Component

PP${\mathbf{G}}_{\mathbf{1}}$

PG${\mathbf{G}}_{\mathbf{2}}$

PG${\mathbf{G}}_{\mathbf{3}}$

PR${\mathbf{G}}_{\mathbf{1}}$

$r_{R\/\mathrm{sS}}$, $r_{R\/\mathrm{lS}}$$$

$r_{O\/I} \= \frac{r_{R\/\mathrm{sS}} - r_{R\/\mathrm{lS}}}{2 r_{R\/\mathrm{lS}}}$

$r_{O\/I} \= \frac{r_{R\/\mathrm{lS}} - 1}{r_{R\/\mathrm{sS}} - r_{R\/\mathrm{lS}}}$

$r_{O\/I} \= \frac{r_{R\/\mathrm{lS}} - 1}{2}$

$r_{R\/P} \= \frac{2r_{R\/\mathrm{lS}}}{r_{R\/\mathrm{lS}} - 1}$

$\mathrm{ideal}\=\mathbf{true}$

$\mathrm{ideal}\=\mathbf{true}$

$\mathrm{ideal}\=\mathbf{true}$

$\mathrm{ideal}\=\mathbf{true}$

$\mathrm{ideal}\=\mathbf{true}$

$\mathrm{ideal}\=\mathbf{false}$

$\mathrm{same} \mathrm{loss} \mathrm{data}\mathbf{\=}\mathbf{true}$

$\mathrm{\η}\left(\mathrm{\omega }\right)\, d$$$

$\mathrm{ideal}\=\mathbf{false}$

$\mathrm{\η}\left({{\mathrm{\omega }}^{}}_{I\/C}^{}\right) \=$$\mathrm{\η}\left(\mathrm{\ω}\right)$

$d \= d$

$\mathrm{ideal}\=\mathbf{false}$

$\mathrm{\η}\left({{\mathrm{\omega }}^{}}_{I\/C}^{}\right) \=$$\mathrm{\η}\left(\mathrm{\ω}\right)$

$d \= d$

$\mathrm{ideal}\=\mathbf{false}$

$\mathrm{\η}\left({{\mathrm{\omega }}^{}}_{I\/C}^{}\right) \=$$\mathrm{\η}\left(\mathrm{\ω}\right)$

$d \= 0$

$\mathrm{ideal}\=\mathbf{false}$

$\mathrm{\η}\left({{\mathrm{\omega }}^{}}_{R\/C}^{}\right) \=$$\mathrm{\η}\left(\mathrm{\ω}\right)$

$d \= 0$

$\mathrm{ideal}\=\mathbf{false}$

$\mathrm{same} \mathrm{loss} \mathrm{data}\mathbf{\=} \mathbf{false}$

${\mathrm{\eta }}_{\mathrm{iP}\/\mathrm{sS}}^{}\left({{\mathrm{\omega }}^{}}_{\mathrm{sS}\/C}^{}\right)\, {\mathrm{\η}}_{\mathrm{oP}\/\mathrm{iP}}^{}\left({{\mathrm{\omega }}^{}}_{\mathrm{iP}\/C}^{}\right)$$$

${\mathrm{\eta }}_{R\/\mathrm{oP}}^{}\left({{\mathrm{\omega }}^{}}_{R\/C}^{}\right)\, {\mathrm{\eta }}_{\mathrm{oP}\/\mathrm{lS}}^{}\left({{\mathrm{\omega }}^{}}_{\mathrm{il}\/C}^{}\right)$

$d_{\mathrm{iP}\/C} \,d_{\mathrm{oP}\/C}$

$\mathrm{ideal}\=\mathbf{false}$

$\mathrm{\eta }\left({{\mathrm{\omega }}^{}}_{I\/C}^{}\right) \= {\mathrm{\eta }}_{\mathrm{iP}\/\mathrm{sS}}^{}\left({{\mathrm{\omega }}^{}}_{\mathrm{sS}\/C}^{}\right)$

