Aircraft electric taxi system design and operation
AssigneeBorealis Technical Limited
InventorsIsaiah W. Cox, Jan Vana, Joseph J. Cox, Yonatan Rotenberg
Life of this patent
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AssigneeBorealis Technical Limited
InventorsIsaiah W. Cox, Jan Vana, Joseph J. Cox, Yonatan Rotenberg
Estimating the term…
A method for designing and operating an aircraft nose landing gear wheel-mounted electric taxi system to move aircraft with optimal torque during a broad range of ground travel conditions. Electric taxi system components may be sized to produce optimal ground travel torque to move aircraft during the majority of aircraft ground travel conditions and operated to produce a maximum or breakaway torque to move the aircraft with the electric taxi system when a higher level of torque is required. Turning the nose landing gear wheels to a selected angle or through a range of angles simultaneously as the electric taxi system is operated produces the breakaway torque required to get the aircraft moving. When lower torque is needed, the aircraft may be driven with the nose landing gear wheels parallel to the longitudinal axis to produce optimal torque for electric taxi system-powered aircraft ground travel.
A method for moving an aircraft equipped with landing gear wheel-mounted electric taxi drive systems during breakaway ground operations and situations requiring a breakaway level of torque to get the aircraft moving and during ground travel operations that do not require a breakaway level of torque to move the aircraft, comprising:
An aircraft nose landing gear wheel-mounted electric taxi drive system designed to produce ground travel torque during most electric taxi drive system-powered aircraft ground travel and operated to produce breakaway torque during ground conditions and situations requiring breakaway torque, comprising:
Dependencies are inferred from the claim text.