This caught my eye. Yes, I realize there are a lot of whack patents out there but it raises a question for me. What are the factors limiting window size on commerical jets? With cockpit windows, redundancy has been a factor (you get cracks or failure one the CPT's panel and you still have the FO's panel intact (this has happened). It appeared that early A350 designs incorporated a one-piece wrap-around panel but later gave way to multiple panels with the rather lame 'raccoon-eyes' compromise. Airbus also wanted much larger pax windows but later made them more conventional. I've always assumed these windows are kept small to prevent a passenger being ejected if one should fail.
Now here is a company proposing to put a huge, one-piece plastic canopy on top of the pressure hull. What if it fails? What are the restrictions on this?
Now here is a company proposing to put a huge, one-piece plastic canopy on top of the pressure hull. What if it fails? What are the restrictions on this?
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