I am not quite sure what you mean by guide rod. Something like the crosshead rods used in the big low speed industrial diesels ?Tommy Cookers wrote: ↑11 Apr 2017, 22:26well the alloy piston revolution in the 20s was largely about increasing TE as the lower piston crown temperature allowed higher CRMudflap wrote:.........Other claims are that a hotter piston also helps combustion and that the reduced heat transfer improves TE - I have not seen concrete evidence of these.
highly boosted heat dilution engines have higher mean gas pressures and so relatively high piston frictional losses
a 1 piece steel piston/guide rod might well usefully eliminate side load friction and have benefits at high rpm (and give SHM)
Who want's vegetable juice.Selvariabell wrote: ↑11 Apr 2017, 20:37Why the larger displacement? They could have a V8 with that.
The 1980s engines did that with 1.5l capacity. So why 2.0l?
1987 engine only had to last a few laps in Qual then replaced for race.wuzak wrote: ↑12 Apr 2017, 00:16The 1980s engines did that with 1.5l capacity. So why 2.0l?
Is the power output including KERS?
1987, max MAP 4 bar, qualifying ~1,000hp, race ~800hp. So similar to what the current engines produce sans ERS.
1988, max MAP 2.5 bar, qualifying ~690hp, race ~625hp.
The problem I see with using just KERS is that it limits how long it can be used.
When asked of the differences between his Force India Mercedes F1 car and Porsche 919 Le Mans car, Nico Hulkenberg said that the Le Mans car leapt out of the corner but lost momentum part way down, while the F1 car pulled all the way down the straights. I like the sound of the latter better.
If the current engines were changed to be twin turbo plus KERS, the MGUH being excluded, and the KERS power increased to 300hp from 160hp with recovery on front and rear axles, you would have 1,000+hp. In the region of 1,050-1,100hp in fact.Sasha wrote: ↑12 Apr 2017, 01:491987 engine only had to last a few laps in Qual then replaced for race.wuzak wrote: ↑12 Apr 2017, 00:16The 1980s engines did that with 1.5l capacity. So why 2.0l?
Is the power output including KERS?
1987, max MAP 4 bar, qualifying ~1,000hp, race ~800hp. So similar to what the current engines produce sans ERS.
1988, max MAP 2.5 bar, qualifying ~690hp, race ~625hp.
The problem I see with using just KERS is that it limits how long it can be used.
When asked of the differences between his Force India Mercedes F1 car and Porsche 919 Le Mans car, Nico Hulkenberg said that the Le Mans car leapt out of the corner but lost momentum part way down, while the F1 car pulled all the way down the straights. I like the sound of the latter better.
2021 3 or 4 engines for the whole season.
So 1000-1200 hp is very good for a engine that would has to last 5-6 race weekends.
Thickness of the section has much more effect than modulus or strength. I just ran FEA on a flat disc (think piston crown) in steel and aluminium. I adjusted thickness to give the same mass for each. (Thickness for steel was 1.72mm, Al was 5mm) With uniform pressure loading to one side of the disk, I got the following results.Mudflap wrote: ↑11 Apr 2017, 01:23While 3x thickness gives you lower stresses, the endurance strength is still lower - by about 4 times (at 10 million cycles, after than Al keeps dropping even further behind). Overall the factor of safety will favor steel pistons if only by a small margin.Tommy Cookers wrote: ↑10 Apr 2017, 23:43you seem to be saying that those NA F1 people were wrong in their piston material ?
and the mass-specific stiffness of steel being equal to that of Al alloy is not a dog in this fight
the piston being substantially loaded in bending, alloy wins as if 3x the thickness has greater strength for the same weight etc
or less weight for the same strength
the reason why planes are alloy not steel
ok the temperature is the crucial factor here (as with some planes or parts thereof)
but it's hard to believe a steel piston is better rpm wise than would an alloy piston be even within its safe working temperature
Endurance strength is a material property, it is not geometry dependent.
