Create trusses
A truss wizard can be used to create a 2D, or a space truss, using steel, timber or cold formed elements. Alternatively you can manually create a free form truss without using the truss wizard.
Create a truss
The Truss Wizard helps you to create trusses in your models. For detailed instructions on how to use the Truss Wizard to create trusses, see the following instructions.
Create a space truss
Tekla Structural Designer allows you to create linear and planar space trusses. You can create space trusses in a 2D or 3D view. For more information, see the following instructions.
Create a free form truss
You can create a free form truss by placing a series of truss members in the required shape. For more information, see the following instructions.
Free form trusses cannot be created in a 3D view, or a 2D level view.
- Open the 2D frame view in which you want to create the truss.
- On the Model ribbon, open the truss/space/freeform list in the Steel, Timber, or Cold Formed group according to your needs.
- Click Free Form
- Click the start point of the first truss member.
- Click the end point of the first truss member.
- Repeat steps 4 and 5 to place each truss member as required.
- When the truss geometry is complete, press Esc to finish.
Modify the geometry of an existing truss
After creating a truss you can modify its geometry by using the Edit command. For more information, see the following instructions.
Modify the properties of existing trusses
You can modify the section sizes, material grades, section orientations, and other truss properties in the Properties window. For more information, see the following instructions.
- Move the mouse pointer over the desired truss, so that it becomes highlighted.
- Click the truss.
- In the Properties window, modify the truss properties according to your needs.
Steel truss member properties
Properties are listed below in the order that they appear in the Properties window.
| General | |
|---|---|
| Name | The automatically generated name. |
| User Name | Can be used to override the automatically generated name if required. |
| Plane | Indicates the level or frame within which the member is placed. |
| Characteristic |
|
| Element type | Beam |
| Material type | Steel |
|
Construction |
The available construction options depend on the characteristic and material type selected, see Member characteristic, construction and fabrication properties |
|
Fabrication |
The available fabrication options depend on the characteristic and material type selected, see Member characteristic, construction and fabrication properties |
| Autodesign | |
| Design section order [Only displayed when 'Autodesign' is selected] |
The design order file from which a section size will be
selected. For details of managing order files, see: Manage design section orders |
|
Rotation |
Rotation of the member about its local x axis. The default (Degrees0) aligns the major properties with the global Z axis, (provided that the member has not been specifically defined within an incline plane). |
| Alignment | |
| Global offset end 1, end 2 |
Can be used to model a physical offset with respect to the global axes at one or both ends of the member, (exceptions apply). |
| Major snap level, Minor snap level |
Defines the major and minor alignment of the member relative to the insertion point. |
| Major offset, Minor offset |
Used to offset the member from the snap point in the major and minor axis. |
| Truss general | |
|---|---|
| Name | The automatically generated name of the parent truss assembly. |
| User Name | Can be used to override the automatically generated name if required. |
| Material type | Steel |
| UDA | |
|
Name Finish Class Phase Note File |
A customizable list of the attributes that can be applied. |
| Span | |
|---|---|
| Section | The section size |
| Geometry (automatic design) [Only displayed if Autodesign is selected] |
The cross section type to be designed |
|
Grade |
Steel grade |
| Compression only, Tension only [Only displayed for Truss Internals] |
Specify if the truss internal is compression only, or
tension only. Note: Tension only
and Compression only members are non-linear elements and
therefore require non-linear analysis. If linear analysis is
performed they will be treated as linear
elements |
| Linearity | Straight |
| Top flange cont. rest. [Only displayed for Truss Top & Bottom members] |
Define if the top flange is continuously restrained. |
| Bottom flange cont. rest. [Only displayed for Truss Top & Bottom members] |
Define if the bottom flange is continuously restrained. |
