LSPSCAT
Structural
- Dec 19, 2007
- 123
See attached sketch of simple frame in a single plane. No other support is provided out of plane. Frame is part of machine equipment with force applied to the horizontal framing member that acts bidirectional in the vertical direction. Magnitude is 100,000 lbs. Now for basic analysis in analyzing frame it is assumed as a non-rigid to determine loads in the main horizontal member and columns. Beam is designed as a simply supported member. The beam is connected to the frame with a 4-bolt fastener group and fasteners are designed based on loading in pure tension.
Now, for stability the frame is checked as a semi-rigid frame and the connections are then check based on the applied moments at the joints. The connection from the vertical column to the horizontal framing member is then checked for the tensile loading from the applied vertical load and for the moment that is developed from any out-of-plane applied forces. For stability loading, between 2% and 5% of the vertical load is applied both in plane and out of plane to the top horizontal member in conjunction with the vertical live load.
Bolting is required for assembly and disassembly. No welding allowed. Bracing is not really an option due to overall configuration.
Second question:
If the 4-bolt fastener group was replaced by a single line of fasteners should it be assumed that no moment can be transferred or would I be able to base the fastener loading on prying action based the geometry of the faying surfaces.
Just working through this and I am mainly concerned about the stability of the frame out of plane.
Now, for stability the frame is checked as a semi-rigid frame and the connections are then check based on the applied moments at the joints. The connection from the vertical column to the horizontal framing member is then checked for the tensile loading from the applied vertical load and for the moment that is developed from any out-of-plane applied forces. For stability loading, between 2% and 5% of the vertical load is applied both in plane and out of plane to the top horizontal member in conjunction with the vertical live load.
Bolting is required for assembly and disassembly. No welding allowed. Bracing is not really an option due to overall configuration.
Second question:
If the 4-bolt fastener group was replaced by a single line of fasteners should it be assumed that no moment can be transferred or would I be able to base the fastener loading on prying action based the geometry of the faying surfaces.
Just working through this and I am mainly concerned about the stability of the frame out of plane.