Adjusting mechanism and method for fuel control

Power plants – Combustion products used as motive fluid

Patent

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Details

60 3931, 137315, 251291, F02C 720

Patent

active

039771830

ABSTRACT:
The indexing of the power lever of a fuel control for a turbine type of power and the mechanism necessary to effectuate the same is simplified so as to facilitate the installation of the fuel control relative to the remotely cockpit-mounted power lever. Preselecting a point on the power lever shaft relative to a pair of outwardly spaced oriented mounting points, permits a factory-adjusted-fuel control to be installed to a complementary adaptor on the aircraft eliminating the customary field adjustments and certain adjusting mechanisms.

REFERENCES:
patent: 2409178 (1946-10-01), Allison
patent: 3153989 (1964-10-01), Roberts
patent: 3395886 (1968-08-01), Fawkes
patent: 3590653 (1971-07-01), Dreckmann
patent: 3677139 (1972-07-01), Wheeler
patent: 3710568 (1973-01-01), Rice
patent: 3842594 (1974-10-01), Grunert

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