WARose
Structural
- Mar 17, 2011
- 5,594
I've been handed the task of designing a new crane runway girder. This will kind of be a open ended thread as I may have more questions as I go. (I haven't done anything like this in about 15 years....so lots of rust.)
For right now, 2 questions:
As far as the lateral load on the runway beam goes.....I seem to recall that you could deal with that as a torsional force in the girder, or you could take care of it by bending in the cap channel + top flange combination. Is that how you do it? That seems to be how they do it in AISC Design Guide 7.
In CMAA 70, among the loads, the following statement is made:
"The twisting moment due to the starting and stopping of bridge motors shall be considered as the starting torque of the bridge motor at 200 percent of full load torque multiplied by the gear ratio between the motors and cross shaft."
I have no clue how to get a load out of that....does anyone know what that means?
For right now, 2 questions:
As far as the lateral load on the runway beam goes.....I seem to recall that you could deal with that as a torsional force in the girder, or you could take care of it by bending in the cap channel + top flange combination. Is that how you do it? That seems to be how they do it in AISC Design Guide 7.
In CMAA 70, among the loads, the following statement is made:
"The twisting moment due to the starting and stopping of bridge motors shall be considered as the starting torque of the bridge motor at 200 percent of full load torque multiplied by the gear ratio between the motors and cross shaft."
I have no clue how to get a load out of that....does anyone know what that means?