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Aim- To perform static structural analysis of spur gears using Ansys Workbench on below mentioned materials 1. Cast Iron 2. Cast Steel 3.Cast Bronze To evaluate results for total deformation, Equivalent stress and stress intensity and comparing the result for all materials and to recommend best material fromdesign point…
Tribhuvankumar Pandit
updated on 18 May 2022
Aim-
To perform static structural analysis of spur gears using Ansys Workbench on below mentioned materials
1. Cast Iron
2. Cast Steel
3.Cast Bronze
To evaluate results for total deformation, Equivalent stress and stress intensity and comparing the result for all materials and to recommend best material fromdesign point of view based on evaluated result.
Theory-
Spur gears are a cylindrical shaped toothed component used in industrial equipment to transfer mechanical motion as well as control speed, power, and torque. These simple gears are cost-effective, durable, reliable and provide a positive, constant speed drive to facilitate daily industrial operations.
At Grob, Inc., we manufacture our own tooling, allowing us the flexibility to fabricate standard or custom cold rolled spur gears designed to meet exact specifications across a wide range of industrial applications.
Stress Intensity Factor-
In fracture mechanics, the stress intensity factor (K) is used to predict the stress state ("stress intensity") near the tip of a crack or notch caused by a remote load or residual stresses.[1] It is a theoretical construct usually applied to a homogeneous, linear elastic material and is useful for providing a failure criterion for brittle materials, and is a critical technique in the discipline of damage tolerance. The concept can also be applied to materials that exhibit small-scale yielding at a crack tip.
The magnitude of K depends on:
Sample geometry
Size and location of the crack
Magnitude of load
Distribution of load
The stress intensity factor is a single-parameter characterization of the crack tip stress field.
To consider the stress analysis of cracked bodies, it is important to distinguish basic "modes" of stressing. As shown in Fig., the three basic modes are: opening (mode I), in-plane shear (mode II) and out-of-plane tearing (mode III). Mode I corresponds to normal separation of the crack faces under the action of tensile stresses, which is by far the most widely encountered in practice. The difference between Mode II and Mode III is that the shearing action in the former case is normal to the crack front in the plane of the crack whereas the shearing action in Mode III is parallel to the crack front. A cracked body in reality can be loaded in any one of these three, or a combination of these three modes.
Fig. Basic modes of crack extension; (a) opening mode, (b) sliding mode, and (c) tearing mode.
From previous analysis, it is clear that when stresses at the crack tip exceed yield (which always happens for engineering materials), plasticity results. However, if the redistribution of stress has a minimal effect on the crack tip elastic stress field, then the K approach to defining the stress field is still of sufficient accuracy for engineering applications. Thus, if plasticity is minimal, then a LEFM approach is justified.
Of importance to practical applications is the critical stress and strain state at the crack tip zone, which, when attained, causes the crack to propagate in a brittle, catastrophic manner. The most dangerous situation occurs when a crack is in a high-energy but constrained field that permits only slight plastic deformation at the crack tip. Expressed another way, the amount of energy absorbed in plastic deformation is reduced to a minimum extent and much more energy is thus available for fracture, i.e. crack propagation. This critical state can be described by a critical stress intensity factor Kc,
which may imply either a low stress acting on long crack or a small crack suffering a high stress.
Procedure-
Connection details-
Joint Details-
Meshing-
Boundary Conditions-
Analysis Setting-
Joint Load Details,
1. Rotational Joint.
Analysis Result-
1. Equivalent Stress (Von-Mises)-
a) Cast Iron-
b) Cast Steel-
c) Bronze Cast-
2. Total Deformation-
a) Cast Iron-
b) Cast Steel-
c) Bronze Cast-
3. Stress Intensity-
a) Cast Iron-
b) Cast Steel-
c) Bronze Cast-
Result Animations-
1. Equivalent Stress (Von-Mises)-
a) Cast Iron-
b) Cast Steel-
c) Bronze Cast-
2. Total Deformation-
a) Cast Iron-
b) Cast Steel-
c) Bronze Cast-
3. Stress Intensity-
a) Cast Iron-
b) Cast Steel-
c) Bronze Cast-
Conclusion-
Case | Material | Equivalent Stress | Total Deformation | Stress Intensity | |||
Max. | Min. | Max. | Min. | Max. | Min. | ||
Case-1 | Cast Iron | 443.1 | 1.25E-08 | 30 | 18.5 | 471.5 | 1.44E-08 |
Case-2 | Cast Steel | 442.7 | 6.25E-09 | 30 | 18.5 | 472.9 | 6.99E-09 |
Case-3 | Bronze Cast | 410.3 | 2.56E-08 | 30 | 18.5 | 439.6 | 2.66E-08 |
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