Aircraft engine automatic throttle control with automatic gain p

Details Aircraft engine automatic throttle control with automatic gain p Aircraft engine automatic throttle control with automatic gain p

1975-08-15

1976-09-21

Ruggiero, Joseph F.

Registers

Transfer mechanism

Traveling pawl

244182, B64C 1318

Patent

active

039814424

ABSTRACT:
An automatic throttle system operable during all flight regimes includes automatic gain control apparatus for minimizing changes in engine thrust during the cruise mode caused by air mass turbulence and provides desirable response to commanded changes in air speed or flight path while maintaining desirable response to large magnitude wind shears. The gain of the air speed error signal is controlled as a function of Mach or true air speed and the gain of the throttle rate command signal normally controlling the engine throttle servo motor is controlled as a function of the commanded change in air speed, the air speed error, the aircraft's Mach or true air speed, and altitude rate by a real time logical control system.

REFERENCES:
patent: 3627236 (1971-12-01), Hess
patent: 3691356 (1972-09-01), Miller
patent: 3892374 (1975-07-01), Lambregts
patent: 3901466 (1975-08-01), Lambregts
patent: 3908934 (1975-09-01), Schloeman

Affiliated with

Also associated with

Rating

Aircraft engine automatic throttle control with automatic gain p does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Aircraft engine automatic throttle control with automatic gain p, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Aircraft engine automatic throttle control with automatic gain p will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFUS-PAI-O-1408999