$d \= d_{\mathrm{iP}\/C}$

$\mathrm{ideal}\=\mathbf{false}$

$\mathrm{\eta }\left({{\mathrm{\omega }}^{}}_{I\/C}^{}\right) \= {\mathrm{\eta }}_{\mathrm{oP}\/\mathrm{iP}}^{}\left({{\mathrm{\omega }}^{}}_{\mathrm{iP}\/C}^{}\right)$

$d \= d_{\mathrm{oP}\/C}$

$\mathrm{ideal}\=\mathbf{false}$

$\mathrm{\eta }\left({{\mathrm{\omega }}^{}}_{I\/C}^{}\right) \= {\mathrm{\η}}_{\mathrm{oP}\/\mathrm{lS}}^{}\left({{\mathrm{\omega }}^{}}_{\mathrm{lS}\/C}^{}\right)$$$$$

$d \= 0$

$\mathrm{ideal}\=\mathbf{false}$

$\mathrm{\eta }\left({{\mathrm{\omega }}^{}}_{R\/C}^{}\right) \= {\mathrm{\eta }}_{R\/\mathrm{oP}}^{}\left({{\mathrm{\omega }}^{}}_{R\/C}^{}\right)$

$d \= 0$

Name

Condition

Description

ID

$\mathrm{Carrier} \left(C\right)$

$-$

Carrier flange

carrier

Ring (R)

$-$

Ring flange

ring

$\mathrm{Small} \mathrm{Sun} \left(\mathrm{sS}\right)$

$-$

Sun flange

small_sun

$\mathrm{Large} \mathrm{Sun} \left(\mathrm{lS}\right)$

$-$

Large flange

large_sun

$\mathrm{Inner} \mathrm{Planet}\left(\mathrm{iP}\right)$

$\mathrm{planet} \mathrm{port}\=\mathbf{true}$

Inner Planet flange

inner_planet

$\mathrm{Outer} \mathrm{Planet}\left(\mathrm{oP}\right)$

$\mathrm{planet} \mathrm{port}\=\mathbf{true}$

Outer Planet flange

outer_planet

$\mathrm{Loss} \mathrm{Power}$

$\mathrm{ideal}\mathbf{\=}\mathbf{false}$

Conditional real output port for power loss

lossPower

Symbol

Condition

Default

Units

Description

ID

$\mathrm{ideal}$

-

$\mathbf{true}$

-

Defines whether the component is:

true - ideal or

false - non-ideal

ideal

data source

$\mathrm{ideal}\=\mathbf{false}$

GUI

-

Defines the source for the loss data:

datasourcemode

$\mathrm{same} \mathrm{loss} \mathrm{data}$

$\mathrm{ideal}\=\mathbf{false}$

true

-

Defines whether one efficiency data table is used for all meshing loss calculations [$\mathrm{same} \mathrm{loss} \mathrm{data}\mathbf{\=}\mathbf{true}$] or the efficiency of each meshing gear pair is given by a separate data table [$\mathrm{same} \mathrm{loss} \mathrm{data}$$\=\mathbf{false}$].

SameMeshingEfficiency

$r_{R\/\mathrm{sS}}$

$-$

$4$

-

Ring/Small Sun Gear ratio

ratio1

$r_{R\/\mathrm{lS}}$

$\mathbf{-}$

$2$

Ring/Large Sun Gear ratio

ratio2

$n_{\mathrm{pl}}$

$\mathrm{ideal}\=\mathbf{false}$

$1$

Number of planet gear pairs

A planet pair consists of a set of inner planet and outer planet gears

numberofPlanets

$\mathrm{\eta }\left(\mathrm{\ω}\right)$

$\mathrm{ideal}\=\mathit{false}$

same loss data = true 

data source = GUI

  $\left[0\,1\,1\right]$ 

$\left[\frac{\mathrm{rad}}{s}\,-\,-\right]$

Defines all velocity dependant meshing efficiencies.

