Adams Machinery > Gear AT > Gear AT Force > New Gear AT Force

New Gear AT Force

To create Gear AT Force there are number of parameters to be entered in following tabs of the dialog box shown in Figure 111:

Main

Figure 111 Create or modify gear force
 
For the options
Do the following
Gear Force Name
Enter the Gear Force name to create or browse for existing gear force to modify
Gear 1 toggle
free to orient / keep orientation
Select the role of the Gear 1 for the gear pair assembly:
Toggle ON to keep the orientation fixed
Toggle OFF to free the orientation
Gear 2 toggle
free to orient / keep orientation
Select the role of the Gear 2 for the gear pair assembly:
Toggle ON to keep the orientation fixed
Toggle OFF to free the orientation
Gear 1
Select existing gear element
Gear 2
Select existing gear element
CGS File Gear 1
Browse for *.CGS file of Gear 1 prepared during meshing preprocessing step. If selected Gear FAST modeling option this field in not enabled, user has to be provide *.CGF file in Contact tab instead
CGS File Gear 2
Browse for *.CGS file of Gear 2 prepared during meshing preprocessing step. If selected Gear FAST modeling option this field in not enabled, user has to be provide *.CGF file in Contact tab instead
Comments
Select to display a dialog box where you can add multi-line comments to any entity to describe its purpose and function.
Clearance check
Select to compute the clearance in the gear pair by using the solids of the gear rim.
Orient Gears
Run clearance study of the gear pair to correctly orient the gears.
Reset to input configuration when both gears are set to free to orient
Verify Gear AT model
Select to create and load automatically an Adams verification model of a gear pair
Extended definition:
Gear 1 / Gear 2 - free to orient / keep orientation
The Gear AT Force element is defined by Gear 1 and Gear 2. Gear AT Elements can be selected or created by the GUI options Pick, Browse, Guess or Create; see section Gear AT Element to learn more about the creation of a Gear AT Element.
The toggle keep orientation defines the gear, which is fixed for the assembly and the free to orient toggle sets the gear to mesh with the other one without contact.
Following combinations are applicable:
 
Gear 1
Gear 2
Action
Result
Keep orientation
Free to orient
Apply / OK / Orient Gears Button
Gear 2 will be oriented relative to Gear 1
Free to orient
Keep orientation
Apply / OK / Orient Gears Button
Gear 1 will be oriented relative to Gear 2
Keep orientation
Keep orientation
Apply / OK
No new orientation
Free to orient
Free to orient
Orient Gears Button
Both Gears will be reset to input configuration (no orientation)
Following rules are applicable:
At least one gear must be an external one
The internal gear must be Gear 2
The Gear 1 is automatically the wheel with smaller width in case of two external gears
Gear AT Mesh gives you the full control about the number of contact planes and the Mesh_density. Therefore you need to select the desired *.cgs files for the gear wheels. It is recommended to use a similar axial distance between the contact planes and an identical Mesh_density for both wheels; please read section FGear AT Mesh.
Clearance check
The icon of Figure 111 computes the clearance in the gear pair by using the solids of the gear rim. If clearance - what should be the normal case - is found, it will be shown as depicted by Figure 120. All gear pairs in the model will be checked for the minimum clearance value. Note that solids do not include the micro-geometry.
Orient gears
The icon of Figure 111 can be used to reset both gears to original configuration by setting both Gear 1 and Gear 2 toggles to free to orient and pushing the button. Hereafter, one can set new orientation by the Gear 1 and Gear 2 toggles and pushing the button again. In background, Adams creates model to run clearance study of the gear pair to correctly orient the gears. At the end of simulation the gears are reoriented according to the Gear 1 / Gear 2 toggles hence the warning message about losing parametric orientation is issued in message window, which can be disregarded.
Verify Gear AT model
The icon of Figure 111 creates and loads automatically an Adams model with the name 'verify_gear_AT_model'; see Figure 112. This model allows a visual check of the profiles of the gear stage. The filled areas represent the portion of the profile between start contact and end contact.
Figure 112 Verify profile definitions

Contact

Contact algorithm implemented in Gear AT is based on numerical approach which makes possible to account for varying backlash and contact stiffness at arbitrary shaft positions and angular misalignments. It can calculate contact up to five teeth at a time to capture variation of gear mesh stiffness.
To define gear pair contact force there are 4 modeling options available. The first modeling option Gear FAST offers pre-computed contact formulation delivering high performance with good quality of results. It is based on results of number of contact simulations by Flexible Tooth modeling option. Other three modeling options Rigid Gear, Flexible Tooth and Full Flex Gear use an advanced surface-to-surface contact algorithm, which delivers accurate and smooth results. The tooth flanks are described by the extruded profile including parametric definition of micro geometry.
The contact model Full Flex Gear employs algorithm of Flexible Tooth contact taking the flexible wheel body deformation into account. Wheel body deformation is based on modal flexibility implemented by Adams Flex and employs modal force (MFORCE) statement. Other contact modeling options employ Adams GFORCE element.
Figure 113 .Contact tab of Gear Force
 
