Autodesk robot structural analysis professional 2018 tutorial pdf free –
The monitor screen will be divided into tree parts: the graphical viewer containing LMC the field for selecting RSAP the structure model; the Diagrams dialog box and the table layout presenting the values of reactions. Defining and Analyzing a Concrete Floor This example will demonstrate step-by-step how the user can define and analyze a simple slab with an opening. Test the operation of, Particular options. In order to define a new combination type, one should click the New option. In the Point field set the Point The point position equal to 0. As it can be seen, in spite of the work in the plastic range, the structure retains stability.
Autodesk Robot Structural Analysis Training Autodesk Robot Structural Analysis Training Author / Uploaded; kevin. Online Resources Download ; Verification Manuals ; Installation Manual (pdf – Kb) ; Getting Started Guide – Imperial Units (pdf – Kb). Autodesk® Robot™ Structural Analysis Professional Training Manual -Metric Version. Download Free PDF. paper cover icon. paper cover thumbnail.
Last Seen. You May Like Also. We bring you the best Tutorial with otosection automotive based. Stay Connected. Home News Technology Gadget Design. Welcome Back! On the X tab chose the Define option Defines the method of axis numbering. Creates the vertical located in the Numbering field and axes designated with consecutive numbers x1, x2, x3, etc. Enter the following values in the Position field: 0 Insert, 1 Insert, 1.
Creates the vertical located in the Numbering field and axes designated with consecutive numbers y1, y2, y3 etc. Enter the following values in the Position field: 0 Insert, 0. Creates the vertical located in the Numbering field and axes designated with consecutive numbers z1, z2, z3 etc. Presents the initial view of the structure axes see the Select the Zoom All icon from picture below. LMC in the Geometry button Opens the dialog box that allows defining a contour. Set the cursor in the green field, then Defines a contour, closes the Polyline – Contour dialog switch to the graphic viewer and box.
Select the Zoom All icon from the Standards toolbar. LMC in the Internal point field and Applies current properties to the selected panel. The defined structure without presentation of the structural axes is shown in the drawing below.
Selects the recently defined panel, whose color changes to red. Activate the ll to Axis option and Once this option is selected, the object will be extruded select the Z axis along the axis that is parallel to the Z axis of the global coordinate system. In the edit field set the length of the Defines the length of the extrusion vector.
Apply, Close Extrudes the selected two-dimensional object along the appropriate axis. Switch to the graphic viewer and Sets a new global work plane for structure definition. Only the structure components located in this plane will remain visible. Select the Three points option in the Selects a rectangle as a base of the cube. The rectangle Definition method field will be defined by means of the two opposite apexes of the rectangle.
Switch to the graphic editor and Defines the cube, closes the Cube dialog box. In the graphic viewer select the top- Translates the selected cube. In the Translation Vector field located in the Translation dialog box, enter the following numbers: 0, 4, 0 , Execute RMC in the graphic viewer and Opens the context menu choose the Select option Select the recently defined cubes Translate the selected cubes.
The defined structure without presentation of the construction axis is shown in the drawing below. Set the cursor in the green field, then Defines contour, closes the Polyline – Contour dialog box. Select the Hidden icon in the If this option is selected, invisible lines in the structure will lower left corner of screen.
Select the Shading icon in the If this option is selected, invisible lines in the structure will lower left corner of screen. Planar tab Switch to the graphic viewer; Selects the surface of the foundation base. Selects the initial RSAP layout. On the Structure tab, in the Display Displays symbols of structure supports on the screen, dialog box activate Supports – closes the Display dialog box.
Using the dynamic zoom option enables structure rotation Select the Rotate, Zoom, Pan and pan, so that the bottom structure part with supports can icon from the Standard toolbar. Only the structure components located on this plane will remain visible. Define the additional nodes whose Defines nodes, closes the Node dialog box. In the graphic viewer select Sets a new global work plane for structure definition.
Define additional nodes whose Defines nodes, closes the Nodes dialog box. In the Plane Location edit field Defines the coordinate of the horizontal mirror axis. In the Coordinates field enter the Defines the additional node no. Selects the RSAP program layout that allows defining structure loads.
