Coupling assembly

Pipe joints or couplings – Packed – Flanged pipe

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Details

285347, 285910, F16L 1706

Patent

active

054701147

ABSTRACT:
A coupling assembly for fluid carrying tubes in a gas turbine engine include first and second fittings fixedly joined to respective ones of the tubes. The first and second fittings include respective first and second mating flanges which are joined together by a clamping band which is adjustable therearound. The first and second flanges include oppositely facing first and second flat faces, with the first flange having a counterbore extending inwardly from the first face, and the second flange having a pilot tube extending outwardly therefrom for being inserted into the counterbore. An annular seal is disposed between the first and second fittings for providing a leak-proof coupling upon clamping together of the two fittings by the clamping band.

REFERENCES:
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patent: 2773709 (1956-12-01), Smith
patent: 3007600 (1961-11-01), Horner
patent: 3029095 (1962-04-01), King et al.
patent: 3554581 (1971-01-01), Mason et al.
patent: 3712631 (1973-01-01), Forchini et al.
patent: 3986732 (1976-10-01), Stanley
patent: 4443029 (1984-04-01), Laxo
patent: 4615547 (1986-10-01), Sutcliffe et al.
patent: 4844515 (1989-07-01), Field
patent: 4850621 (1989-07-01), Umehara
patent: 4934742 (1990-06-01), Williamson
patent: 5040714 (1991-08-01), McManigal
patent: 5308125 (1994-05-01), Anderson, Jr,
SAE, "Coupling Assembly, V-Retainer, High Pressure, High Temperature, Pneumatic Tube," Feb. 1988, Aerospace Standard AS1895, pp: Cover and 1-3 & 7.
USAF, "Seal, Plain Rubber (-65 to +160 Deg. F Fuel Resistant), Mold in Groove," MS27194(USAF), one page.
USG, "Flange, Swivel, Retaining," MS20756, Aug. 1957, pp: 1-3 & sketch.

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