For the options
Do the following
Modeling Option
Choose one of the following option to define the type of contact:
Gear FAST
Rigid Gear
Flexible Tooth
Full Flex Gear
If selected Gear FAST modeling option:
Create CGF File
Select this button to create new CGF file
CGF File
Browse for existing CGF file
If selected Rigid Gear modeling option:
Contact Stiffness (k)
Enter the value of contact stiffness that is used to calculate the contribution of the material stiffness to the normal contact force; see Equation  (28)
Default: 1.0e6
Stiffness Exponent (cexp)
Enter the value of stiffness exponent that specifies the exponent of the force deformation characteristic. For stiffening characteristic use value of cexp>1.0; see Equation  (28)
Default: 1.4
If selected Flexible Tooth or Full Flex Gear modeling option:
Contact Overlap
Choose one of the following option to control relaxation of contact algorithm:
Small (stiffer contact)
Normal
High (softer contact)
Default: Normal
 
Extended definition:
 
Modeling option defines the type of contact: you have 4 options to select from. The first modeling option Gear FAST offers pre-computed contact formulation delivering high performance with good quality results; for more information see Gear AT Fast Preprocessing. It is modeled with Adams GFORCE element as well as Rigid Gear and Flexible Tooth contact options.
Other three modeling options Rigid Gear, Flexible Tooth and Full Flex Gear use an advanced surface-to-surface contact algorithm, which delivers accurate and smooth results. The algorithm considers varying shaft positions and angular misalignments. The tooth flanks are described by the extruded profile including the micro-geometry. The solids for display are not used for the contact computation.The contact is checked for the left and right flanks of 5 tooth pairs.
For rigid body contact, the maximum penetration of each contact plane of Gear 1 into the flank of Gear 2 is used for the of the corresponding contact force Fcnt as shown by Equation  (28). The vector sum of all contact forces is giving the resulting contact force and torque vector per gear pair.
(28)
where:
k contact stiffness
pene maximum penetration
cexp exponent force law
 
In general, the deformation of a tooth is coming from the deformation of the wheel body, the deformation of the teeth and the 'Hertz contact'. The contribution of the 'Hertz contact' is limited compared to the two other contributions. Consequently, one has to assume, that the Stiffness Exponent is close to 1 or only slightly higher. An exponent of 1 corresponds to a linear contact stiffness.
For the Flexible Tooth contact model, the transmitted force between tooth flanks considers the flexibility of the teeth through the solution of a non-linear contact problem. The contact algorithm is of type surface-to-surface. A small relaxation by Contact Overlap is introduced for better performance; supported values are Small, Normal or High. Small overlap corresponds to stiffer contact whereas High overlap corresponds to softer contact. The effect of this additional flexibility is small compared to the flexibility of the teeth.
The contact model Full Flex Gear employs algorithm of Flexible Tooth contact taking the flexible wheel body deformation into account. Wheel body deformation is based on modal flexibility implemented by Adams Flex.

Friction

Friction of gear pair implemented in Gear AT is based on Coulomb friction model. Contribution of friction to total contact force can be turned On / Off by the friction model option. It is computed for each contact plane of Gear_1 based on the relative sliding velocity at the contact point.
 
Figure 114 Friction tab of Gear Force
 
For the options
Do the following
Friction Model
Choose one of the following options:
Off - in this case the other fields in this card will be disabled
On
Default: Off
Static Coefficient (µs)
Enter value of Static Friction Coefficient to define Coulomb friction
Default: 1.1e-2 [-]
Slip Velocity (vs)
Enter value of Slip Velocity to define Coulomb friction
Default: 1.0 [mm/sec]
Dynamic Coefficient (µd)
Enter value of Dynamic Coefficient to define Coulomb friction
Default: 1.0e-2 [-]
Transition Velocity Slip (vd)
Enter value of Transition Velocity Slip to define Coulomb friction
Default: 10.0 [mm/sec]
 
Extended definition:
 
The static friction coefficient is usually somewhat higher than the dynamic friction coefficient. Step functions are used for smoothing the transitions; see Figure 115. Parameter of slip velocity limits the region of sign change of the sliding velocity. The combination of very small slip velocity and high friction can reduce the performance of the integrator. You are advised to validate his selection through post-processing of the sliding velocity. Transition velocity defines the start of the region, where the dynamic friction is constant. A small difference between slip velocity and transition velocity could also lead to numerical issues of the integrator.
Figure 115 Friction coefficient
 
Under Gear FAST modeling option damping and friction are computed with simplified methods. The relative velocities in contact are evaluated only in middle plane of gear wheels. This approach can lead to noisy results under dynamic simulations; therefore adjustments for damping should be made with caution. The Friction model is reduced to 2 parametric model, with one friction coefficient and one threshold velocity.