In the Values Z: field enter Defines the value of the uniform load acting on surface FEs in the direction of the Z axis of the global coordinate system. Add Closes the Uniform Planar Load dialog box. Set the cursor in the Apply To field, Displays the currently selected structure panel. LMC on the Contour definition Opens the dialog box that allows defining the contour to button which the load will be applied.
It may be performed either in the dialog box or graphically on the screen. In the green field enter the points Defines the contour to which the loads will be applied. In the Values Z: field enter , Defines the concentrated force loads acting on a selected Add structure node. Select a node located nearest Displays the currently selected structure panel see the 10;0;4 picture below. Once the Select the Calculations icon calculations are completed, the viewer title bar will show the from the Standard toolbar.
Layout Select the load case: 4 LL3. On the Detailed tab, in the Values in Selects the visualization of the displacement for individual the local system field, activate the FEs in the local coordinate system.
LMC the Apply button Presents the structure displacement see the picture below. On the Deformation tab deformation of the currently designed structure – see the select the active option located in the picture below. Deformations field, Apply Select the load case: 3 LL2.
In the Deformations field switch on Activates presentation of deformation for the currently the Active option designed structure.
Apply Presents the structure displacement. Shell Structures This chapter contains a presentation of several short examples of modeling three-dimensional structures by means of extrude and revolve options. After a while, there appears on screen the dialog box, where one should select the second icon in the second row Shell design. Data units: m. Define the following four bars: Definition of RC beams beam 1: begin.
LMC in the Section field and select the type HEB if the section is absent on the list of available sections, open the New section dialog box by pressing the button and select the required section Define the following four steel Definition of steel columns columns of the 10 m length: col. Define the following four beams: Definition of steel spandrel beams beam1:begin. LMC in the Section field and select the type CAE x12 if the section is absent on the list of available sections, open the New section dialog box by pressing the button and select the required section Define the following bracings: Bracing definition 1: begin.
Meshing Options In the Available meshing methods Sets the meshing parameters. Eight load cases have been assigned to the structure and six of them are displayed in the drawings below. The vignette window will be displayed on the screen and the icon in the second row Shell Design should be selected. LMC in the Geometry button Opens the dialog box which allows defining a contour. Enter the following coordinates into Defines a contour.
Select Zoom All icon from the standard toolbar. LMC in the Model field and set Defines a calculation model that will be applied to the Shell model defined panel. The defined structure is displayed in the drawing below. On the Model tab in the Display Displays symbols of structure supports on the screen, dialog box activate closes the Display dialog box.
Opening of the Trapezoid Truss structures – beams, frames, trusses Type 3 dialog box. LMC twice the icon the last one in the third row In the Dimension tab LMC the Defines length of the lower truss chord it may be defined Length L1 field graphically in the graphical viewer.
On the Dimensions tab in the Applies divided chords to the structure. To all truss chords upper and lower assign TRON x6. Apply, OK Creates the defined structure at the indicated point within the construction and closes the Merge Structure dialog box. Switch to the graphic viewer and Selects all truss bars.
The defined structure is LMC on the field to select the displayed in the drawing below. LMC in the Section field and select. TRON x6. Chose the Select option and indicate the recently defined bar. Opens the Load Definition dialog box.
In the Values Z: field enter In the Apply To field enter 1 Displays the current selection of structure panel. Apply Applies predefined load to a chosen panel.
In the Load Definition dialog box Opens the Uniform planar load on contour dialog box. LMC on the Contour definition Opens the dialog box that allows defining the contour to button which the load is applied.
LMC on the Contour definition Opens dialog box that allows defining the contour, to which button the load will be applied. In the green field enter coordinates Defines contour to which the loads will be applied. In the field Apply To type 1 Displays the current selection of structure panel.
Apply, Close Applies the predefined load to a chosen panel, closes the Uniform Planar Load contour dialog box. LMC on the fifth field in the Case Defines loads for the fifth load case. LMC on the fifth field in the Case Defines loads for the sixth load case.
Enter: in the Database field: User in the Database name field: User-defined database in the Database description field: User-defined vehicles in the Internal units of the database chose m as Length units and kN as Force unit Create Closes the New Moving Load dialog box.
Opens the Moving Loads dialog box and starts defining a new vehicle. LMC the third line in the table Defines operating forces. Select User database and press the Saves the defined vehicle to the user-defined database. OK button in the Moving load databases dialog box Add, Close Adds the defined vehicle to the list of active vehicles and closes the Moving Loads dialog box.