| Releases | |
| Fixity end 1, end 2 |
[Fully Fixed, and Moment pin (Mz) are only available for Truss Top & Bottom members] |
| Cantilever end 1, end 2 [Not displayed for Truss Internals] |
Check one end only to define a cantilever end. |
|
Axial load release end 1, end 2 [Not displayed for Truss Internals] |
Check one end only to define an axial release. |
| Torsional load release end 1, end 2 |
Check one end only to define a torsional release. |
| Wind loading | |
| Apply open structure wind load |
Select this option if you want open structure wind loads to be calculated. |
| Shape factor, Cf | The default shape factor varies according to the entity
type and is taken from Model Settings > Loading >
Wind Loading Default Cf factors are taken from the document ‘Wind Loads For Petrochemical And Other Industrial Facilities’ published by ASCE. |
| Effective area XY | |
| Formula | The default effective area formula varies according to the entity type and is taken from Model Settings > Loading > Wind Loading |
| Factor | The factor used in the above formula can be edited if required. |
| Effective area XZ | |
| Formula | The default effective area formula varies according to the entity type and is taken from Model Settings > Loading > Wind Loading |
| Factor | The factor used in the above formula can be edited if required. |
| Live Load Reduction [ACI/AISC] | |
|
KLL |
Specify the KLL factor in accordance with Table 4-2 in ASCE 7-05/ASCE 7-10. |
| Imposed Load Reduction [Codes other than ACI/AISC] | |
| Reduce imposed loads by |
This property is particularly applicable to the design of transfer beams. Although the percentage of imposed load reduction is not determined automatically for beams, this property allows you to specify the percentage manually. It can be
applied to all, or individual spans.
The reduced results are used in concrete beam design. |
| Compression | |
|
Effective length factors |
Specified as Kx, Ky for ACI/AISC. Effective length factor y-y, z-z for other codes. |
| Tension | |
| Net area | Specified as an effective net area or a percentage value. |
| Deflection limits [Only displayed for Truss Top & Bottom members] |
|
| Apply span\factor | With this option checked, the limit can be defined as a Relative span/factor. |
| Apply abs. limit | With this option checked, the limit can be defined as an absolute value. |
| Size constraints | |
| Max depth, Min depth, Max width, Min width |
Size Constraints are only applicable when Autodesign is
checked. They allow you to ensure that the sections that Tekla Structural Designer proposes match any particular size constraints you may
have. For instance for a composite beam you may want to
ensure a minimum flange width of 150mm (6in). If so you
would simply enter this value as the Minimum width, and Tekla Structural Designer would not consider sections with flanges less than this
width for the design of this beam. See: Size constraints |
| Apply max span/depth ratio Max span/depth ratio |
After setting a max span/depth ratio you can check the
'Apply' button for it to be considered by auto-design.
During design, only sections which satisfy the maximum ratio
limit will be selected. The setting can also be reviewed and/ or copied via Review View > Show/Alter State. See: Size constraints |
| Instability factor | |
| Prevent out of plane instability | Define if out of plane stability is prevented. See: Instability factor |
| End 1 / End 2 [Only displayed for ACI/AISC regional code] |
|
| Apply SidePlate connection |
Select to apply a side plate connection at the specified end(s). |
| Utilization ratio | |
| Apply (to autodesign) |
Selected - When an Autodesign is performed, the design will be incremented to achieve a utilization ratio less than the ratio limit. Unselected - When an Autodesign is performed, the design will be incremented to achieve a utilization ratio less than 1.0. |
| Apply (to check) |
Selected - When a Check is performed, the check will pass provided the utilization ratio is less than the ratio limit. Unselected - When a Check is performed, the check will pass provided the utilization ratio is less than 1.0. |
| Ratio limit | The utilization ratio against which the autodesign or check is performed (when applied above). |
| Fire proofing | |
| Protected |
|
| Exposure | Exposed on all sides |
| UDA | |
|
Name Finish Class Phase Note File |
A customizable list of the attributes that can be applied to individual members and panels. |
Timber and cold formed truss member properties
Properties are listed below in the order that they appear in the Properties window.
