pichet pinit
DESCRIPTION
MTE 427 MACHINE DESIGN. Pichet Pinit. Design of Spur Gears. 14 Sep, 2008. Template provided by. Lewis Bending Equation. Lewis Bending Equation: Dynamic Effect. Dynamic Factor. As a general rule, spur gears should have a face width F from 3 to 5 times the circular pitch p. - PowerPoint PPT PresentationTRANSCRIPT
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Lewis Bending Equation: Dynamic Effect
Dynamic Factor
As a general rule, spur gears should have a face width F from 3 to 5 times the circular pitch p.
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In these equations l and t are from the layout in Fig. 14–1, is the pressure angle, isthe fillet radius, b is the dedendum, and d is the pitch diameter.
Stress Concentration Factor
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AGMA Stress Equation
Two fundamental stress equations are used in the AGMA methodology, one for bending stress and another for pitting resistance (contact stress).
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Two fundamental stress equations are used in the AGMA methodology, one for bending stress and another for pitting resistance (contact stress).
AGMA Stress Equation: Bending Stress
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Two fundamental stress equations are used in the AGMA methodology, one for bending stress and another for pitting resistance (contact stress).
AGMA Stress Equation: Pitting Resistance
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Two fundamental strength equations are used in the AGMA methodology, one for bending stress and another for pitting resistance (contact stress).
AGMA Strength Equation: Bending Stress
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AGMA Strength Equation: Pitting Resistance
Two fundamental strength equations are used in the AGMA methodology, one for bending stress and another for pitting resistance (contact stress).
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AGMA Factors
• Geometry Factor• Elastic Coefficient• Dynamic Factor• Overload Factor• Surface Condition Factor• Size Factor• Load-distribution Factor• Hardness-ration Factor• Stress Cycle Factors• Reliability Factor• Temperature Factor• Rim-thickness Factor• Safety Factors
Important factors of AGMA used for gear analysis are as following,
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AGMA Factors: Surface Condition Factor
Surface condition factor, Cf (ZR)
The surface condition factor Cf (ZR) is used only in the pitting resistance equation. It depends on
• Surface finish as affected by, but not limited to, cutting, shaving, lapping, grinding, shot peening• Residual stress• Plastic effects (work hardening) Standard surface conditions for gear teeth have not yet been established.
When a detrimental surface finish effect is known to exist, AGMA specifies a value of Cf (ZR) greater than unity.
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AGMA Factors: Hardness-ratio Factor
Hardness-ratio factor, CH
The hardness-ratio factor CH is used only for the gear. Its purpose is to adjust the surface strengths for this effect.
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AGMA Factors: Hardness-ratio Factor
Hardness-ratio factor, CH
When surface-hardened pinions with hardnesses of 48 Rockwell C scale (Rockwell C48) or harder are run with through-hardened gears (180–400 Brinell), a work hardening occurs. The CH factor is a function of pinion surface finish fP and the mating gear hardness.
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AGMA Factors: Hardness-ratio Factor
Hardness-ratio factor, CH
When surface-hardened pinions with hardnesses of 48 Rockwell C scale (Rockwell C48) or harder are run with through-hardened gears (180–400 Brinell), a work hardening occurs. The CH factor is a function of pinion surface finish fP and the mating gear hardness.
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AGMA Factors: Reliability Factor
Reliability Factor, KR (YZ)
The reliability factor accounts for the effect of the statistical distributions of material fatigue failures.
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AGMA Factors: Temperature Factor
Temperature Factor, KT (Y)
For oil or gear-blank temperatures up to 250°F (120°C), use
KT = Y = 1.0. For higher temperatures, the factor should be
greater than unity. Heat exchangers may be used toensure that operating temperatures are considerably below this value, as is desirable for the lubricant.
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AGMA Factors: Rim-thickness Factor
Temperature Factor, KB
When the rim thickness is not sufficient to provide full support for the tooth root, the location of bending fatigue failure may be through the gear rim rather than at the tooth fillet. In such cases, the use of a stress-modifying factor KB or (tR) is recommended. This factor, the rim-thickness factor KB, adjusts the estimated bending stress for the thin-rimmed gear.