You did not have to do fea for that - the disk you are discribing is just an axisymmetric beam. From beam bending equations you would get about 8.4 higher stress in steel and 8.6 higher deflection assuming E= 200 Gpa for steel and 70 Gpa for Al.gruntguru wrote: ↑12 Apr 2017, 06:45Thickness of the section has much more effect than modulus or strength. I just ran FEA on a flat disc (think piston crown) in steel and aluminium. I adjusted thickness to give the same mass for each. (Thickness for steel was 1.72mm, Al was 5mm) With uniform pressure loading to one side of the disk, I got the following results.Mudflap wrote: ↑11 Apr 2017, 01:23While 3x thickness gives you lower stresses, the endurance strength is still lower - by about 4 times (at 10 million cycles, after than Al keeps dropping even further behind). Overall the factor of safety will favor steel pistons if only by a small margin.Tommy Cookers wrote: ↑10 Apr 2017, 23:43you seem to be saying that those NA F1 people were wrong in their piston material ?
and the mass-specific stiffness of steel being equal to that of Al alloy is not a dog in this fight
the piston being substantially loaded in bending, alloy wins as if 3x the thickness has greater strength for the same weight etc
or less weight for the same strength
the reason why planes are alloy not steel
ok the temperature is the crucial factor here (as with some planes or parts thereof)
but it's hard to believe a steel piston is better rpm wise than would an alloy piston be even within its safe working temperature
Endurance strength is a material property, it is not geometry dependent.
Stress at centre of disc - 8x higher for steel.
Deflection at centre of disc - 8x higher for steel.
Endurance strength means squat when you are forced to design for yield strength.
What if there was a way to use less material in that region but retain similar strength, for example using a diamond cubic lattice or octet truss to create the ribs via 3d printing?Mudflap wrote: ↑13 Apr 2017, 23:14You did not have to do fea for that - the disk you are discribing is just an axisymmetric beam. From beam bending equations you would get about 8.4 higher stress in steel and 8.6 higher deflection assuming E= 200 Gpa for steel and 70 Gpa for Al.gruntguru wrote: ↑12 Apr 2017, 06:45Thickness of the section has much more effect than modulus or strength. I just ran FEA on a flat disc (think piston crown) in steel and aluminium. I adjusted thickness to give the same mass for each. (Thickness for steel was 1.72mm, Al was 5mm) With uniform pressure loading to one side of the disk, I got the following results.Mudflap wrote: ↑11 Apr 2017, 01:23
While 3x thickness gives you lower stresses, the endurance strength is still lower - by about 4 times (at 10 million cycles, after than Al keeps dropping even further behind). Overall the factor of safety will favor steel pistons if only by a small margin.
Endurance strength is a material property, it is not geometry dependent.
Stress at centre of disc - 8x higher for steel.
Deflection at centre of disc - 8x higher for steel.
Endurance strength means squat when you are forced to design for yield strength.
The problem is that you are assuming the load is carried by the crown - in reality the largest portion of the load ( that creates bending about the pin axis) is carried by the ribs joining the pin bores to the skirt. The moment of area of these is proportional to the cube of the height rather than the cube of the thickness. Now, if you redo your fea the stress in the steel rib is only 2.9 times higher than Al while deflection is virtually the same (2% higher with the elastic moduli I mentioned ).
The same results also hold true for the pin bores which can be assumed to be loaded in pure tension under inertial loads and pure compression under gas loads.
Also if you do the math the pistons experience about 12 milion load reversals in 300 km per race at 150 kmph, 10 k rpm and 5 races - not even counting qualy. At that many cycles you have to design for theoretically infinite life therefore endurance strenght is important. Classic fatigue theory assumes about 1000 cycles to failure at stresses equal to 0.9 x yield strength...
I think that such structures hamper conductive heat transfer which is critical for pistons.godlameroso wrote: ↑15 Apr 2017, 01:25
What if there was a way to use less material in that region but retain similar strength, for example using a diamond cubic lattice or octet truss to create the ribs via 3d printing?