The columns:

[${\mathrm{\omega }}_{}$     (${\mathrm{\eta }}_1$ ($\mathrm{\ω}$ )     ${\mathrm{\eta }}_2$ ($\mathrm{\ω}$ )]

Five options are available:

Entered value is taken as the constant efficiency for forward and backward cases

${\mathrm{\eta }}_1$ ($\mathrm{\ω}$ ) = ${\mathrm{\eta }}_2$ ($\mathrm{\ω}$ ) = ${\mathrm{\eta }}_{}$

First entered value is taken as the constant efficiency for forward case and the second for backward cases

${\mathrm{\eta }}_1$ ($\mathrm{\omega }$) = ${\mathrm{\eta }}_1 \, {\mathrm{\η}}_2$ ($\mathrm{\ω}$ ) = ${\mathrm{\eta }}_2$

First column is ignored and the second and third values are taken as constant efficiencies for forward and backward cases, respectively

Second column is forward and backward efficiency

$\mathrm{\η}$ ($\mathrm{\ω}$) = ${\mathrm{\eta }}_1$ ($\mathrm{\omega }$ ) = ${\mathrm{\eta }}_2$($\mathrm{\ω}$ )

Second column is forward efficiency

${\mathrm{\eta }}_1$ ($\mathrm{\ω}$)

Third column is backward efficiency

${\mathrm{\eta }}_2$ ($\mathrm{\omega }$ )

meshinglossTable5

$\mathrm{ideal}\=\mathbf{false}$

same loss data = true 

data source = attachment

- 

Defines velocity dependant meshing efficiency table

First column is angular velocity (${\mathrm{\omega }}_{}$)

(See $\mathrm{col}$$\left[\mathrm{\η}\right]$ below)

data5

$\mathrm{ideal}\=\mathbf{false}$

same loss data = true 

data source =  file 

-

fileName5

$\mathrm{col}$$\left[\mathrm{\η}\right]$

$\mathrm{ideal}\=\mathbf{false}$

same loss data = true

data source = attachment or file

  $\left[2\,3\right]$

-

Defines the corresponding data columns used for forward efficiency (${\mathrm{\eta }}_1$) and backward efficiency (${\mathrm{\eta }}_2$ )

Two options are available:

Data column corresponding to the column number is used for both forward and backward efficiency $\mathrm{\η}\={\mathrm{\η}}_1 \= {\mathrm{\eta }}_2$ 

Data column corresponding to the first column number is used for forward efficiency (${\mathrm{\η}}_1\)$and data column corresponding to the second column number is used for backward efficiency (${\mathrm{\η}}_2\)$

columns5

${\mathrm{\eta }}_{\mathrm{iP}\/\mathrm{sS}}^{}\left({{\mathrm{\omega }}^{}}_{\mathrm{sS}\/C}^{}\right)$

$\mathrm{ideal}\=\mathbf{false}$

same loss data = false 

data source = GUI

  $\left[0\,1\,1\right]$ 

$\left[\frac{\mathrm{rad}}{s}\,-\, -\right]$

Defines inner Planet/small Sun velocity dependant meshing efficiency as a function of ${{\mathrm{\omega }}^{}}_{\mathrm{sS}\/C}$ .

The columns are:

[${{\mathrm{\omega }}^{}}_{\mathrm{sS}\/C}$     ${\mathrm{\eta }}_{\mathit{1}}^{}\left({{\mathrm{\omega }}^{}}_{\mathrm{sS}\/C}^{}\right)$     ${\mathrm{\eta }}_2$(${{\mathrm{\omega }}^{}}_{\mathrm{sS}\/C}^{}$ )]

First column is angular velocity of the small sun gear w.r.t. the carrier (${\mathrm{\ω}}_{\mathrm{sS}\/C}$)

Five options are available:

Entered value is taken as the constant efficiency for forward and backward cases

${\mathrm{\eta }}_1$(${\mathrm{\omega }}_{\mathrm{sS}\/C}$ ) =${\mathrm{\η}}_2$$\left({\mathrm{\omega }}_{\mathrm{sS}\/C}\right)$ =${\mathrm{\η}}_{}$

First entered value is taken as the constant efficiency for forward case and the second for backward cases

${\mathrm{\η}}_1$(${\mathrm{\omega }}_{\mathrm{sS}\/C}$ ) =${\mathrm{\η}}_1 \, {\mathrm{\η}}_2$(${\mathrm{\omega }}_{\mathrm{sS}\/C}$ ) =${\mathrm{\eta }}_2$

First column is ignored and the second and third values are taken as constant efficiencies for forward and backward cases, respectively

Second column is forward and backward efficiencies.

${\mathrm{\eta }}_{ }$(${\mathrm{\omega }}_{\mathrm{sS}\/C}$ ) =${\mathrm{\eta }}_1$ (${\mathrm{\omega }}_{\mathrm{sS}\/C}$ ) =${\mathrm{\eta }}_2$ (${\mathrm{\omega }}_{\mathrm{sS}\/C}$ )

Second column is forward efficiency

${\mathrm{\eta }}_1$ (${\mathrm{\omega }}_{\mathrm{sS}\/C}$ )

Third column is backward efficiency

${\mathrm{\eta }}_2$(${\mathrm{\omega }}_{\mathrm{sS}\/C}$ )

meshinglossTable1

$\mathrm{ideal}\=\mathbf{false}$

same loss data = false 

data source = file

- 

Defines the velocity dependent meshing efficiency

First column is angular velocity (${\mathrm{\omega }}_{\mathrm{sS}\/C}$ )

(See $\mathrm{col}$$\left[{\mathrm{\eta }}_{\mathrm{iP}\/\mathrm{sS}}^{}\right]$ below)

data1

$\mathrm{ideal}\=\mathbf{false}$

same loss data = false 

data source = file

-

fileName1

$\mathrm{col}$$\left[{\mathrm{\η}}_{\mathrm{iP}\/\mathrm{sS}}\right]$

$\mathrm{ideal}\=\mathbf{false}$

same loss data = false 

data source = attachment or file

  $\left[2\,3\right]$

-

Defines the corresponding data columns used for forward efficiency (${\mathrm{\eta }}_1$) and backward efficiency (${\mathrm{\eta }}_2$)

Two options are available:

Data column corresponding to the column number is used for both forward and backward efficiency (${\mathrm{\eta }}_1\={\mathrm{\eta }}_2 \= \mathrm{\η}\)$ 

Data column corresponding to the first column number is used for forward efficiency (${\mathrm{\eta }}_1$) and data column corresponding to the second column number is used for backward efficiency (${\mathrm{\eta }}_2$)

columns1

${\mathrm{\eta }}_{\mathrm{oP}\/\mathrm{iP}}^{}\left({{\mathrm{\omega }}^{}}_{\mathrm{iP}\/C}^{}\right)$

$\mathrm{ideal}\=\mathbf{false}$

same loss data = false 

data source = GUI

  $\left[0\,1\,1\right]$ 

$\left[\frac{\mathrm{rad}}{s}\,-\, -\right]$

Defines outer Planet/inner Planet velocity dependant meshing efficiency as a function of ${{\mathrm{\omega }}^{}}_{\mathrm{iP}\/C}$ .

The columns are:

[${{\mathrm{\omega }}^{}}_{\mathrm{iP}\/C}$     (${\mathrm{\eta }}_1$(${{\mathrm{\omega }}^{}}_{\mathrm{iP}\/C}$ )     ${\mathrm{\eta }}_2$(${{\mathrm{\omega }}^{}}_{\mathrm{iP}\/C}$ )]

First column is angular velocity of the inner planet gear w.r.t. the carrier (${{\mathrm{\omega }}^{}}_{\mathrm{iP}\/C}$)

Five options are available:

