Fuel drainage connector system for aircraft gas turbine

Details Fuel drainage connector system for aircraft gas turbine Fuel drainage connector system for aircraft gas turbine

1992-06-05

1993-11-09

Casaregola, Louis J.

Power plants

Combustion products used as motive fluid

With safety device

60739, 285 14, F02C 722

Patent

active

052591859

ABSTRACT:
A fuel drain can assembly positioned between the fuel manifold and the fuel nozzles of a gas turbine engine which utilizes detachable connectors rotatable into locking engagement without special tooling.

REFERENCES:
patent: 2684860 (1954-07-01), Rafferty
patent: 2690648 (1954-10-01), Pearce et al.
patent: 2846845 (1958-08-01), Parker
patent: 2881827 (1959-04-01), Roche et al.
patent: 3645562 (1972-02-01), Fandetti et al.
patent: 3858910 (1975-01-01), Oetiker
patent: 4467610 (1984-08-01), Pearson et al.
patent: 4708371 (1987-11-01), Elsworth et al.
patent: 4960153 (1990-10-01), Bergsma

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