Method and apparatus for guiding a jet aircraft in a noise-abate

Details Method and apparatus for guiding a jet aircraft in a noise-abate Method and apparatus for guiding a jet aircraft in a noise-abate

1975-11-13

1977-04-26

Blix, Trygve M.

Aeronautics and astronautics

Aircraft control

Automatic

73178T, 23515022, 244180, B64C 1500

Patent

active

040197026

ABSTRACT:
A pilot guidance system that computes and displays pitch and speed steering commands is automatically operated during the post-takeoff climb (at specified times clocked from the start of the takeoff run), to present commands that assist the pilot in cutting (and later in restoring) thrust for a predetermined interval to reduce engine noise, and in guiding the aircraft in a safe, gentle climb over the proximate community. The specified times (unique for each model of aircraft, airport, runway and departure flight path), synchronize the thrust cutback interval with the boundaries of the community in line with chosen departure path.

REFERENCES:
patent: 3025494 (1962-03-01), Andresen
patent: 3522729 (1970-08-01), Miller
patent: 3800127 (1974-03-01), Knemeyer

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