AGMA 2101-D04 PDF

CAUTION NOTICE: AGMA technical publications are subject to constant improvement, ANSI/AGMA D04, Fundamental Rating Factors and Calculation. Credit line should read: “Extracted from ANSI/AGMA. Standard D04 or -D04 Fundamental Rating Factors and Calculation Methods for Involute Spur. Citations should read: See ANSI/AGMA D04, Fundamental Rating Factors and Calculation Methods for Involute Spur and Helical Gear.

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2110-d04 When the gear tooth is loaded on one flank, a point near the fillet of the loaded flank will see a full tensile load. This standard does not provide a method to estimate the minimum film thickness required. A major problem occurs in the calculation of the deflections.

The symbols and terms contained in this document may vary from those used in other AGMA standards. Those presented are used to show many of the considerations which may vary on each application. The YJ factor calculation uses the stress correction factors developed by Dolan and Broghamer [19].

Various terms factor of safety, service factor, and 2101d-04 factor are used in the gear industry to describe this important concept. This calculation is also performed using Method B.

These loads must be included with other externally applied forces in the overload factor, Ko. The final values are plotted and KH is calculated. Differs only slightly from the previous version, C This does not mean that all materials can be accurately estimated with the 0. A factor of safety accounts for uncertainties in: The best solution to this problem is to make an estimate of the load distribution and use this to calculate the actual deflection and iterate on this technique until the assumed load distribution curve and the actual agree within some reasonable tolerance.

In certain cases, a system may possess a torsional natural frequency close to an excitation frequency associated with an operating speed. It is not intended for use by the engineering public at large. To obtain values of the operating tangential load, the designer should use the values of power and speed at which the driven device will perform. It occurs when the oil film thickness is small enough to allow the flanks of the gear teeth to contact and slide against each other.


New Refinements to the Use of AGMA Load Reversal and Reliability Factors

In some applications this is not acceptable. Criteria for grades 1, 2, and 3 apply to both stress numbers unless HP FP otherwise specified in the metallurgical factor column. Most gearing applications are in one-way bending only. How does one determine what the load reversal factor is?

The effect of this undercut is to move the highest point of single tooth contact, negating the assumption of this ama method. Product application standards can be ag,a good source for the appropriate value of service factor see annex C for a more detailed discussion of application analysis.

The successful use of through hardened parts above HB depends upon experimentally developing a satisfactory technique for heat treating which will develop both high hardness and high fatigue strength. The empirical method shall not be used when analyzing the effect of a momentary overload.

The formulas evaluate gear tooth capacity as influenced by the major factors which affect gear tooth pitting and gear tooth fracture at the fillet radius. Hardness, tensile strength, microstructure and cleanliness are some criteria for determining allowable stress numbers.

As the uncertainties in design, materials, manufacturing, and loading become known: This standard is intended for use by the experienced gear designer, capable of selecting reasonable values for the factors. Hardness ratio factor, ZW surface hardened pinions. Other items such shot peening can also affect fatigue life. The effect of tapered rims has not been investigated. A collected sample of 210-1d04 data indicates the variability in values that can be used for capacity calculation of life factors.

Ideally this modification would create a lead that is the mirror image of the deflected gear, see figure D. The dynamic factor relates the total tooth load including internal dynamic effects to the transmitted tangential tooth load. But in view of the limited data, it is presented as two straight lines with a knee at 1. Ft b mn 15 The effects of webs and stiffeners can be an 2101-c04 but are not accounted for in annex B.

The fully reversing bending endurance limit of a material may be found 2101-d40 testing gears or may be found in publications for gears. In such cases, some size factor greater than unity should be used. For critical drives, a separate dynamic analysis of the entire system is recommended. Suggestions for improvement of this standard will be welcome.


Where root fillets of the gear teeth are produced by 2101-d4 process other than generating. Heat agm low alloy PM steels October 15, Variations in microstructure account for some variation in gear capacity. For the fully reversing bending 2101d-04, the mean stress is 0. In these cases, the design should afma checked 1201-d04 make certain that the teeth are not permanently deformed. The dynamic factor, Kv, does not apply to resonance. Allowable stress numbers for steel gears are established by specific quality control requirements agmz each material type and grade.

A guide for minimum case depth for nitrided external not internal teeth based on the depth of maximum shear from contact loading is given by the formula: It is not the intent of this standard that all requirements for quality grades be certified, but that practices and procedures be established for their compliance on a production basis. AGMA A03 provides a method of evaluating the risk of a gear set scuffing.

The ratings for pitting resistance are based on the formulas developed by Hertz for contact pressure between two curved surfaces, modified for the effect of load sharing between adjacent teeth. In such cases, the cumulative fatigue effect of the duty cycle is considered in rating the gear set.

Item Detail – ANSI/AGMA D04 (reaffirmed March )

For gearing requiring maximum performance, especially large sizes, coarse pitches, and high working stresses, detailed studies must be made of application, loading, and manufacturing procedures to determine the desired gradients of hardness, strength, and internal residual stresses throughout the tooth.

The influencing parameters can be categorized into four groups, all of which are normal to the manufacturing process but still cause face misalignments of the mating gear teeth. These radii are used to evaluate the Hertzian contact stress in the tooth flank.