Laminated glazing thermal, especially for cockpit of aircraft.

摘要

The invention relates to a LUNA THERMAL LAMINATE, ESPECIALLY FOR AIRCRAFT cockpits. MOON comprises at least two sheets of STRUCTURAL GLASS (12, 14) which are fixed in a groove in the cockpit and are joined by a first layer interlayer (16) transparent plastic material, at least one third SHEET GLASS (18), unattached SLOT AND THAT IS ATTACHED TO THE SHEET GLASS STRUCTURAL (14) EXTERIOR by a second interlayer (20) of plastic material, and conducting means CAPA FINA (6) arranged between two BANDS BROUGHT POWER (28) which are connected to a power source, wherein said means CONDUCTORES (26) ARRANGED IN THE THICK OF THE MOON, outside the set of two glass sheets STRUCTURAL (12, 14) , SIDE FACING OUTSIDE THE CABIN.