A method of braking left and light landing gear wheels on respective left and right sides of an aircraft. A desired left braking parameter (L) is received for the left wheel and a desired right braking parameter (R) is received for the right wheel. The left wheel is braked with a reduced left braking parameter (L') which is less than the desired left braking parameter (L), and the right wheel is braked with a reduced light braking parameter (R') which is less than the desired right braking parameter (R). A difference between the braking parameters is maintained so that L'-R'=L-R.


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    Titel :

    Differential braking of aircraft landing gear wheels


    Beteiligte:
    HOWELL GEORGE (Autor:in) / BEN LIVIER (Autor:in) / ROMANA LOUIS-EMMANUEL (Autor:in)

    Erscheinungsdatum :

    27.01.2016


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen



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