Aircraft landing gear steering system

Details Aircraft landing gear steering system Aircraft landing gear steering system

B - Operations, Transporting

64

C

B64C 25/50 (2006.01)

Patent

CA 2664885

The invention relates generally to an aircraft landing gear steering system (110, 210, 310) comprising a turning member (118, 218, 318) that is operably coupled to a landing gear leg (116, 216, 316) through a harmonic drive mechanism (260, 360). The landing gear steering system (110, 210, 310) may be electrically driven. Additionally, the landing gear system (110, 210, 310) has various advantages, including the provision of a safe failure mode should the harmonic drive mechanism (260, 360) fail.

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