Entered value is taken as the constant efficiency for forward and backward cases

${\mathrm{\eta }}_1$(${{\mathrm{\omega }}^{}}_{\mathrm{iP}\/C}$ ) =${\mathrm{\η}}_2$$\left({{\mathrm{\omega }}^{}}_{\mathrm{iP}\/C}\right)$ =${\mathrm{\η}}_{}$

First entered value is taken as the constant efficiency for forward case and the second for backward cases

${\mathrm{\η}}_1$(${{\mathrm{\omega }}^{}}_{\mathrm{iP}\/C}$ ) =${\mathrm{\η}}_1 \, {\mathrm{\eta }}_2$(${{\mathrm{\omega }}^{}}_{\mathrm{iP}\/C}$ ) =${\mathrm{\eta }}_2$

First column is ignored and the second and third values are taken as constant efficiencies for forward and backward cases, respectively

Second column is forward and backward efficiency

${\mathrm{\eta }}_{ }$(${{\mathrm{\omega }}^{}}_{\mathrm{iP}\/C}$ ) =${\mathrm{\eta }}_1$ (${{\mathrm{\omega }}^{}}_{\mathrm{iP}\/C}$ ) =${\mathrm{\eta }}_2$ (${{\mathrm{\omega }}^{}}_{\mathrm{iP}\/C}$ )

Second column is forward efficiency

${\mathrm{\eta }}_1$ (${{\mathrm{\omega }}^{}}_{\mathrm{iP}\/C}$ )

Third column is backward efficiency

${\mathrm{\eta }}_2$(${{\mathrm{\omega }}^{}}_{\mathrm{iP}\/C}$ )

meshinglossTable2

$\mathrm{ideal}\=\mathbf{false}$

same loss data = false 

data source = attachment

- 

Defines the velocity dependent meshing efficiency

First column is angular velocity (${{\mathrm{\omega }}^{}}_{\mathrm{iP}\/C}$ )

(See $\mathrm{col}$$\left[{\mathrm{\eta }}_{P\mathrm{1}\/S}\right]$ below)

data2

$\mathrm{ideal}\=\mathbf{false}$

same loss data = false 

data source = file

-

fileName2

$\mathrm{col}$$\left[{\mathrm{\η}}_{\mathrm{oP}\/\mathrm{iP}}\right]$

$\mathrm{ideal}\=\mathbf{false}$

same loss data = false 

data source = attachment or file

  $\left[2\,3\right]$

-

Defines the corresponding data columns used for forward (${\mathrm{\eta }}_1$) and backward (${\mathrm{\eta }}_2$) efficiency

Two options are available:

Data column corresponding to the column number is used for both forward and backward efficiency (${\mathrm{\eta }}_1\={\mathrm{\eta }}_2 \= \mathrm{\η}\)$ 

Data column corresponding to the first column number is used for forward efficiency (${\mathrm{\eta }}_1$) and data column corresponding to the second column number is used for backward efficiency (${\mathrm{\eta }}_2$)

columns2

${\mathrm{\eta }}_{R\/\mathrm{oP}}\left({{\mathrm{\omega }}^{}}_{R\/C}\right)$$$

$\mathrm{ideal}\=\mathbf{false}$

same loss data = false 

data source = GUI

  $\left[0\,1\,1\right]$ 

$\left[\frac{\mathrm{rad}}{s}\,-\, -\right]$

Defines Ring/outer Planet velocity dependant meshing efficiency as a function of  ${{\mathrm{\omega }}^{}}_{R\/C}$ .

