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  1. simkatu

    Hold Catia open for extended periods using a program?

    I used to have a little executable called "CatiaHold.exe" or something like that. When you had a Catia session open with a license that expires after 30 minutes of non-use and you wanted to hold your particular set of licenses until you returned from lunch in an hour, you could run this little...
  2. simkatu

    Copying multiple part bodies and pasting into a single part.

    I have hundreds of "standard parts" instantiated in an assembly. Now I want to copy all of the part bodies in each of the hundreds of parts and paste them all into a single detail part that will act as a collector for the parts. I have not been able to find a way to select multiple part bodies...
  3. simkatu

    Why do I experience two different behaviors for "Insert --> Geometrical Set"?

    I am actually using the Menu Bar's "Insert --> Geometric Set...", which does have the elipsis at the end of it every time I use it. I don't think the behavior is related to the workbench I'm using because it seems to happen whether I'm in part design, GSD, or aerospace sheet metal. It's just...
  4. simkatu

    Why do I experience two different behaviors for "Insert --> Geometrical Set"?

    In CATIAv5 R19 I often experience two different things when I perform "Insert --> Geometrical Set". Most of time I get the desired behavior, which is the appearance of the "Insert Geometrical Set" dialog box that allows me to enter in the Name, Father, and Features of the set. However, on some...
  5. simkatu

    Sizing for a drag link connecting a wing to a fuselage

    @rb1957 - It is definitely a work problem. I'm designing structure for a small jet airplane and was told by someone in the stress group that I needed to use [9g * mass of entire airplane] as a critical loading case for the drag link. I cannot see how anything in FAR23.561 (crash loads)...
  6. simkatu

    Sizing for a drag link connecting a wing to a fuselage

    I'm trying to determine sizing for a drag link that is connecting an underbelly wing to a fuselage. Assuming that this drag link is horizontal and only transmits loads in the forward and aft direction and assuming this aircraft is to be FAA certified to Part 23 standards for a normal...

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