In the Name field, enter the name of Defines a name of the moving load. Select the User database, OK in the Saves the defined vehicle to the user-defined database. Moving load databases Add, Close Adds the defined vehicle to the list of active vehicles and closes the Moving Loads dialog box. Assume the default value of load direction: 0,0,-1 which means that the load will be operating in the Z direction and its sense will be opposite to the Z axis sense LMC the Automatic option located in Selects the plane of load application.
Once the calculations are completed, the title bar of the viewer will present the following information: Finite Elements Results – available. Layout Selects the load case: 2 LL1. On the Detailed tab activate the z Activates visualization of the displacement for individual option in the Displacement – u,w line surface FEs in the local coordinate system.
These are the displacements in the direction perpendicular to the element surface. Activate Maps option Allows presentation of results obtained for FE in the form of maps. Selects the load case: 7 Moving vehicle. On the Deformation tab switch on the Activates presenting deformation of the currently designed Active option structure. LMC the Start button Starts performing the displacement animation for the structure.
Stops the animation. In the Buckling length coefficient Y Opens the Buckling Diagrams dialog box which allows defining buckling length for members. In the Buckling length coefficient Z Opens the Buckling Diagrams dialog box which allows defining buckling length for members. In the Member Type field enter: Applies the name to a new bar type. Opens the Member Definitions – Parameters dialog box. In the Member Type field enter: Assigns the name to a new bar type.
Diagonals Save, Close Saves current parameters for the Cross braces member type, closes the Member Definitions – Parameters dialog box. Definitions dialog box press the New button Define the first group with the Defines the first group consisting of all bars belonging to the following parameters: upper chords in the structure.
Using this In the Selection of Sections dialog option user can select sections that will be applied during box select all TRON profiles which verification and design of steel and aluminum elements. Also evaluate the patent for its ability to safeguard or defend the concept or process compared to other products on the market and the structure for which it is written. A few similar patents include: 9,,; 10,,; 10,,; 10,,; 6,, Any proposal involving demolition of a building should include a statement setting out why it is not possible to retain and improve the existing building in line with Policy 38, cross referencing the whole life cycle carbon analysis where required.
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It’s checked out by default It means that the elements added to printout composition will be located in separate pages. Robobat Polska Sp. Indicate Loads component and activate the context menu by means of the right-hand mouse button. Thus, the Loads component will be placed on the same page as the Bars component. Go to the left-hand panel and indicate all screen captures apart from “Capture 1” click the selected elements with the Cir!
Uncheck the checkbox imposing location on separate pages the one beside the red dashed line. Move the screen captures to the right by means of the Add button. Select the Start on a new page option from the context menu. There will appear a dashed red line indicating that the given elements start at a new page.
Reopen the context menu and select the Note before option. Close the editor by confirming the message on saving the changes. Indicate the first components in the list, ie. Close the editor. NorbeFosri: ones Print the created document. Press the Print button at the bottom of the dialog box. Close the Printout Composition dialog box. Open the 7-results file 2. Once the dialog box is open see the picture below , click the New Lllicon. To achieve this, one should click the Li ] icon, which results in the appearance of the dialog box see the picture below that allows one to select the buckling length coefficient.
By clicking the appropriate icon, one should select the coefficient 1. Once the selection is done, close the dialog box by clicking OK button. Define the parameters of lateral buckling type in the Lateral Buckling Parameters dialog box: — Define the lateral buckling type by clicking the icon Lat Buckling Type within the Lateral Buckling Parameters field.
ES Once the selection is done, close the dialog box by clicking OK button. Define the effective length coefficient for beam by clicking the icon: Upper Fiange do the same with Lower Flange. Nome Destbaing ast loa eae ait latin abut ng. Check out the check boxes referring to the Member deflection options in the Limit Displacements field. Save the above settings by clicking Save in the Member Definition — Parameters dialog box.
Then, close the dialog box by clicking the Close button. Then one should go to the graphical viewer and indicate the two structure beams, while the Ctrl button is pressed. Confirm by clicking Apply and close the dialog box by clicking Close. The screen will be divided into three parts: the View graphic viewer, the Definitions and Calculations dialog box see the picture below. Once the selection is done, close the dialog box by clicking Close. Therefore, one should select the Ultimate and Service options in the Limit State field.