Damping

The effects of hydrodynamic damping depend on gap height and squeeze velocities. The implemented damping force defined through Damping Rate Oil approximates hydrodynamic damping in function of the gap for each contact plane between the tooth flanks and the corresponding squeeze velocity.
 
Figure 116 Damping tab of Gear Force
 
For the options
Do the following
Damping Rate Oil
Enter value of Damping Rate Oil to define hydrodynamic damping as a function of oil squeeze velocity and actual oil film gap; see Figure 117.
Default: 200.0 [kg/sec]
Oil Film Thickness
Enter value of Oil Film Thickness per contact flank to define threshold value from which the hydrodynamic damping starts to build up; see Figure 117.
Default: 1.0e-2 [mm]
Damping Rate Structure
Enter value of Damping Rate Structure to define structural damping. It represents material damping therefore it is made proportional to the contact force.
Default: 1.0e-2 [-]
Damping Exponent
Enter value of Damping Exponent to define nonlinear hydrodynamic damping dependency on the actual oil film gap; see Figure 117.
Default: 2.0 [-]
 
Extended definition:
 
The function b defined by Equation  (28) is used to define the damping; see Figure 117.
(28)
There is no hydrodynamic damping, when b < 0; see Equation  (29)
(29)
Hydrodynamic damping increases exponentially with decreasing oil film height. The introduction of the damping exponent dexp in Equation  (30) is used for this purpose; see Figure 117.
(30)
In case of contact (penetration), the hydrodynamic damping force is set as shown by Equation  (31).
(31)
Figure 117 Function of hydrodynamic damping
 
Structural damping is usually a small value. The structural damping force is made proportional to the contact force as shown by Equation  (33). A value of 0.01 means, that the structural damping force is 1.0 percent of the elastic contact force.
(33)

Lubrication

Parameters entered in the lubrication tab do not influence computation of contact force, they are used to compute wear results of minimum oil film thickness; see Advanced Results.
Figure 118 Lubrication tab of Gear Force
 
For the options
Do the following
Pressure Coefficient of Viscosity (αp)
Refers to the relationship between the load placed on the oil film (pressure) at the dynamic load zone and the thickness of the oil film (viscosity) at that load, when all other factors (material, temperature, geometry, speed, load) are constant.
Units for input are [mm^2 / N]
Dynamic Viscosity (ν)
Dynamic viscosity (also known as absolute viscosity) is the measurement of the fluid's internal resistance to flow. Dynamic viscosity is product of kinematic viscosity and oil density.
Units for input are [Pa * s = N * s / mm^2]
Thermal Conductivity (λ)
Thermal conductivity (often denoted as k, λ, or κ) refers to the intrinsic ability of a material to transfer or conduct heat.
Units for input are [W / m * K = N / s * K]
Temperature Coefficient of Viscosity (αt)
Refers to the relationship between the temperature of oil at the load zone and the thickness of the oil film (viscosity) at that load, when all other factors (material, geometry, speed, load) are constant. Units for input are [1 / K]
 
Extended definition:
 
Min_oil_film thickness (hmin) is the key parameter to evaluate linear wear coefficient (C_lT). The coefficient can be found for different pair of materials in contact from lookup tables.
The results of Min_oil_film thickness can be found in the Wearing component of request and plotted as 2D curve or 3D plot via Advanced Results. It is calculated according to PLEWE formula. The thermal correction coefficient is also considered.
(1)
where:
Reqv - equivalent radius of curvature
G - elasticity coefficient
(2)
U - velocity coefficient
(3)
W - load coefficient
(4)
C - thermal correction
(5)
(6)
where:
αp - pressure coefficient of viscosity
αt - temperature coefficient of viscosity
λ - thermal conductivity
ν - dynamic viscosity
vΣ - sum of tangent velocities
Eeqv - equivalent module of elasticity
T - Torque
db - base diameter of pinion
αw - working pressure angle
b - width of contact
 
Figure 119 EHL film thickness behavior