B10 GeniE Member Plate Code Checking
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Transcript of B10 GeniE Member Plate Code Checking
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DNV SOFTWARE1
Sesam GeniE
DNV Software Sesam
GeniE_CC_Intro_Workshop
Rev. date 12 March 2011
SESAM User Course
GeniE Workshop:A quick introduction to punching shear, member and plate code
checking
To learn new users how to model a structure and apply loads and boundary conditions to do Joint modelling (cans, stubs, cones) and tubular punching shear check
Member code check and re-design
Plate code check based on the PULS standard
The structure and loads are highly fictitious as the main purpose is to give a quickintroduction to modelling and code checking in one simple model that you can model
within a few hours. Program defaults are used for all code check runs
If this is your first exposure to GeniE you should do the tutorial B1-A small introduction toGeniE
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DNV SOFTWARE2
Sesam GeniE
DNV Software Sesam
GeniE_CC_Intro_Workshop
Rev. date 12 March 2011
Program versions
You need GeniE version D5.3-07 or later. This tutorial can be executed fromGeniE.lite except for the plate code checking. If you have the full version of GeniE
your license file must include code checking for beams and plates as well as
structural analysis.
You can recreate this workshop (except the report creation) by making a new
workspace and importing the file B10_in.js. If you want to recreate the structure and
the loads only you can use the file B10_clean.js
Content
1. Start the program Page 3
2. Define section properties Page 3
3. Define material Page 8
4. Define thickness Page 9
5. Define guide plane Page 10
6. Define upper elevation Page 12
7. Define the vertical columns Page 22
8. Define the lower deck Page 23
9. Model the tubular joints Page 28
10. Add boundary conditions Page 33
11. Define the loads Page 34
12. Define mesh settings and run analysis Page 39
13. Look at results Page 40
14. Code checking Page 42
15. Make a report Page 48
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GeniE_CC_Intro_Workshop
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1. Start the program, create a new workspace (File|New Workspace) and name it Test.Let the units be in N and m.
2. Start by defining section properties. For this tutorial you will need the followingsection types:
L-profiles: Jap_L150x90x9x9, Jap_L200x90x9x14 & Jap_L250x90x10x15
T-bar: Tbar425x120x12x25 & Tbar630x150x12x30
I-bar: HEA140A, HEA200A, HEA240A
Pipe OD406.4x10, OD508x10, OD610x10, OD813x10
All the sections can be imported from the section library.
To import the L-profiles:
Click Create/Edit Section
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Sesam GeniE
DNV Software Sesam
GeniE_CC_Intro_Workshop
Rev. date 12 March 2011
Click Section Library Click Browse
Select anglebar.xml and clickopen
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Browse until you find the sectiontypes
Jap_L150x90x9x9
Jap_L200x90x9x14
Jap_L250x90x10x15
and click OK
You can select all three in one
operation by using ALT+CLICK
Click OK
There are now three sections in
your section library
You can look at and edit the
details by selecting one of them,RMB and choose Edit (Do not
modify if you want the same
results as in this tutorial)
Click OK
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Repeat the same process for the other profiles.
For the T-bar you find the profiles in
Tbar425x120x12x25 & Tbar630x150x12x30
For the I-profiles you find the details in
HEA140A, HEA200A, HEA240A
For the tubes you find the sections in
OD406.4x10, OD508x10
OD610x10, OD813x10
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You should now have thefollowing sections:
You can also view, modify and create new sections from the browser
Click Save
Select a section type, RMB &
Edit to modify a section
Right click the folder Section
to insert a new section
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3. Define a material S235
Either define the material fromEdit>Properties>Material or From browser as shown:
Add the details as shown
Right click the
folder Materials
Click OK
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4. Define a thickness Th15 (15mm) for the upper deck
Either define the material fromEdit>Properties>Thickness or From browser as shown
Add the details as shown notice that the units are given in mm
Click Save
Right click the
folder Thicknesses
Click OK
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5. Define a guide plane for the definition of the upper deck
Insert > Guiding Geometry > Guide Plane Dialog
Give it a name and fill in the details as follows
Click OK
1. Set the elevation to 10m
2. Modify P2, P3 and P4 as shown
P1, 0, 0, 10
P2: 15, 0 , 10
P3: 15, 15, 10
P4: 0, 15, 10
3. Modify u and v as shown
u spacings: 15
v spacings: 3
4. Click OK
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You should now see the guide plane in the graphics window
Remember that the display mode should be set toDefault Display
If you still dont see the guide plane,click on fit to screen (or F9)
If you want to switch from colour background to white background do soby ALT+B or from View > Options > General
In the following all graphics are shown with white background
Click ALT+B
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6. Define the upper elevation built up from L and T profiles and a plate thickness
Start by defining defaults From the browser Sections select the profile Jap_L250x90x10x15, RMB and
set as default
You can see that this is the default section from theBrowser
Pulldown menu
Set the material S235 (from browser materials) and thickness Th15 (frombrowser Thicknesses) to default
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Insert the L-profiles frtom the menuInsert > Beam > Straight Beam
Move the cursor over the guide plane until you see that it prompts you with the
number 1 and Click. This means that you have now selected the start point of the
beam and GeniE is now waiting for the end point.