In order to define the verification parameters, one should click the Configuration button. In order to launch the verification process, one should click the Calculations button. The program will automatically verify the selected sections and, once the calculations are finished, there appears the dialog box presenting the verified members see below.
Note option. There appears the Printout dialog box see the picture below. Select here the Table Printout option. Thus, we obtain a table with all the verified elements. This can be done by means of the Full printout option. By means of the Table screen capture option, one may obtain a screen capture of the table of results.
There will appear the Results dialog box presenting detailed results see the picture below. Close the dialog box by pressing OK. Confirm the operation clicking the OK button. Structure geometry Open the plate file Proposed scheme of the plate 6.
Radzikowskiego 47D, Krakow, Poland c p. Click the Hlill button located to the tight of the Section field. This results in the appearance of the New Section dialog box shown on the picture below and define a concrete beam with the section dimensions x Set the cursor in the Node Coordinates field and enter the following points.
Definition of the beam supporting the arc-shaped part of the plate There are two ways to define an arc-shaped beam supporting the arc-shaped part of the plate. One should remember that the plate fragment should be zoomed in appropriately to the needs. Once the operation is finished, one should close the Bars dialog box. Introduce coordinates of the second point 9; 10 in the Coordinates field and confirm with the Add button.
Two new nodes are thus created. Nodal forces will be applied in these nodes. After opening the dialog box for load definition, define a new load case of the Live LL3 nature. Select the Nodal Force load type in the Node tab of the dialog box. Set the cursor in the Apply To field of the Load Definition dialog box and introduce the numbers of the two above-defined nodes. Confirm by clicking the Apply button. Close the dialog box by clicking Close button.
Once the option is selected, the program adjusts the FE mesh to the newly defined nodes. Once the operation is confirmed by clicking OK, there appears the Combinations dialog box that allows one to define combination parameters.
The Case List field contains all the load cases that may be included in the new combination. The Factor field allows one to modify the combination factor. The default factor values may be checked and modified for a nature by clicking the Factor Definition button. In order to carry out a modification of the factor, one should indicate one of the load cases e. LL1 and introduce the new factor value in the Factor field, 1. Then, the selected case will be moved to the right-hand panel of the List of Cases in Combinations dialog box with the new factor value.
The remaining load cases, should be moved to the right-hand panel without factor modification by clicking the I button. Note: In the exercise all factors was set as default. In order to define a new combination type, one should click the New option.
Did you find this document useful? Is this content inappropriate? Report this Document. Flag for inappropriate content. Download now. For Later. Jump to Page. Search inside document. The selected elements may be edited in a new window. To do so, one should press the Eclt in New Window icon [A – after selecting the required elements. There will appear a new window viewer with the selected element. Tables Structure parameters may be modified by means of the relevant tables.
The tables relevant to the current layout become visible, when one enters the layout. There will appear the Tables: Data and Results dialog box.
A table containing data will be generated for each of the indicated items. Once the Edit tab is activated in the bottom left corner of a given table, one may perform the operation of modifying structure parameters. Structural axes Itis possible to modify the position of structural axes during the design process. Once the Select option is chosen except when one is in the START layout , one should double-click the symbol numbering referring to the required axis, which results in the appearance of the below-presented dialog box used for structural axis modification.
Test the operation of, Particular options. The available tabs allow one to get access to the data on structure parameters. Default options Once the 3 icon the third one icon in the bottom left comer of the screen is pressed, the program restores the default attributes presented on screen.
Robobat Polske Sp. Structure geometry 1. Proposed model of a 2D frame Proposed scheme of the frame RC beam x, columns x Structural axes definition Click the Axis Deftriton 82! Tab X: -4; 0; 6; 12; 4 — Set Numbering to: 1, 2, and Tab Z: 0; 3.
To define the B x section, one should: — Set RC Beam option located in the Section Type field, — Set in the b field, — Set in the h field, — End the operation by pressing the Add button the newly defined section appears in the Bar Sections dialog box. To define the UC xx89 section, one should: — Set Stee! Repeat the operation for UB xx54 section then close the New Section dialog box.