The columns are:

[${{\mathrm{\omega }}^{}}_{R\/C}$     (${\mathrm{\eta }}_1$(${{\mathrm{\omega }}^{}}_{R\/C}$ )     ${\mathrm{\eta }}_2$(${{\mathrm{\omega }}^{}}_{R\/C}$ )]

First column is angular velocity of the ring gear w.r.t. the carrier (${{\mathrm{\omega }}^{}}_{R\/C}$)

Five options are available:

Entered value is taken as the constant efficiency for forward and backward cases

${\mathrm{\eta }}_1$(${{\mathrm{\omega }}^{}}_{R\/C}$ ) =${\mathrm{\η}}_2$$\left({{\mathrm{\omega }}^{}}_{R\/C}\right)$ =${\mathrm{\η}}_{}$

First entered value is taken as the constant efficiency for forward case and the second for backward cases

${\mathrm{\η}}_1$(${{\mathrm{\omega }}^{}}_{R\/C}$ ) =${\mathrm{\η}}_1 \, {\mathrm{\eta }}_2$(${{\mathrm{\omega }}^{}}_{R\/C}$ ) =${\mathrm{\eta }}_2$

First column is ignored and the second and third values are taken as constant efficiencies for forward and backward cases, respectively

Second column is forward and backward efficiency

${\mathrm{\eta }}_{ }$(${{\mathrm{\omega }}^{}}_{R\/C}$ ) =${\mathrm{\eta }}_1$ (${{\mathrm{\omega }}^{}}_{R\/C}$ ) =${\mathrm{\eta }}_2$ (${{\mathrm{\omega }}^{}}_{R\/C}$ )

Second column is forward efficiency

${\mathrm{\eta }}_1$ (${{\mathrm{\omega }}^{}}_{R\/C}$ )

Third column is forward efficiency

${\mathrm{\eta }}_2$(${{\mathrm{\omega }}^{}}_{R\/C}$ )

meshinglossTable3

$\mathrm{ideal}\=\mathbf{false}$

same loss data = false 

data source = attachment

- 

Defines the velocity dependent meshing efficiency

First column is angular velocity (${\mathrm{\ω}}_{R\/C}$ )

(See $\mathrm{col}$$\left[{\mathrm{\eta }}_{R\/\mathrm{oP}}\right]$ below)

data3

$\mathrm{ideal}\=\mathit{false}$

same loss data = false 

data source = file

-

fileName3

$\mathrm{col}$$\left[{\mathrm{\eta }}_{R\/\mathrm{oP}}\right]$

$\mathrm{ideal}\=\mathbf{false}$

same loss data = false 

data source = attachment or file

  $\left[2\,3\right]$

-

Defines the corresponding data columns used for forward (${\mathrm{\eta }}_1$) and backward (${\mathrm{\eta }}_2$) efficiency

Two options are available:

Data column corresponding to the column number is used for both forward and backward efficiency (${\mathrm{\eta }}_1\={\mathrm{\eta }}_2 \= \mathrm{\η}\)$ 

Data column corresponding to the first column number is used for forward efficiency (${\mathrm{\eta }}_1$) and data column corresponding to the second column number is used for backward efficiency (${\mathrm{\eta }}_2$)

columns3

${\mathrm{\eta }}_{\mathrm{oP}\/\mathrm{lS}}^{}\left({{\mathrm{\omega }}^{}}_{\mathrm{lS}\/C}^{}\right)$$$

$\mathrm{ideal}\=\mathbf{false}$

same loss data = false 

data source = GUI

  $\left[0\,1\,1\right]$ 

$\[\frac{\mathrm{rad}}{s}\, -\, -$

Defines outer Planet/large Sun velocity dependant meshing efficiency as a function of ${{\mathrm{\omega }}^{}}_{\mathrm{lS}\/C}$ .

The columns are:

[${{\mathrm{\omega }}^{}}_{\mathrm{lS}\/C}$     ${\mathrm{\η}}_1$(${{\mathrm{\omega }}^{}}_{\mathrm{lS}\/C}$ )     ${\mathrm{\η}}_2$(${{\mathrm{\omega }}^{}}_{\mathrm{lS}\/C}$ )]

First column is the angular velocity of the large sun gear w.r.t. the carrier (${{\mathrm{\omega }}^{}}_{\mathrm{lS}\/C}$)

Five options are available:

