ENHANCED TAKE-OFF SYSTEM

An automatic takeoff flight control system provides takeoff speed reduction to thereby reduce the takeoff distance (TOD) and, as a consequence, increase the takeoff weight (TOW); sets the horizontal stabilizer (HSTAB) in a non-trimmed condition - named "mistrim"; and provide best beta for...

Full description

Saved in:
Bibliographic Details
Main Authors Carneiro, Luiz Gustavo Medeiros, De Tarso Ferreira, Daniel Paulo, De Camargo Clark Reis, Jose Roberto Ferreira, Guedes, Patrice London, Kestenbach, Thomas
Format Patent
LanguageEnglish
French
German
Published 26.08.2020
Subjects
CONTROLLING
PHYSICS
REGULATING
SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
Online AccessGet full text

Cover

More Information
Summary:An automatic takeoff flight control system provides takeoff speed reduction to thereby reduce the takeoff distance (TOD) and, as a consequence, increase the takeoff weight (TOW); sets the horizontal stabilizer (HSTAB) in a non-trimmed condition - named "mistrim"; and provide best beta for optimum climb at takeoff, through lateral-directional surfaces commands.
Bibliography:Application Number: EP20170190574