteners, that is the bearing, not the radial forces inside in the holes. If the fasteners come loose, of course tighter diametrical clearances provide a better last resort, but that is past the point of failure of the engineered design.
And there is the trade off.....stock rods are light, steel Carrillo rods are not. Standard pattern Carrillo rods with bushes are very heavy, JSM Carrillo rods are longer but lighter, particular at the bushless small end, but you get less choice of piston sources.The stock rods are very light.
We read the story of a grenaded engine a few days ago. No inspection report yet, but it appears the timing side rod has ruptured.And there is the trade off.....stock rods are light, steel Carrillo rods are not. Standard pattern Carrillo rods with bushes are very heavy, JSM Carrillo rods are longer but lighter, particular at the bushless small end, but you get less choice of piston sources.
Pay's your money and takes your choice. I chose JSM long short stroke rods and pistons. Empirically, I think it contributes greatly to reduced vibration.
I can see that JSM pistons on stock rods might suit a primarily road use motor, and would cost most people, who already have rods they want to re-use, much less.
I wouldn't do it in a race motor, but it's personal choice. I raced 4 seasons with the same set of standard 1975 rods in a high spec 850 with no issues. They aren't bad rods but will ultimately have a shorter life than Carrillo rods.
Yes they are.The stock rods are very light.
Before I became a stress engineer, I spent many years in the WHL structural test dep't. doing static and fatigue tests on helicopter components. There was no non destructive method to determine how near an aluminium item was to fatigue failure. I doubt that one exists today. Certainly not one that wouldn't cost far more than the value of the bike.We read the story of a grenaded engine a few days ago. No inspection report yet, but it appears the timing side rod has ruptured.
My question is therefore, is there a way to assess the fatigue condition of RR aluminium rods when an engine is dismantled?
In theory, there should be a length deviation between new and "as is". Maybe fatigue life (D = 0 ....1) can be assessed by this deviation? Will radiography provide a reliable answer?
I am just wondering, as I have many rod pairs in storage.
- Knut