Post by FredxxPost by Dave Plowman (News)Post by Peter HillWhen Yamaha re-designed the Ford Kent into the Zetec to accommodate the
sloppy tolerance of Ford's block machining line they had 20 main bearing
shell thicknesses with the right tight running clearance. They couldn't
stock undersize shells so the bottom end can't be repaired.
Certain types of treatment to crankshafts mean they can't be reground. And
aluminium cylinder bore are coated, so can't be re-bored either. But if
that treatment extends the life dramatically, the engine may well never
need a major overhaul anyway.
How many treatments? Most are a very thin layer, such as nitriding. Shot
peening being another.
Both can be done after a reground, but I've always been sceptical how
they increase the life for the crankshaft.
Shot peening introduces a compressive layer at the surface. As
compressive stresses do not crack, resistance to fatigue cracking is
greatly improved. The stress is additive, a tensile stress that would
normally cause cracking can be reduced below the endurance limit. If
stress is below endurance limit of steel it will never crack. Other
materials with alloys such as titanium, nickel or aluminium have no
endurance limit, they will crack with very small stresses applied often
enough (Mr Geller's stainless steel tea spoons). To double the cyclic
life the stress only has to reduce by 12.3%. For instance, 500 Mpa
tensile stress with 61 MPa compressive stress due to shot peen.
All rotating jet engine parts, shafts, discs and drums are shot peened.
Everything in a jet engine is going to crack sometime. The art and cost
is removing and replacing them at 2/3 of the life that the worst min
spec part will fail at.
All journal bearing surfaces should be hardened and polished. This
prevents scuffing on startup before oil film develops.
The treatment that is pure hogwash is dunking in cryogenic Nitrogen. The
only aerospace parts that are processed using cryogenic heat treatment
are steel ball and roller bearing tracks. They use an acetone and solid
CO2 mixture at -75°C to quench the red hot bearing ring, the whole
heating and quench process is done in an inert atmosphere to prevent
oxidation. This is to obtain the required hardness and not life. As each
flight for a large civil jet engine is around £500 in overhaul costs,
one more flight life would pay for a huge amount of liquid nitrogen
dunked parts. But as it doesn't give any life improvement at all they
don't bother. Dunking parts in liquid nitrogen is worse than using
water. Water makes steam which insulates the hot part, nitrogen will
boil and bubble just the same with room temperature parts. That's why
quenching is normally done in oil.
Meanwhile jet engine makers do platinum plate some parts, for corrosion
protection, paint would burn off.