Aeronautics and astronautics – Aircraft structure – Fuselage and body construction
Patent
1988-03-21
1990-03-06
Peters, Jr., Joseph F.
Aeronautics and astronautics
Aircraft structure
Fuselage and body construction
2441293, 296201, 296 9621, B64C 114
Patent
active
049059351
ABSTRACT:
An aircraft windshield transparency includes a base frame defining an opening into which an inboard-positioned transparency is mounted with at least one outboard-positioned transparency and an interlayer between the two transparencies. The interlayer exhibits a stronger adhesion to the outboard transparency than to the inboard transparency. The peripheries of the outboard transparency and interlayer carry a means which functions to expose a groove penetrating to the surface of the inboard transparency such that the outboard transparency and interlayer may be removed and the inboard transparency thereafter functions as the primary windshield transparency of the aircraft.
REFERENCES:
patent: 3559928 (1971-02-01), Dohmeyer
patent: 3807791 (1974-04-01), Boyer
patent: 3836193 (1974-09-01), Donahoe
patent: 4020033 (1977-04-01), Dannels
patent: 4204374 (1980-05-01), Olson
patent: 4224436 (1980-09-01), Doss
patent: 4258105 (1981-03-01), Williams
patent: 4267307 (1981-05-01), Louthan et al.
patent: 4725501 (1988-02-01), Rukavina et al.
Germain L. A.
Loral Corporation
Peters Jr. Joseph F.
Sartelle Anne
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