| abstract |
In a laminated heated plate glass, especially for an airplane cockpit, the plate glass includes at least two sheets of structural glass (12, 14) which are secured in a rabbet of the cockpit and connected to one another by a first intermediate layer (16) made of transparent plastic material, at least one third sheet, made of glass (18), which is not secured in the rabbet and which is connected to the external sheet of structural glass (14) through the intermediary of a second intermediate layer (20) made of plastic, and conducting devices in a thin layer (26) which are arranged between two current input strips (28), which are connected to a source of current. The connecting devices (26) are arranged in the thickness of the plate glass, on the outside of the set of the two sheets of structural glass (12, 14), on the side facing the outside of the cockpit. |