Canopy mosaic thermal barrier

Aeronautics and astronautics – Aircraft structure – Details

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Details

244121, 244117A, 428 49, 428 46, B64C 114, B32B 700

Patent

active

043890300

ABSTRACT:
A heat resisting canopy which utilizes a mosaic overlay of quartz or heat resisting glass elements adhesively bonded to a transparent organic shell. A transparent adhesive bonds each mosaic element to the organic canopy shell. A plurality of metallic ribbons, egg-crated together to form a lattice, stabilizes the mosaic structure, and individual elements are retained by a metallic wire mesh which covers the mosaic layer and which is attached to the canopy shell.

REFERENCES:
patent: 2319534 (1943-05-01), Crowley
patent: 2464826 (1949-03-01), Nehes et al.
patent: 2939186 (1960-06-01), Norwood et al.
"Thermal Protective Coatings", Perry et al., Mar. 31, 1976, Report No. U-3.

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