wuzak
Captain
Allison improved the heat treatment by work-hardening (peening) and tempering the (steel) crank case and crank shaft, and then they coated the bearings with a metal called indium.
Crankcase was aluminium.
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Allison improved the heat treatment by work-hardening (peening) and tempering the (steel) crank case and crank shaft, and then they coated the bearings with a metal called indium.
Wasn't there also an improvement in fuel that allowed the increase from 1150hp to 1325hp?
Hey Schweik,
Thanks for the info - on both metallurgical subjects.
Short answer.
The improved fuel allowed the engine to make 1325hp (and a higher WEP) for short periods of time (seconds or a few minutes).
It was the improved materials and heat treatment/processes that allowed the engine to make the higher powers on a more regular basis for longer periods of time without breaking.
Crankcase was aluminium.
As I understand it, the fuel allowed the engine to develop 1325HP at takeoff for 5 minutes without detonation. The strengthening (improved materials and heat treating) were needed for the engine to handle that extra power. Maybe we are saying the same thing.Short answer.
The improved fuel allowed the engine to make 1325hp (and a higher WEP) for short periods of time (seconds or a few minutes).
It was the improved materials and heat treatment/processes that allowed the engine to make the higher powers on a more regular basis for longer periods of time without breaking.
P-40K was rated at 1550 hp and 60" Hg for 5 minutes at sea level for WEP, and
1325 hp and 51" Hg at sea level for takeoff, also for 5 minutes.
That is with a V-1710-73 or an overhauled V-1710-39
My source for that is Shamburger, Page & Christy, Joe. "The Curtiss Hawks". Wolverine Press, 1972. Library of Congress No. 79-173429
Just to clarify, the 150 hour test was continuous, right? The segments were just throttle/rpm/mixture changes while the engine was continuously running.You may very well be right on the overhaul. I highlighted the "overhauled" part as the newer crankshafts would drop into the older crankcases,
The fuel may allow the engine to run at those manifold pressures and power levels without detonation.
However the Engines had to pass a type test, which for American engines was at least 150 hours total running time.
10 hours (which could be broken into 120 5 minute segments) at take-off or military power, and 40 hours at "Normal" (Max continuous) or 91% of take-off power, which ever was greater ( they may be some discrepancy here) The engine also had to run at 10 hours in an over speed condition but not making full power, this part of the test could also be run in 120 30-60 second segments.
When WEP ratings showed up the test included 7 1/2 hours at the WEP rating either continuously or in the 5 minute segments.
Sometimes engines were put into production before they past a type test, or sometimes if there was little difference the type test was waived (change of type of magneto?)
What pilots/mechanics did in the field was one thing but the the guys in the supply chain didn't want engines wearing out/breaking before they were supposed to. It turned out that even 20% spare engines was nowhere near enough at times and pushing engines for extra performance meant shorter times between overhauls even if the engine/s didn't fail in flight.
Just like with hot rods and modified motorcycles making more power is seldom a big problem, getting the engine to survive the extra power is where the trouble is.
The test was supposed to be continuous. However a few breaks were often allowed for "minor" repairs or servicing, like changing spark plugs or perhaps a broken valve or valve spring.Just to clarify, the 150 hour test was continuous, right? The segments were just throttle/rpm/mixture changes while the engine was continuously running.
Expand please.One book I read in my teen years (1950s) told of the many parts the mechanics in the PTO could make from a US copper penny.