Close the Sections dialog box. The program will apply supports to the three selected nodes, which will be displayed in the View Viewer. Robobet Polska Sp. The screen will be divided into three parts: graphical viewer, Loads table and Load Types dialog box. Go to the Apply To field in the Load Definition dialog box; the mouse cursor will change from the choice mode into the selection mode. Then, indicate beams 4,5,6,7 in the graphical viewer with the Ctrl button pressed, click on the bars.
The bar numbers will appear in the Apply To field. Apply this load to elements 6 and 7 Robobat Polska Sp. Select the left columns bar No.
Select the left beam bar No. Select the right columns bar No. Select the right beam bar No. Go to the Loads table. The Edit tab allows one to modify the existing loads and define new ones. Load Combinations defined manually Open 3-loads file We can create load combinations using two methods. In the Factor edit field introduce the new value 1. Close the dialog box by pressing the Close button.
Move the 1 to 5 load cases to the List of Cases in Combination dialog box. By means of the 13! The fist solution allows one to control the factors for each separate case Le. If the Auto option is set, the factor will assume the value defined in the Combination Factors dialog box Confirm the creation of the COMB1 load combination by pressing Apply button. Robotat Polska Sp. The screen will be divided into three parts: the graphical viewer View, the Reactions table and the Diagrams dialog box.
Restore the default attributes of the structure view by clicking the 32! Supports, sections, numbers of nodes and bars and the dimension lines should disappear. If one selects only some of the structure elements in the View window, then, only these elements will be visible in the new window.
Confirm the selection by clicking Apply. Introduce the cursor into the Cases list box upper toolbar and change the load cases by means of keyboard cursors up and down arrows and observe the results in the View window.
If necessary, re- scale the drawing by means of the Normalize button. Leave the default name and confirm by clicking OK. Disable the display of displacements by switching off the Deformation checkbox in the Deformation tab. Confirm by clicking Apply. Check out the Horizontal option in the Diagram Description field of the Parameters tab. Then, click the Open a New Window option at the bottom of the dialog box.
As before, look through the results for all cases – the Case Selection dialog box. Prepare screen captures for the cases with combinations 7: Comb 1. Leave the default name. Close the window with the diagram by means of the Exit button. Set filtering according to load cases in the top left comer i.
Detailed analysis of bars in graphical form Select the Table Columns option from the context menu. Check out the display of RY rotations in the Displacements tab. Confirm by clicking OK. Leave the default name and press OK. The screen will be divided into two parts: the View graphical viewer and the Detailed Analysis dialog box. Check out the Open a new window checkbox at the bottom of the dialog box. Press the Apply button. The currently, opened window is divided into two parts: the top one contains results in graphical form, while the bottom one displays the results in the form of a table.
Activate the display of horizontal descriptions in the Parameters tab click Horizontal in the Diagram Description field. Go to the Division Points tab. Click the NV points along bar length option and type 10 in the field beside. Press Apply. The window with results will display results S max stress values for 10 points evenly distributed over bar length.
Once the Apply button is pressed, the results for the four characteristic points will be introduced into the results window.
Polska Sp. To do so one should click the relative checkbox in the Division points tab. Press the Add button. Go to the Detailed Analysis combo-box and press the Refresh button and then the Apply button.
Go to the window with graphical results and prepare a screen capture with the default name. Close the window by pressing Exit. Preparation of a document for printing 1. The Printout Composition — Wizard dialog box consists of four tabs: — Standard — allows one to add standard positions to the printout composition, ie. The left-hand panel of the dialog box contains elements that may be introduced into the final printout. Clicking a radio button activates one of the four fields: Nodes, Bers, Cases, and Modes.
These results in activation of the following fields: Bars, Cases and Modes. Uneheck all the check boxes, leaving only the following components active: Bars, Loads and forces: values. The tab is divided into two panels. Provides building about Details download- software structural the perform autodesk with structural analysis software more of offers enabling analysis engineers structures- capabilities simulation of for large quickly robot analysis simulation and a variety engineers complex workflow advanced structural professional smooth analysis and a to robot structures-.
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Add to collection. These simple to follow tutorials show how to model and analyze different types of structure, and lead you through the primary workflow used. Virus inside their computer. Autodesk robot structural analysis professional x64 interesting tutorials reliability analysis is a technique used to determine the load when the structure becomes unstable. Those feel stuck in their current job 3. Those want to switch to diff career 4.
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