I need to get normal modes for an electronic board. It is made of FR4 laminate. Does Inventor Professional 2014 supports transverse isometric materials in a modal analysis?
View 6 RepliesI have an app that uses a paletteset. The paletteset displays a modal dialog on a particular action. From the modal dialog, the user needs to be able to click a button to zoom to a particular coordinate. I have it all working, with one problem. The Zoom doesn't occur until the user closes the modal dialog. I know this is related to my limited understanding of contexts in AutoCAD.
I've tried calling my Zoom method from the modal dialog, from the parent paletteset, and asynchronously using doc.SendStringToExecute() back to my main commands class, with the same result. The Zoom occurs after exiting the modal dialog. How I can make the zoom occur while remaining in the modal dialog?
I'm trying to load a modal dialog, at the first loaded/created drawing. How can i find out when autocad is done with loading to activate the form. I have event handlers for document created but it gets called to early.
View 1 Replies View RelatedI`m trying to determine will Inventor satisfy the needs that I`m having regarding simulation options. So I started with some elementary stuff.
If it is possible in stress analysis to manually select which degrees of freedom body has.
"Fixed constraint" block all 6 DOF and I would like to block only transitional DOF so that I keep rotational degrees of freedom?
Is it possible to refresh drawing content when modal form is running?
I placed sample project in attachment.
There is simple form with only one button.
Private Sub Button1_Click(sender As System.Object, e As System.EventArgs) Handles Button1.Click Class1.DrawLineOnScreen() End Sub
After button is pressed, application prompting user for picking 2 points, and draw a line (based on picked points).
Public Shared Sub DrawLineOnScreen() Dim editor As Editor = Application.DocumentManager.MdiActiveDocument.Editor Dim pFirst As PromptPointOptions = New PromptPointOptions("First point: ") Dim rFirst As PromptPointResult = editor.GetPoint(pFirst) Dim pSecond As PromptPointOptions = New PromptPointOptions("Second point: ") Dim rSecond As PromptPointResult = editor.GetPoint(pSecond) If rFirst.Status = PromptStatus.OK AndAlso rSecond.Status = PromptStatus.OK Then Dim line As Line = New Line(rFirst.Value, rSecond.Value) Dim tr As Transaction = Application.DocumentManager.MdiActiveDocument.TransactionManager.StartTransaction Using tr Dim modelSpace As BlockTableRecord = tr.GetObject(Application.DocumentManager.MdiActiveDocument.Database.CurrentSpaceId, OpenMode.ForWrite) modelSpace.AppendEntity(line) tr.AddNewlyCreatedDBObject(line, True) tr.Commit() End Using End If End Sub
Problem is that line had been added to transaction (to Model Space block table record) but nothing change on a drawing. Line will appear on a drawing after closing the form.
In opposite situation, without using modal form (only console) everyting works fine.
<CommandMethod("DrawLine", CommandFlags.Modal)> _ Public Sub DrawLine() Class1.DrawLineOnScreen() End Sub
I have created a report from a frame analysis of an arrangement of I-Beam steelwork. I need to check that I have placed the nodes in the right order and this is reflected in the results of the report. I have the parent and child nodes connected at the ends of the beams as shown on the attached screen shot. I'm interested to know if the order in which I have selected the nods makes any difference to the results. There a 3 node connection points at each corner section.
View 3 Replies View RelatedI have purchased the Autodesk Product Design Suite Premium. It comes with the Frame Generator but does not seem to have the Frame Analysis with it. Is that provided in other Suites or should I have it??
View 1 Replies View RelatedI am trying to simulate the following:
I have an 8" OD/5.523" ID steel tube. A 5.5" OD/4.957"ID tube is placed inside. The 8" and 5.5" tubes are placed over a 4.9375"OD shaft. So basically you have a hollow shaft attached to a drive shaft, with a filler tube placed between them to fill the gap. Two 1-1/2" UNC bolts are placed in matching1.531" diameter holes in every component (thru bolted) with a nut. Tightening the nut will tend to flatten the pipes, taking up the clearance between then and creating a contact pressure on the drive shaft. I have having trouble getting all of the contacts correct since the components are not in contact at the beginning of the simulation due to the radial clearances.
Two axial bolt loads of 129,000 lbs will be placed on the tubes. I have used a sliding/no separation contact between the bolt and nut. Then I put a fixed constraint on the bottom face of the nut (not in contact with the tube) and put a 129,000 force on the top of each bolt head to simulate the axial load created by the bolt preload. What type of contact should I use between the tubes that have radial clearance?
