Flexible flow through saddle

Pipe joints or couplings – With strain relief

Patent

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Details

285239, 285175, 403 41, F16L 1304, F16L 3500

Patent

active

049899031

ABSTRACT:
A flexible flow through saddle for ship-to-ship refueling systems. The flble flow through saddle includes a tubular structure having a pair of ribs located on the top and bottom of the tubular structure, each rib having an aperture therein. Extending from each end of the tubular structure and having an end portion thereof connected to the tubular structure is a helical shaped wire. The opposite end portion of each helical shaped wire is connected to a coupling member. That portion of each helical shaped wire between the coupling member and the tubular structure is encased in an elastomeric material which provides for flexibility and prevents premature fatigue and rupture of a hose element connected by the coupling member to the tubular structure through the encased helical shaped wire.

REFERENCES:
patent: 933516 (1909-09-01), Witzenmann
patent: 1371981 (1921-03-01), Rose
patent: 2185741 (1940-01-01), Sorg et al.
patent: 2700988 (1955-02-01), Smisko
patent: 3199553 (1965-08-01), Garrett et al.
patent: 3921257 (1975-11-01), Appleby et al.
patent: 4367967 (1983-01-01), Albert, Jr.
patent: 4395802 (1983-08-01), Albert, Jr.
patent: 4509877 (1985-04-01), Sobin et al.
patent: 4565493 (1986-01-01), Hallerback
patent: 4794957 (1989-01-01), Metzler, Jr.
Hose Rig Hardware, Part No. T04016-Size D, Aeroquip Catalog.
Commercially Produced Hose, Prior Art #7.

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