SchmidtMotorWorks wrote:Kevin Johnson wrote:Aside: Erland, sorry about internet wars. This is important.
Jon, I think the problem is that you are not used to doing academic research.
For someone that goes on and on about research, you sure choose to cite some real garbage.
Time to man up and admit the references you posted in regards to crankshafts, if followed, would make junk as racing cranks.
Prepare for some more real garbage.
When I checked out Taylor I also checked out the
Standard Handbook of Machine Design by Shigley and Mischke, 1986 Volumes 1 and 2. In Chapter 13 Mischke mentions in 13-3-6 miscellaneous influences on fatigue strength, including induction hardening. The suggestion is that the fatigue strength factor associated with these processes are largely detrimental but that "they are not well understood quantitativly in any comprehensive way".
Moving to:
Subsurface fatigue crack initiation and propagation behavior of induction-hardened shafts under the effect of residual and applied bending stresses by
Zhang, Stephens & Glinka in Fatigue and Fracture Mechanics: 30th Volume, ASTM STP 1360
Page 243:
"Fatigue crack propagation is usually analyzed using fracture mechanics with the assumption that cracks already exist in the components" and that the core case interface is the presumed location.
Moving to:
Increasing the fatigue limit of a high-strength bearing steel by a deep cryogenic treatment by E. Kerscher, K.-H. Lang
Journal of Physics: Conference Series 240 (2010) 012059 Issue 1, 2010
Abstract:
High-strength steels typically fail from inclusions. Therefore, to increase the fatigue limit of high-strength steels it is necessary to modify the inclusions and/or the surrounding matrix. The goal must be a higher threshold for crack initiation and/or crack propagation. One possibility to reach this goal seems to be a deep cryogenic treatment which is reported to completely transform the retained austenite as well as to facilitate the formation of fine carbides. Therefore, specimens were annealed before or after deep cryogenic treatment, which was carried out with different cooling and heating rates as well as different soaking times at −196° C. Hardness and retained austenite measurements and fatigue experiments were used to evaluate the different sequences of treatments mentioned above. The fatigue limit increases only after some of the sequences. The results show that the soaking times are not relevant for the fatigue limit but it is very important to temper the specimens before the deep cryogenic treatment. Also, repeated deep cryogenic treatments had a positive influence on the fatigue limit.
And:
http://www.benthamscience.com/open/tome ... 1TOMEJ.pdf
The Open Mechanical Engineering Journal, 2008, 2, 1-11 1
1874-155X/08 2008 Bentham Science Publishers Ltd.
Deep Cryogenic Treatment: A Bibliographic Review
P. Baldissera and C. Delprete
page 3 wrote:EFFECTS ON THE MATERIAL MICROSTRUCTURE
Ferrous Alloys
According to the literature about cryo-treated tool steels,
the improvement of mechanical properties can be ascribed to
different phenomena:
• Complete transformation of the retained austenite into
martensite;
• Fine dispersed carbides precipitation;
• Removal of residual stresses.
It is known that almost all steels at 193 K transform the
austenite into martensite. The use of cold treatment has been
initially developed on martensitic tool steels in order to remove
retained austenite with benefits on hardness.
Moving to:
http://www.metal-wear.com/history.html
We've traced cryogenic processing as far back as the 1930's where the Junkers company in Germany used it on components of their Jumo aircraft engines. We got this from a fellow who worked with an ex-Junkers engineer by the name of Adolph Luerker. Mr. Luerker emigrated to the US after the war and ended up in California working for McCulloch Chain Saw company. He suggested that they use the process on chain saw blade links. They did and started cryo treating their chainsaw blades but kept it a secret so other manufacturers could not make better blades. This was around the mid 1950's.
Moving to:
http://de.wikipedia.org/wiki/Junkers_Jumo
My emphasis:
Junkers Jumo war die Marken-Bezeichnung der von Junkers Motorenbau und Junkers Flugzeugwerk bzw. ab 1936 von den Junkers Flugzeug- und Motorenwerken (JFM) selbst hergestellten Otto- und Diesel-Flugmotoren, Strahltriebwerke und Zweitakt-Dieselmotoren für Nutzfahrzeuge.
Die Abkürzung Jumo setzt sich aus den Worten Junkers Motor zusammen.
Moving to:
My emphasis:
Lurenbaum in:
Jahrbuch
1937 der deutschen Luftfahrtforschung.
Unter Mitwirkung des Reichsluftfahrtministeriums und der Luftfahrtforschungsanstalten und -Institute sowie de Lilienthal-Gesellschaft.
Moving to:
Cryogenics, The Racer’s Edge
Diekman, Frederick J. and Roger Schiradelly
Heat Treating Progress
November 2001, pp. 43-49
Available at:
http://www.cryogenictreatmentdatabase.o ... cers_edge/
~~~~~~~~~~
Remarks: Cryogenic treatment of aircraft engine components would have been top secret information in both Germany and during WWII and after the war for the Allies. It is possible that the components that Lurenbaum tested were cryogenically treated and this is why they exceeded the strength estimates predicted in 37.14, Figure 37-2 of Shigley and Mischke for solid versus hollow bars.
Jon, you need to seriously improve your research skills and ability to correlate information from disparate sources and that includes making connections between historical and current research.