Turbine engine thrust booster

Power plants – Reaction motor – Method of operation

Patent

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Details

60223, 60224, 60243, F02K 312

Patent

active

043144454

ABSTRACT:
Trim signals are removed from the fuel control computers of aircraft propulsion engines to increase thrust upon detection of a predetermined difference between engine speeds.

REFERENCES:
patent: 3521448 (1970-07-01), Amelio
patent: 3601984 (1971-08-01), Davis
patent: 3832846 (1974-09-01), Leeson
patent: 3852956 (1974-12-01), Martin
patent: 3854287 (1974-12-01), Rembold
patent: 3969890 (1976-07-01), Nelson
patent: 3987620 (1976-10-01), Giordano et al.
patent: 4173119 (1979-11-01), Gruene et al.

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