Click
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Move the cursor over the guide plane until you see that it prompts you with the
number 2 and Click. You have now inserted the first beam
The beam can also be found
in the browser for any type
of manipulation
ClickClick
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Select the beam (click on it), then right click the selection and choose Copy
Use a vector of (1, 0, 0) and do a multiple copy of 13. The preview is shown
There are now 14 beams
Click Apply
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Modify the selected beams (Bm5 and Bm10) to section profile Tbar425
Select the beams, Right Click and choose Properties
Select Tbar425 and click OK
Bm5 and Bm10 have nownew section propertiesassigned
Properties can also be changedfrom the browser by choosingthe new section, right click andApply Section to Selection
Click OK
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Insert beams at the outer boundaries of the upper deck
Select beam Bm10, RMB and select copy
Use translation vector (5, 0, 0)
Repeat the copy by using a translation vector (-10, 0, 0)
Click Apply
Click Apply
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Insert beams at the outer boundaries of the
upper deck
Change the default section to Tbar630
Then insert beams as shown
E.g. fromInsert -> Beam > Straight Beam and click start and stop
Insert the plate fromInsert > Plate > Flat Plate Dialog and click on the four corner
points as shown
1
2
3
4
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The final modelling task for the upper deck is to flush all beams below the deck
Select the set Upper-deck from the browser Utility Sets In the graphics window right click (RMB) and select Edit Beams
Select 1. Offset Vector, 2. Align Section and 3. Flush top
All beams now receive eccentricities based on their section properties
1
2
3
Click OK
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The picture below is shown using the display settings
Modelling Transparent
The following picture includes colour coding of the section properties
Hint: Make the picture, right click on the sections (from the browser) andselect colour coding
To remove colour coding from the graphics click the paintbrush button
Click Save
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7. Insert the vertical columns
Change default setting to OD610 Start inserting a vertical column byInsert > Beam > Straight Beam
1. Click in the field above (End 1)
2. Click in the graphical window to find the start position
3. Click in the field above (End 2)
4. Click in the graphical window to find the x and y coordinates of the endposition
5. Subtract 10 m from the z-coordinate
6. Copy the highlighted tube to the threeremaining corners
1
2
3
4
5
6
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8. Define the lower deck
Change default setting to HE240A The lower deck elevation is at +2.5 m and a temporary snap plane will be used to
define snap points along the columns at elevation +2.5 m
1. Start by clicking on the arrow next to the symbol for snap perpendicular
2. Select the Snap plane option
3. Make sure the Snap Plane symbol is activated (pushed in) and type in thez-elevation 2.5 m.
4. Start inserting beams graphically. Make sure that the insert beam button isactivated (ticked off) and that the snap point is also activated.
1
2
3
4
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You can now insert the beams by clicking at the snap points as defined in the
intersection between the columns and the temporarily snap plane
The first beam is defined by clicking as shown below.
