I don’t have the relevant qualifications in these fields so please pardon my ignorance; after all I’m just a gear cutter.
tbuelna & israelkk; Thank you for the valid and important concerns you both mention. I’m not sure but it almost sounds to me that both of you are saying that perhaps it can’t be done. I admit that the problem is not a common one but none the less, non lubricated steel gears are widely used in industry. It appears that there are no standards for this type of application and this surprises me due to fact there are so many sets out there working quite satisfactorily.
dimjim: One day I hope to get to the US and take part in one of Ray’s workshops. You touch on the point of accuracy; this is one area I feel that requires careful consideration in this application.
tbuelna; In answer to your questions:
From what I understand of the subject; Flash Temperature can be derived from one of Blok’s equations (in this case taken from Dudley’s Gear Handbook, edited by Dennis Townsend) where lubricant film has no relevance to the instantaneous surface temperature under hertzian contact. Blok’s “Classical” equation for Flash Temperature assumes hertzian pressure distribution, equal surface temperature on both surfaces and no oil film. My understanding of Tribology is that Flash Temperature does not necessarily have to include heat generation & heat conduction within the oil film and heat transfer to the contacting bodies. As far as I can see…..Blok’s equation seems to show that this is in fact the case. In fact none of the flash temperature equations I’ve been able to find use oil film data. Am I missing something?
I’m yet to fully understand the theory but would it be correct to theorise that, when the lubrication regime is in an E.P. boundary condition and lambda less than 0.40 and sliding speed is less than 1.5m/sec, the convection of heat generated from within the oil film to the surrounding sliding bodies would approach a point where it would have less relevance on Flash Temperature? After all……..boundary lubrication suggests that, due to a higher number of asperity contacts and those asperities either deforming or shearing off and also reduced sliding or rolling between the members less oil is available for developing an E.H.D. film. Wouldn’t this then suggest that, because of the reduced amount of lubrication present, the heat developed within the oil due to shearing and pressure is going to have less of an effect on the surrounding bodies?
The 1400N/mm^2 contact stress you claim I mention as being the actual contact stresses involved is incorrect. Please re-read my posting and you will see that this figure is taken from the S/N Curve for the material I propose to use. As my post states, the calculated stress is around 715N/mm^2.
As far as load cycles; as I understand it, the S/N charts I’m looking at show (1e +01) is equivalent to 10. So (1e+10) would be 10,000,000,000. I note that I made a mistake in my post; the required life is not 4.2e+06 rather it should have been 4.65e+07 or 46,500,000 cycles or 10,000 hours @ around 77.50 rpm. Once again, I have no qualifications in regards to maths or engineering so please correct me if I’m wrong.
israelkk: below is the current gear data and also the data of the set I propose to use.
Based on ISO6336 this is the best I can come up with remembering that this standard requires lubrication. I figured that if I can come up with a design that has the highest flank safety while trying to reduce the amount of sliding by using 25 deg PA, I might have a chance or at least have a point to start off with. I can get higher flank safeties by reducing the PA but this increases sliding.
The current configuration uses a type of nylon called Ertalon, which is extruded bar stock, for the pinion and flame hardened K1045 carbon steel for the gear. Estimated AGMA 2000 grade is around 6-7. This is mainly due to the estimated amount of distortion of the ring type gear as a result of flame hardening.
Service life of the nylon pinion varies between different machines but an average life expectancy is around 50 – 100 hours. The machines are being run at greater capacity than what they were originally designed for.
The machines are called Take Up Units and are part of a wire galvanising line. The machines are at the end of the line and pull the wire from the start of the line and then coil the wire into bundles. So load is steady and even.
Drive is provided by VFD controlled 9kw motors and transmitted to the gear sets via V belts and pulleys.
Current Gear Data, Plastics To Niemann:
Module = 5.08
Pressure angle = 20deg
Helix angle = 12.50deg
Zp = 34
Zg = 55
F.W. p = 40mm
F.W.g = 40mm
Xp = -0.4544
Xg = -0.5346
Centre distance = 226.00mm
Application factor = 1.25
Required Service life = 10,000hrs
Safety root Pinion = 0.1537
Safety flank Pinion = 0.1472
Proposed Gear Data to ISO6336:
Material: Case Hardened 4317, 58-62 Rc
AGMA 12
Module = 3.75
Pressure angle = 25deg
Helix angle = 12.25deg
Zp = 45
Zg = 73
F.W. p = 68mm (max. due space constraints)
F.W.g = 56mm (max. due space constraints)
Xp = 0.0194
Xg = -0.1269
Centre distance = 226.00mm
Application factor = 1.25
Required Service life = 10,000hrs
Safety root Pinion = 3.795
Safety flank Pinion = 2.253
Any thoughts would be much appreciated.
Ron Volmershausen
Brunkerville Engineering
Newcastle Australia