I have attached the tubes and drive shaft. The 1-1/2" bolts and nuts (both heavy hex) were found in the library.
How to set up a symmetric stress analysis?
I read about using symmetric analysis on a symmetric assembly, but no description of how it is done.
I am trying to properly stress test a steel aircraft fuselage. I can easily model the estimated weight of the pilot, copilot, etc as loads on the airframe. However, when it comes to simulating a high-G situation, (a load factor of around 7.5 times the force of gravity), I am not sure what to do. On one hand, I can simply multiply the loads on the airframe by the load factor and see if the frame can take it. In most cases, it performs very poorly, (safety factor less than 1). However, if I model all the loads under normal conditions, (normal pilot weight, etc.), then add a gravity load equal to 7.5 G, the airframe performs well. Yet I am not sure if the loads on the airframe, (such as pilot weight), are being adjusted along with the increased gravitational load.
My question is, what is the best way to accurately simulate real world loading for high-G situations?
I am doing an eigen frequency analysis of a structure in the range of 0 to 1500 Hz. For my structure I am getting about 6 modes as expected.
For the final results I will mass normalize to convert to an energy based on the relative "displacements" However, each of the "displacements" for the 6 eigenfrequencies are the same?
I know this can not be right as it would mean that all have the same energy which is impossible.
I am trying to determine how to properley constrain the assembly below, so that the compression of the rubber gasket will be properly indicated.
Currently I am seeing the deflection of the shelf in the downward direction, but I do not see any indication of stress in the gasket behind.Currently the gasket is "bonded" to the steel tube the screws are bonded to the shelf bracket and the steel tube.
I put in "work axis" at the center line of the shelf bracket and the CL of the gasket, but I can't find a way to constrain to a work axis.The file is too large to upload here...
inventor 2012
64 bit machine
12gig ram
and it says I don't have enough memory! How can this be? Its not that complicated of an assembly. I have done bigger. I excluded all the part I'm not using and they are all basic plate and tube parts. There are less than 20 parts in the assembly.
How can do the thickness analysis in autodesk inventor like solidwiorks thickness analysis, it show the thickness of the part in point to point
View 1 Replies View RelatedI have used a few times 'Stress analysis' before. Today I discovered it is disabled. I applied a software update (SP1, build 222), after which I could run a Stress analysis again. However, Inventor crashed soon, and after restarting it, Stress analysis is disabled again. In 'Add-In Manager' the 'Simulation: Stress analysis' is shown as 'Automatic/Loaded'.
UPDATE: I have unchecked the 'Load Automatically' option for this module, quit Inventor, started it again, loaded the module and now it seems to work. I don't know yet for how long...
UPDATE2: well I could start a Stress analysis, but everything is disabled there, I can not create a simulation for example.
I am trying to run a simulation on a 4 layer part that has two base layers of I-beams, a frame I made in the frame generator (below) and a solid sheet on top. I am having some issues with the FEA side and was curios to see if the frame analysis tool would yield the same results as the stress analysis simulation. For the frame generator I saw 4 times the amount of deflection despite using (what I believe) are similar loading and constraints, however now I am unsure if I can trust to run an FEA simulation with a frame generated component. The frame is made up of 2 inch steel box beam with a 0.25 inch wall thickness. For the frame analysis package, I have applied a pressure that equates to a 70 kN load across four different sections of the frame. Supports have been placed under all four corners, with 1 being fixed and the other 3 free to move. For the FEA simulation, I applied a similar pressure by creating 2 inch wide plates and applying the same pressure at the same four points. There are also 2 inch square pads under the four corners of the frame with one edge of one pad being fixed and the bottom of the pads having a frictionless constraint. There are separation contacts between both the pressure plates on top of the frame and the frame as well as between the pads and the frame.
with the frame generator is that all the segments of the frame are bonded together (under contacts) which makes sense since they are welded together. However when I put a sheet on top of the frame, there are 3 contact points created between each beam on the frame and the sheet (one on the face of the frame that is in contact with the sheet and the other two on the rounds of the frame and the sheet, even though the rounds are not actually in contact with the sheet). Either way, I am seeing deflections of less than 0.1 mm when a 70 kN load is applied which I know is not right and just want to know if using a frame generated component is not possible with an FEA simulation.
I have just installed Inventor 2012 on a clients machine and the stress analysis tab is missing.
View 2 Replies View RelatedWe just migrated from Inv 2011 where I had set the letter A as a shortcut for Zoom All. I tried setting it up again and ran into an issue where two commands were tied to it with the other command being Interference Analysis. I can't find interference analysis in the keyboard customization section and am wondering if there is a way to get rid of it's association with the letter A.
