whee wrote:I wonder about building a failure mode into the windows. Something like reduce the edge distance of the holes so that if you kick the window the fasteners tear out. Or oversize the holes so if you kick the window the head of the fasteners pulls through the holes.
If it's a flat panel or slightly curved surface (like a door) it's pretty simple to make your windows where you can apply enough pressure so the material will bow/bend out enough to slip out of a channel and pop out. This is easy to get it constrained to a single direction of force (ie bird strike wouldn't pop it out, but kicking from inside would), and this method is used commonly in non-aircraft engineering situations. If I'm not making sense, I can elaborate more or draw up a diagram or something.
Also - more of a mechanical fuse, but I've seen enclosures built where a bolt is used with a rubber washer. The hole in the panel is larger than the head of the bolt but smaller than the washer diameter. When enough force is applied, the bolt will slip through the rubber washer, or depending on hole size, the washer could slip through the hole in the panel. But like all mechanical fuses, you're adding a failure mode into the system. Can also be done with grommets rather than rubber washers.
For the record, my experience is not with aircraft but other enclosures, and there are likely issues in an aircraft application that I haven't thought of. Hope I'm not just adding to clutter.
-asa
Edit: Both options above are resettable - a very desirable quality of engineered mechanical fuses, but if you're actually using this feature to save your life after a crash, it's not really important.