AGMA 91FTM15-1991 Gear Hardness Technology《齿轮硬度工艺》.pdf
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1、91 FTM 15AvGear Hardness Technologyby: M. J. Broglie and D. F. Smith, Dudley Technical GroupAmerican Gear Manufacturers AssociationA- TECHNICALPAPERGearHardnessTechnologyM. J. Broglie and D. F. SmithDudley Technical GroupTheStatementsandopinions contained hereinarethoseof the authorandshouldnotbe co
2、nstrued asan official action oropinion of the American Gear ManufacturersAssociation.ABSTRACT:As progress continuallyplaces demands on the geardesignerto makegearing that is smaller, lighter and more reliable,the demand for bettergear materials and heat treatprocesses increases. Proper hardnessof a
3、gear, both inthe tooth and inthe body is becoming increasingly critical since load carrying capacity is dependent on hardness.The scope of this paper is limited to the most common methodsof heat treatmentof steel gearing, yet within this areathere are still many methods of heat treatment in wide use
4、 throughoutthe industry. The fact that there are so manymethods in use is testimony to the shortcomings of each process. When a designer selects the material and heattreatment to be used, among the considerations are the size of the gear and the gear tooth, facilifes available for heattreatment, the
5、 overall cost associated with the material and process, and the reliability which is required by theapplication of the gear.Copyright 1991American Gear Manufacturers Association1500 King Street, Suite 201Alexandria, Virginia, 22314October, 1991ISBN: 1-55589-612-XGEAR HARDNESS TECHNOLOGYMichael J. Br
6、oglie and Danny F. SmithDudley Technical Group IncorporatedSan Diego, California1.0 Introduction. the machinability. Intercritical annealinginvolves heating the part to a temperatureIn a very general sense, increasing the above the AI point but below the A_ point.- hardness of a steel gear increases
7、 the Finally there is subcrltical annealihg whichstrength of the gear. However, for each heats the part to just below the firstv process there is a limlt to its effective- transformation temperature (AI), as inness. This paper contains background infor- tempering, and it is slow cooled; just as inma
8、tlon on each of the processes covered. In full annealing. Subcritical annealing iseach section what is desired and what is often done to stabilize the structure priorachievable is discussed. Typical processes to carburizing.are presented along with comments on vari-ables which affect the result. By
9、reviewingthe capabilities and processes it is pos- Normalizing. Normalizing is a process whichsible to determine the limits to each pro- involves heating the part to above the uppercess. critical as in annealing, but it is cooledoutside the furnace in still or agitatedThroughout this paper several h
10、ardness air. Normalizing is done to relieve resid-scales are mentioned. The abbreviations for ual stresses in a gear blank and for dimen-these scales are as follows: sional stability. A normalized part is verymachinable but will be harder than if itBHN Brinell hardness number were annealed.KHN Knoop
11、 hardness numberHRC Rockwell “C“ scaleHV Vickers hardness number Stress relieving. Stress relieving isheating to below the lower transformation2.0 Prellminary Heat Treatment Processes. temperature, as in tempering, and cooling inair. This is done primarily to relieveThere are several heat treatments
12、 performed internal stresses. This process isduring the manufacturing process which are sometimes called process annealing.intended to condition the metal for manufac-turing. Since these are essential processesthey will be described briefly. 3.0 Through Hardening.Through hardening refers to heat tre
13、atment_nnealing. Annealing is a process in which methods which do not produce a case. Thisa part is heated and then slowly cooled in term does not imply that the hardness isthe furnace to 600 oF (316 C). Full anneal- uniform throughout the gear tooth. Sincev ing involves heating to a temperature abo
14、ve the outside of a gear is cooled faster thanthe upper critical (A_ point). This will the inside, there will a gradient in theresult in softening t_e part and improving hardness. The achievable hardness is basedon the amount of carbon in the steel. The The Process. To harden a part by thisdepth of
15、hardness depends on the hard- process, the part is heated to the aus- _enability of the steel, tenitic range, a temperature that varies,depending on the carbon and alloy content,For the purposes of this paper we will within the range of about 1500-1600 F (815- vconcentrate on the quench and temper p
16、ro- 870 C). In this state the steel becomescess. This method is used to obtain the austenite, which is a term for the solidfinal core properties of the material for solution of carbon in fcc iron (ref. 3).gears which are either cased or not cased. Then the part is rapidly quenched in oil (orWhen thi
17、s process is used to develop the sometimes water) to transform the austenitecore properties for nitrided gears, it is into martensite. If the quench is too slowdone prior to the nitriding cycle. When it the structure will not be fully transformedis used to harden a carburized gear, it is to martensi
18、te. The resulting microstructuredone after the gear has been carburized, will then contain what are called transfor-For gears which are not cased the load mation products, such as ferrite, bainite,carrying capacity of a gear is dependent on pearlite and cementite. The properties ofthe core hardness
19、of the material (The hardness, toughness, ductility and strengthcapacity of case hardened gears is primarily are dependent on the transformation productsdependent on case hardness). It is general- which are present.ly accepted to use the hardness value mea-sured at the root diameter in the center of
20、 The rate of cooling which must be achievedthe tooth when making comparisons to properly transform the steel to marten-site and minimize the percentage ofDepending on the loading the gear must transformation products is dependent on thehandle, it is often necessary to increase chemistry of the alloy
21、 being used. The a-the hardness of the steel. According to mount and type of alloying elements in theAGMA standards (ref. 1), a gear with a steel determine its hardenability.hardness of 400 BHN, which has a design lifeof 10 cycles, can handle as much as 20% Hardenability is a measure of the relative
22、more load than a gear which is hardened to depth to which hardness is achieved for a300 BHN. For hardnesses above 400 BHN the given quench rate and section thickness. Incapacity increases with respect to pitting other words, a material with a high hard-resistance, but the capacity decreases with ena
23、bility, which is quenched at the samerespect to bending strength, whlchdeterior- rate as a part of the same size, but withares because the tooth becomes brittle, low hardenability, will have hard material Adeeper.Though a great deal of attention is given tothe hardness of the material, it is import-
24、 The alloying elements which have an impactant to understand that the microstructure, on the hardenability of the steel are man-upon which the hardness depends, is what ganese, chromium, nickel, and molybdenum.really matters. Although in-depth discus- Table 1 is a table showing several alloysion of
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