Aircraft windshield system with frangible panel for aircrew emer

Details Aircraft windshield system with frangible panel for aircrew emer Aircraft windshield system with frangible panel for aircrew emer

1993-04-07

1994-03-01

Huppert, Michael S.

Aeronautics and astronautics

Aircraft structure

Fuselage and body construction

244121, B64C 132

Patent

active

052899969

ABSTRACT:
An improved aircraft cockpit canopy for allowing thru-the-canopy ejection of an ejection seat is disclosed. The canopy includes windshield and side sections of transparency panels tough enough to withstand high energy bird strikes and a portion of an overhead section of the canopy made of a frangible transparency panel that will break into small fragments if struck by an ejecting ejection seat. The frangible transparency panel is made thinner than the tougher transparency panel. The frangible transparency panel is held in place by either an elastomeric sealing gasket or by a metal bracket with an elastomeric sealing layer. Both the elastomeric sealing gasket and the metal bracket can be made to bend or break to release the frangible transparency panel when struck by an ejecting ejection seat. The elastomeric sealing gasket and the metal bracket can also absorb the dynamic oscillations of a bird strike elsewhere on the canopy. The improved aircraft canopy can also be made by direct forming, where the area of the canopy through which an ejection seat will exit is made more frangible by modifying the material properties of the transparency at that location, by making the transparency thinner over that area, by scoring the transparency over that area or by a combination of those and other methods.

REFERENCES:
patent: H451 (1988-04-01), Pinnell
patent: 3618881 (1971-11-01), Fellers et al.
patent: 3880387 (1975-04-01), Martin, Jr.
patent: 4570879 (1986-02-01), Dupin
patent: 5085383 (1992-02-01), Larkin et al.

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