EdgeDistance
Aerospace
- Jun 8, 2016
- 2
Hello All,
I am working on an analysis of a simple antenna on a pressurized aircraft. This is a XPDR antenna, external doubler, double row of rivets all around, pretty straight forward.
Where I am getting hung up is figuring the end fastener rivet loading. What I am seeing is this could be an example of an "idealized strip" where at fully developed limit load the end fasteners carry the most load, making the corner rivet the critical fastener.
It seems to be tribal knowledge that "the end fastener load is lass than 30% of the total load"
Can any one explain this to me so I can add sufficient explanation in the analysis?
Or is there a better way to explain the corner critical rivet in this explanation?
Thanks all
I am working on an analysis of a simple antenna on a pressurized aircraft. This is a XPDR antenna, external doubler, double row of rivets all around, pretty straight forward.
Where I am getting hung up is figuring the end fastener rivet loading. What I am seeing is this could be an example of an "idealized strip" where at fully developed limit load the end fasteners carry the most load, making the corner rivet the critical fastener.
It seems to be tribal knowledge that "the end fastener load is lass than 30% of the total load"
Can any one explain this to me so I can add sufficient explanation in the analysis?
Or is there a better way to explain the corner critical rivet in this explanation?
Thanks all