| General | |
|---|---|
| Name | The automatically generated name. |
| User Name | Can be used to override the automatically generated name if required. |
| Plane | Indicates the level or frame within which the member is placed. |
| Characteristic |
|
| Element type | Beam |
| Material type |
|
|
Construction |
The available construction options depend on the characteristic and material type selected, see Member characteristic, construction and fabrication properties |
|
Fabrication |
The available fabrication options depend on the characteristic and material type selected, see Member characteristic, construction and fabrication properties |
|
Rotation |
Rotation of the member about its local x axis. The default (Degrees0) aligns the major properties with the global Z axis, (provided that the member has not been specifically defined within an incline plane). |
| Alignment | |
| Global offset end 1, end 2 |
Can be used to model a physical offset with respect to the global axes at one or both ends of the member, (exceptions apply). |
| Major snap level, Minor snap level |
Defines the major and minor alignment of the member relative to the insertion point. |
| Major offset, Minor offset |
Used to offset the member from the snap point in the major and minor axis. |
| Truss general | |
|---|---|
| Name | The automatically generated name of the parent truss assembly. |
| User Name | Can be used to override the automatically generated name if required. |
| Material type | Steel |
| UDA | |
|
Name Finish Class Phase Note File |
A customizable list of the attributes that can be applied. |
| Span | |
|---|---|
| Section | The section size |
|
Grade |
Material grade |
| Compression only, Tension only [Only displayed for Truss Internals] |
Specify if the truss internal is compression only, or
tension only. Note: Tension only
and Compression only members are non-linear elements and
therefore require non-linear analysis. If linear analysis is
performed they will be treated as linear
elements |
| Linearity | Straight |
| Releases | |
| Fixity end 1, end 2 |
[Fully Fixed, and Moment pin (Mz) are only available for Truss Top & Bottom members] |
| Cantilever end 1, end 2 [Not displayed for Truss Internals] |
Check one end only to define a cantilever end. |
|
Axial load release end 1, end 2 [Not displayed for Truss Internals] |
Check one end only to define an axial release. |
| Torsional load release end 1, end 2 |
Check one end only to define a torsional release. |
| Wind loading | |
| Apply open structure wind load |
Select this option if you want open structure wind loads to be calculated. |
| Shape factor, Cf | The default shape factor varies according to the entity
type and is taken from Model Settings > Loading >
Wind Loading Default Cf factors are taken from the document ‘Wind Loads For Petrochemical And Other Industrial Facilities’ published by ASCE. |
| Effective area XY | |
| Formula | The default effective area formula varies according to the entity type and is taken from Model Settings > Loading > Wind Loading |
| Factor | The factor used in the above formula can be edited if required. |
| Effective area XZ | |
| Formula | The default effective area formula varies according to the entity type and is taken from Model Settings > Loading > Wind Loading |
| Factor | The factor used in the above formula can be edited if required. |
| Live Load Reduction [ACI/AISC] | |
|
KLL |
Specify the KLL factor in accordance with Table 4-2 in ASCE 7-05/ASCE 7-10. |
| Imposed Load Reduction [Codes other than ACI/AISC] | |
| Reduce imposed loads by |
This property is particularly applicable to the design of transfer beams. Although the percentage of imposed load reduction is not determined automatically for beams, this property allows you to specify the percentage manually. It can be
applied to all, or individual spans.
The reduced results are used in concrete beam design. |
| Deflection limits [Only displayed for Truss Top & Bottom members] |
|
| Apply span\factor | With this option checked, the limit can be defined as a Relative span/factor. |
| Apply abs. limit | With this option checked, the limit can be defined as an absolute value. |
| Instability factor | |
| Prevent out of plane instability | Define if out of plane stability is prevented. See: Instability factor |
| Fire proofing | |
| Protected |
|
| Exposure | Exposed on all sides |
| UDA | |
|
Name Finish Class Phase Note File |
A customizable list of the attributes that can be applied to individual members and panels. |
Truss (for steel and cold formed), or
Truss (for
timber).