The second beam is also defined in the same manner
The two remaining beams between the columns are inserted in the samedirections as the previous beams
1
2
1
2
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Create the inner parts of the lower deck by
1. Copy the selected beam 2 times with a vector of (5,0,0)
2. Copy the selected beam (Bm28) 14 times with a vector (0, 1, 0)
3. Select all the beams in the lowerdeck, RMB and chooseNamed Set.Make a new named setLower_deck andinclude the selection
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4. Change the section properties of the below selected beams to HE140A
5. Finally, modify the sections of the selected beams to HE200A
6. Select all the beams in thelower deck, RMB and selectEdit Beam. Perform a flushoperation from the offsetvector tab
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A detailed view of the lower deck may be (seen from below):
Click Save
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9. Model the tubular joint part
1. Start by changing the default section to OD406. Insert the beam as shown belowby using a snap plane at elevation 6.25m. See previous pages on how do it
2. Insert the bracings in the sequence (1-4) as shown below
1
2 + snap plane at el. 6.25m
1
2
4
3
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3. Define joints for use in joint design. A joint is inserted from
the joint button or fromInsert > Joint > Joint Dialog
Insert two joints as shown below. To be able to see
the joints the symbol for joints needs to be activated
4. Perform the joint design by selecting the joints, RMB and choose Add Can/Stub
This example is based on using the default values as given underEdit >Rules > Joint design
Each joint willnow have bothcans and stubs
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From browser Properties Reinforcement click on AutoCan, RMB and chooseSelect Objects. Modify the selected cans so that they receive section property
OD813.
The structure should now look as
Repeat the process above for the cans and modify the sections of these toOD508 for stubs
12
3
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The structure should now look as
Add conical transitions by selecting the joints and the connected cans and stubs.
Make sure that the joint symbol for selection is activated and that the select beam
filter is set to Filter Segment.
You can do a rubber-band select to include the joint and
the cans & stubs. Right click and select Add Cone to selected beams/segments
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The structure should now look as (remember to setthe beam filter back to default)
Finally, perform a gap calculation by selecting the joints (remember that youneed to activate the Joint selection button), RMB and select Add Gap. Thestructure looks like:
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10. Add Boundary conditions
Insert boundary conditions from the support button Click at the ends of each column to insert a
support
Modify the two highlighted support points (select them, RMB and Properties) sothat they are free to move in Dx, Dy, Rx, Ry and Rz
Click Save
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11. Define the loads
There will be a total of 6 loadcases for this example there are 5 basic load casesand 1 load combination
1. Selfweight
2. X_acceleration
3. Upper_pressure
4. Equipments_U_deck
5. Equipments_L_Deck
6. Combo (a combination of 1-5)
Start by defining the load case names
fromInsert > Load Case
The load combination is defined from
Insert > Load Combination
The load cases can be modified from the browser Analysis Load Cases
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Selfweight
Select the load case Selfweight, RMB and click properties. Make sure youtick off for Include structure selfweight in structural analysis. Theacceleration is the same as gravity
X-acceleration
Modify this load case by ticking off for Include structure selfweight instructural analysis and modifying the acceleration vector to Vector3d(1m/s^2,0 m/s^2,0 m/s^2)
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Upper_pressure
From theInsert > Explicit Load > Surface Loaddefine a pressure of -5 KPato the plate of the upper deck.
Before you do so, select the load case Upper_pressure, RMB and Set current.
Click on each plate corner to fill in the co-ordinate values and specify theintensity to -5KPa.
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Equipments_U_deck
Select the load case Equipments_U_deck and set it to current. Define the equipments Box1 and Pump1 fromInsert > Equipment > Prism
Equipmentas follows:
Place the equipments in the load case as follows:
From the folder Equipment, select Box1, RMB and choose Place inLoadcase. Drag the equipment to a temporary position, select it and chooseProperties. Type in the exact coordinate values of the position of the
equipments bottom centre (11, 2, 10).
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Place the equipment Pump1 in the same way as described on the previouspage, but the coordinate values of the bottom centre shall be (3, 10, 10).
The load-case shall now look like
Equipments_L_deck
Select the load case Equipments_L_deck and set it to current.
Define the equipment ToolBox1 and place it in the load case at the followingposition (8, 7.5, 2.5). Use the techniques as described on the previous pages.
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12. Define mesh settings and run analysis.
Specify one mesh setting Md_plate = 1m and apply to the plate. From browser Properties Mesh you
define the new mesh setting
Apply this mesh setting to the plate
in the upper deck
Before analysis you should check the model from Tools > Structure > Verify.