View 5 Replies View RelatedI work for a tank building company and we are starting to use Inventor for stress analysis. We have a tank that we are designing that has a tank inside of another tank. The internal tank will be holding product while the outside tank is there to prevent product leakage in the event that the internal tank has a leak. There is piping that is welded to both the inside tank and the outside tank.
So here's my question: We know the radial deflection of the piping on the internal tank due to pressure, but we want to know what the stress is going to be on the external tank shell. Is there a way that I can input the amount of deflection and so that inventor will calculate the stresses involved?
I saw thermal properties in the list of Inventor's materials. However, I didn't find how to make a thermal analysis using Inventor MEF. Is it possible?
View 3 Replies View RelatedSo I have an assembly made up of several smaller assemblies and have constrained them in the main assembly but when I run the analysis, the interaction does not seem to exist.
An image has been displayed below, the pin should line up with the holes.
I've attached file. This is trestle and SWL(safety work load) is 2T. How can understandable that this load is going to be withstand by trestle.
View 6 Replies View RelatedI'm a student working on a team project to build a vehicle and we're required to do a stress analysis to make sure if the vehicle (chassis, supports, etc) can withstand the weight of the driver, etc.
The problem is that the analysis that I did doesn't seem to make any sense at all, like there was no stress between the joints, the frame bent when the applied force was only 5 kg...
The metal used is mild, steel.
Having an assembly, modeled in the frame generator, then with some additional parts (ribs, plates, etc) added to the assembly as parts and constrained with assembly constraints.. which is the best way to do a frame analysis with the frame analysis enviroment for considering the all structure (frame generators parts + the additional enforcing parts) ?
The assembly look like for example, to this (modeled in autocad).
explain the circumstances where 'Release' is applied to a beam (node?) when using the Frame Analysis tool.
View 1 Replies View RelatedI am using Inventor 2009 professional and I have to run a stress analysis on a beam. I put the constraints and the forces I need and when I hit the calculate button, the results so up, but when I click on the results, nothing appears. I need to run this calculation and do not want to resort to hand calculations.
View 9 Replies View RelatedI'm trying to run a simulation on a part to test it's resistance to explosive forces and pressures. All the tutorials I find on stress analysis seem to be grader toward mechanical parts or tables.
View 9 Replies View RelatedWhen I go to Environments>Frame Analysis, I used to get a menu for Constraints, Loads and other settings (similar to the Stress Analyisis menu). I don't get that now. I can right-click on an existing simulation and add constraints and loads, but I would really like to get the menu back.
I can go to tools>Customize, Toolbars tab and Frame Analysis Panel is there. I can click Show and it will show the panel but it stays up all the time. Not what I want.
I have tried resetting the menu, repair installing Inventor and Reinstalling Inventor, but still not joy. How do I get this back to the original setting so that it comes up when I select Frame Analysis?
This is in 2011.
I'm trying to create a report on a stress analysis I've made. Reading the report I don't find any result on safetyfactor. When I was browsing the forum I found a thread concerning safety factor and a report file attached. My report is missing some of the information that I found in this attached report (such as "result summary".
View 2 Replies View RelatedI'm performing a static stress analysis on a benchframe. The benchframe is imported out of a STP file and I assume that's where the problems begin.
When I start the simulation, everything goes well. When I see the results, almost the whole part is blue, and only a really small part in a corner is shown red, with extremely high stresses.
The corner is actually not what I wanted to test, but it is messing up the other visible results because now I have to place probes all over the part to see the stresses (because the colors are calibrated with the high peak).
I have tried working with local mesh control and convergences, but I can't control the results in the small corner. I also tried rebuilding surfaces and adding fillets.
Is it possible to set a maximum stress, so that the other colors are visible in the important areas. It is not possible to exclude the corner from the simulation because it's part of a substantial part.
I am having problems creating a Stress Analysis Report from the Dynamic Simulation on this assembly.
My goal is to show the cam shaft rotating at 3500 rpm, and the stress it creates. I am looking to show the stress concentrations at the fasteners as well as the rotating components, the cam will have a torque of 15 ft lb, with a counter torque of the compressor equal to that.
I have been working through Wasim Younis' Book for Inventor 2014, but seem to be coming up short in its application.
I am using Inventor Professional 2014.
Autodesk Inventor 2013 Certified Professional
Autodesk Product Design Suite, Ultimate 2013