Wear resisting sleeve system for aircraft landing arresting...

Aeronautics and astronautics – Retarding and restraining devices – Friction brakes

Reexamination Certificate

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Reexamination Certificate

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06981673

ABSTRACT:
The aircraft landing arrest cable has wear resisting sleeves positioned thereon in spaced relation to each other to thereby hold the cable out of contact with a non-skid landing surface in a lowered position of the cable. Stresses imposed on the cable when engaged by a tail hook suspended from aircraft during landing, are absorbed by the wear resisting sleeves which are held clamped in positions on the cables by fluid adhesive previously injected into the sleeves. The wear resisting sleeves are respectively formed from pivotally connected sleeve sections made of an impact shatter-proof and durable material such as polyurethane with abutting edges held in contact with each other under a clamped condition of the sleeves on the cable, established by the injected adhesive.

REFERENCES:
patent: 3010683 (1961-11-01), Cotton
patent: 3179358 (1965-04-01), Schlegel
patent: 3615960 (1971-10-01), Hoshii et al.
patent: 3670997 (1972-06-01), Fonden et al.
patent: 3799477 (1974-03-01), Carnevale
patent: 4328394 (1982-05-01), Aloisio et al.
patent: 4660183 (1987-04-01), McGowan et al.
patent: 4738504 (1988-04-01), Jones
patent: 5207302 (1993-05-01), Popp et al.
patent: 6131873 (2000-10-01), Blazon et al.
“Carrier: Powerhouse of the fleet”, Mar. 29, 2004 from http://www.chinfo.navy.mil web site.

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