The analysis is started from Tools > Analysis > Activity Monitor(or ALT+D). This
will set up Analysis 1 and by clicking on OK you can start the analysis
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13. Look at results. This tutorial includes 2 examples on post-processing
Global deformations Change the view settings to Results with Mesh and set the load case Combo
to current.
Most likely you see the mesh, but not any results. From the Tools > Analysis> Presentation (ALT+P) you define which result attribute to view.
You should check out the other options to present results from the Tools >Analysis > Presentation
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Beam stresses
Change the view settings to Modelling Structure. Select the beam(s) you want to compute the forces on
Start the beam computation from Tools > Analysis > Beam Force/StressDiagram
In the example below the axial stresses of Bm18 are computed (a Tbar 630profile) for the load combination Combo for hotspot 8.
Click on the tab Graphs to see the diagram.
If you run analysis with 2nd order elements the diagram becomes moresmooth.
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14. Code checking
There are three examples in this tutorial. They are meant as a quick introduction for more details you should consult the other relevant tutorials or the User manuals.
Member code checking
1. From browser Capacity insert anew Capacity Manager
2. From the folder Capacity CC_Member you create the members as shown
3. From the folder Capacity CC_Member you add a run as shown (defaultsettings are used for the code check run)
You should check out the options of modifying the code checkparameters
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4. From the folder Capacity CC_Member you compute the code check forcesfor a run as shown
5. From the folder Capacity CC_Member you perform the code check.
6. From the folder Capacity CC_Member CC_Member(run1) you can look atresults
Alternatively from the viewsetting Capacity Models.Select all members, RMB,Color Code, Results, UfTot
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Tubular punching shear check
1. From browser Capacity insert anew Capacity Manager
2. From the folder Capacity CC_Joint you create the joints as shown
3. From the folder Capacity CC_Joint you add a run as shown (defaultsettings are used for the punching shear check)
You should check out the options of modifying the code checkparameters
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4. From the folder Capacity CC_Joint you compute the code check forces(default settings are used for the code check Capacity Manager)
5. From the folder Capacity CC_Joint you perform the code check.
6. From the folder Capacity CC_Member CC_Member(run1) you can look atresults
Alternatively from the viewsetting Capacity Models.Select all members, RMB,Color Code, Results, UfTot
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PULS Plate code checking
Un-stiffened panels
1. From browser Capacity insert anew Capacity Manager
2. From the folder Capacity CC_Puls you create the panels as shown
3. From the folder Capacity CC_Puls you add a run as shown (default settingsare used for the plate code check)
You should check out the options of modifying the code checkparameters, e.g. if you want to run for stiffened panel
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4. From the folder Capacity CC_Puls you compute the code check forces(default settings are used for the code check Capacity Manager)
5. From the folder Capacity CC_Puls you perform the code check.
6. From the folder Capacity CC_Member CC_Member(run1) you can look atresults
Alternatively from the viewsetting Capacity Models.Select all members, RMB,Color Code, Results, UfTot
Click Save
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15. Make a report
Generate a report that includes some content for the structure, the loads and all thecode checks. This is just an example so you should test out the other chapters. The
chosen format is a MS Word report, but you can also test out a plain text file, html or
MS Excel.
From the File > Save Report
1. Give it a file name (e.g. This_is_a_file)
2. Give it a report name, this will be in the report heading (e.g. B10)
3. Select report format (e.g. WordXML)
4. Click on Structure 5. Click on Add Selected
1
2
3
4 5
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15. Make a report
6. Click on Report 7. Click on Loads
8. Click on Add Selected
9. Click on report
10. Click on Frame Code Check
11. Click on Add Selected
12. Select Capacity Manager to CC_Member, add lower limit forUfTot to 0.5 and modify the Chapters as shown below
6
7
8
9
10
11
12
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GeniE_CC_Intro_Workshop
Rev. date 12 March 2011
15. Make a report
13. Click on Report 14. Click on Frame Code Check
15. Click on Add Selected
16. Select Capacity Manager to CC_Joint, add lower limit for UfTot to0.2 and modify the Chapters as shown below Click on report
17. Click on Report, Plate Code Check, Add Selected, set CapacityManager to CC_Puls, and use lower limit 0.3
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7/28/2019 B10 GeniE Member Plate Code Checking
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Sesam GeniE
15. Make a report
18. Click on Save 19. Click on View to see the report in MSWord
Click Exit to quit and save File > Exit
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