Braking process for an airplane
a technology for airplanes and braking systems, applied in aircraft braking arrangements, navigation instruments, instruments, etc., can solve problems such as damage to front landing gears, rapid derotation of airplanes, damage that can go as far as breakage, and achieve the effect of reducing braking possibilities
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[0038]FIG. 1 is a schematic, functional view of certain elements of an aircraft 101. FIG. 1 shows, in particular, that the aircraft 101 has a logic 102 programmed according to instruction codes recorded in a memory 103. The programmed logic 102 is then designated as a processing device 102. The device 102 also has a microprocessor 104 and input / output circuits 105. Elements 103 to 105 are interconnected by a bus 106.
[0039]The device 102 is designated, in practice, by the term “calculator.”
[0040]The memory 103 has at least some instruction codes for implementing the process in the invention. These instruction codes are recorded in a zone 103.1 of the memory 103.
[0041]The circuits 105 allow the device 102 to be connected to the other communicating devices of the aircraft 101. For the invention, these communicating devices are at least:[0042]a command interface device 107 for braking. It is with this device 107 that the pilot of the aircraft 101 controls the braking of said aircraft.[00
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