Frangible fitting assembly

Pipe joints or couplings – Safety release – With frangible or deformable element

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Details

285 3, 285 4, 285304, 403 2, F16L 3500

Patent

active

051452138

ABSTRACT:
A frangible fluid conduit fitting particularly suitable for servicing aircraft wherein the fitting is attached to an aircraft service bulkhead coupling. The fitting consists of two parts, one attached to the supply hose and the other attachable to the bulkhead coupling. The fitting parts are maintained in a sealed assembly relationship by a frangible connector having two separate frangible sections. One frangible section fracturing and releasing the fitting parts under excessive bending forces while the other frangible structure releases upon excessive tension forces being imposed upon the fitting.

REFERENCES:
patent: 3719194 (1973-03-01), Anderson et al.
patent: 4090524 (1978-05-01), Allread et al.
patent: 4643216 (1987-02-01), Allread et al.
patent: 4884591 (1989-12-01), Webster
patent: 4898199 (1990-02-01), Morris et al.

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