Cockpit canopy shattering system for escape of airmen

B - Operations – Transporting – 23 – K

Patent

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327/33, 244/96

B23K 9/04 (2006.01) B64C 1/32 (2006.01)

Patent

CA 1061417

ABSTRACT OF THE DISCLOSURE Apparatus for shattering an aircraft cockpit canopy in the path of an ejector seat, wherein the canopy has in intimate contact therewith, preferably embedded therein, a pattern of fusible conductors having at least one region of increased fusibility in each conductor. The conductors are connected via a switch system to a high energy electrical source, the switch system being linked with initiation of an ejection sequence. When ejection is initiated the conductors are fused and the canopy shattered at least in the path of the ejector seat.

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