Aircraft transparency having chemically tempered...

Stock material or miscellaneous articles – Surface property or characteristic of web – sheet or block – Surface modified glass

Reexamination Certificate

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C428S409000, C428S426000, C428S428000, C428S432000, C501S055000, C501S063000, C501S065000, C501S066000, C501S067000, C501S068000, C501S069000, C501S070000, C501S072000

Reexamination Certificate

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08062749

ABSTRACT:
An aircraft transparency in a glass piece, wherein the glass piece includes a chemically tempered first major surface and a chemically tempered opposite second major surface, a first case depth begins at the first major surface, a second case depth begins at the second major surface, and a tensile stress zone is within the glass piece between the end points of the first and the second case depths. The glass between the end points of the first and second case depth has a glass composition including:IngredientPercent by weightSiO260 to 75;Al2O318 to 28; andLi2O3 to 9, andthe glass has at least one of the following properties (a) a log 10 viscosity temperature of at least 1413° F. and (b) a liquidus temperature of at least 2436° F.

REFERENCES:
patent: 3357876 (1967-12-01), Rinehart

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