System for supplying fuel to an aircraft engine

Details System for supplying fuel to an aircraft engine System for supplying fuel to an aircraft engine

1986-03-14

1987-08-18

Casaregola, Louis J.

Power plants

Reaction motor

Condition responsive thrust varying means

60 39281, F02C 928

Patent

active

046868259

ABSTRACT:
This invention relates to a system for supplying fuel to an aircraft engine, wherein an electronic computer subdivides the stroke of the throttle lever into a plurality of zones, in each of which the thrust of the engine varies between a maximum value and a minimum value. The computer ensures a modulation of the thrust about the value corresponding to that displayed by the position of said throttle lever. No mechanical link is provided between the lever and the fuel admission valve.

REFERENCES:
patent: 3854287 (1974-12-01), Rembold
patent: 4248042 (1981-02-01), Larsen et al.
patent: 4258545 (1981-03-01), Slater
patent: 4314445 (1982-02-01), Lewis
patent: 4468924 (1984-09-01), Moore
patent: 4551972 (1985-11-01), Lewis

Affiliated with

Also associated with

Rating

System for supplying fuel to an aircraft engine does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with System for supplying fuel to an aircraft engine, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and System for supplying fuel to an aircraft engine will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFUS-PAI-O-1110177