The invention discloses an aeronautic glass formula. The aeronautic glass formula comprises the
raw material components: in percent by
mass, 55-65% of SiO2, 15-25% of Al2O3, 10-15% of Na2O, 1-5% of Li2O, 1-5% of MgO, 1-3% of K2O, 1-3% of P2O5, 0.5-3% of Bi2O, 0.5-2% of TiO2 and 0.05-0.3% of Cl2, uniform mixing is performed, and melting is performed in a
smelting furnace at a temperature of 1600-1650 DEG C. Meanwhile, the invention discloses a preparation method of the aeronautic glass. The preparation method comprises the following steps: (1) weighing the raw materials accurately, (2), introducing SiO2 by using ultra-white
quartz sand, introducing Na2O by using soda ash and
sodium chloride, introducing MgO by using heavy
magnesium carbonate, and performing mixing with Al2O3
powder, Li2O
powder, P2O5
powder, Bi2O powder and TiO2 powder, and performing uniform stirring; and (3), putting the mixture obtained in the step (2) into a
glass melting furnace; and (4) completing annealing and molding in an annealing furnace. The formula is reasonable, the whole quality,
mechanical strength and
chemical stability of the glass can be ensured, and enlargement of the application range of the glass is facilitated; and meanwhile, the
processing method is beneficial to improvement of the
processing efficiency.