That sets the piston travel to a lower setting ... when deburring the machining of the walls during the initial break-in.GJEMD wrote:I would suggest a 3 hr trip at sustained 3000 rpm
I actually think that almost everyone agrees that is and example of what NOT to do, but what do I know??GJEMD wrote:I would suggest a 3 hr trip at sustained 3000 rpm
Your wing comparison may apply at 7000 rpm, where the connecting rod is beyond factory specs and may stretch a bit or bend. But by the way we are talking about engine breakin and 7000 rpm is not relevent to the discussion and in fact would surely set you up a new engine for oil consumption. Break in is mostly moot with computer machined engines with molybdenum coated cylinders. The top end with titanium valveswith harden seats is like wise mostly moot. The rings are very well the weak link in these engines and if the case no system is stronger than its weakest link. The VK within operating ranges specified by the factory is static with little to no inertia. That would include the heads with 4 valves/cylinder, very little movement and virtually no valve train inertia.ken in az wrote:Actually yes, the engine will behave differently at different rpms. The system is not static as everyone thinks. If you have the idea that the piston moves exactlt the same at 600rpm then it does at 7000rpm then you are completely mistaken.
The same rules apply to all metallurgical structures. Take a look at an aircraft wing durring flight - it is not fixed, more like it is flopping in the wind flexing attributing to the forces at hand. Also look at skyskrapers, they sway in the wind. Why do they flex? If they didn't, they'd break. Same thing is happening to the moving parts in an engine. even though the tolerances are much tighter and the movement isn't percievable to the eye, is is still flexing and behaving differently.
Just a little pysics for you - http://www.steel.org/AM/Templa...23463