Aeronautics and astronautics – Landing gear – Wheel
Patent
1991-02-11
1992-09-08
Barefoot, Galen
Aeronautics and astronautics
Landing gear
Wheel
25022715, 340550, 301 63DS, B64D 4500
Patent
active
051451271
ABSTRACT:
To monitor for the formation of a crack in a metal wheel such as that of an aircraft tire and wheel assembly the wheel is provided with an optical fiber arranged to extend no-rectilinearly in a position of the wheel surface selected to be preferential for the development of a crack; preferably the preferential region for crack development is the tire bead seat region and the optical fiber is arranged to extend non-rectilinearly around the circumference of the tire bead seat region thereby to lie interposed between the wheel and tire.
REFERENCES:
patent: 3707270 (1972-12-01), Laimins
patent: 3712680 (1973-01-01), Hyland et al.
patent: 4367460 (1983-01-01), Hodara
patent: 4538527 (1985-09-01), Kitchen
patent: 4603252 (1986-07-01), Malek et al.
patent: 4629318 (1986-12-01), Malek et al.
patent: 4692610 (1987-09-01), Szuchy
patent: 4808814 (1989-02-01), Hofer et al.
patent: 4812645 (1989-03-01), Griffiths
Barnes Raymond H.
Lee Nicholas R. P.
Wells Trevor C.
Barefoot Galen
Dunlop Limited a British Company
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