Entered value is taken as the constant efficiency for forward and backward cases

${\mathrm{\η}}_1$(${{\mathrm{\omega }}^{}}_{\mathrm{lS}\/C}$ ) =${\mathrm{\η}}_2$$\left({{\mathrm{\omega }}^{}}_{\mathrm{lS}\/C}\right)$ =$\mathrm{\η}$

First entered value is taken as the constant efficiency  for forward case and the second for backward cases

${\mathrm{\η}}_1$(${{\mathrm{\omega }}^{}}_{\mathrm{lS}\/C}$ ) =${\mathrm{\η}}_1 \, {\mathrm{\η}}_2$(${{\mathrm{\omega }}^{}}_{\mathrm{lS}\/C}$) =${\mathrm{\η}}_2$

First column is ignored and the second and third values are taken as constant efficiency for forward and backward cases, respectively

Second column is forward and backward efficiency

$\mathrm{\η}$(${{\mathrm{\omega }}^{}}_{\mathrm{lS}\/C}$ ) =${\mathrm{\η}}_1$ (${{\mathrm{\omega }}^{}}_{\mathrm{lS}\/C}$ ) =${\mathrm{\η}}_2$ (${{\mathrm{\omega }}^{}}_{\mathrm{lS}\/C}$ )

Second column is forward efficiency

${\mathrm{\η}}_1$ (${{\mathrm{\omega }}^{}}_{\mathrm{lS}\/C}$ )

Third column is backward efficiency

${\mathrm{\η}}_2$(${{\mathrm{\omega }}^{}}_{\mathrm{lS}\/C}$ )

meshinglossTable4

$\mathrm{ideal}\=\mathbf{false}$

same loss data = false 

data source = attachment

- 

Defines the velocity dependent meshing efficiency

First column is angular velocity (${{\mathrm{\omega }}^{}}_{\mathrm{lS}\/C}$ )

(See $\mathrm{col}$$\left[{\mathrm{\eta }}_{\mathrm{oP}\/\mathrm{lS}}\right]$ below)

data4

$\mathrm{ideal}\=\mathit{false}$

same loss data = false 

data source = file

-

fileName4

$\mathrm{col}$$\left[{\mathrm{\eta }}_{\mathrm{oP}\/\mathrm{lS}}^{}\right]$

$\mathrm{ideal}\=\mathbf{false}$

same loss data = false 

data source = attachment or file

  $\left[2\,3\right]$

-

Defines the corresponding data columns used for forward (${\mathrm{\η}}_1$) and backward (${\mathrm{\η}}_2$) efficiency

Two options are available:

Data column corresponding to the column number is used for both forward and backward efficiency $\mathrm{\η}\={\mathrm{\η}}_1 \= {\mathrm{\η}}_2$ 

Data column corresponding to the first column number is used for forward efficiency (${\mathrm{\η}}_1$) and data column corresponding to the second column number is used for backward efficiency (${\mathrm{\η}}_2$)

columns4

$d_{\mathrm{iP}\/C}$

l$\mathrm{ideal}\=\mathbf{false}$

same loss data = false 

0

$\left[\frac{\mathrm{N}\cdot \mathrm{m}}{\frac{\mathrm{rad}}{s}}\right]$

Linear damping in planet1/carrier bearings

d1

$d_{\mathrm{oP}\/C}$

$\mathrm{ideal}\=\mathbf{false}$

same loss data = false 

0

$\left[\frac{\mathrm{N}\cdot \mathrm{m}}{\frac{\mathrm{rad}}{s}}\right]$

Linear damping in planet2/carrier bearings

d2

d

$\mathrm{ideal}\=\mathbf{false}$

same loss data = true 

0

$\left[\frac{\mathrm{N}\cdot \mathrm{m}}{\frac{\mathrm{rad}}{s}}\right]$

Linear damping in planet/carrier bearing

d3

smoothness

$\mathrm{ideal}\=\mathbf{false}$

Table points are linearly interpolated

-

Defines the smoothness of table interpolation

There are two options:

smoothness