Frameless aircraft canopy actuation system and method

   
   

An apparatus and method for attaching an injection-molded canopy to a hinge assembly is provided. The apparatus includes attachment components that are at least partially embedded in the injection-molded canopy. A hinge assembly attaches to the attachment components for controlling the position of the canopy. The canopy is a polycarbonate or acrylic frameless canopy. The hinge assembly is hingedly attached to the vehicle. The hinge assembly includes a center support and port and starboard supports. The center support is located approximately along a centerline of the canopy, the port support is located on a port side of the vehicle, and the starboard support is located on a starboard side of the vehicle.

 
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