Landing gear method and apparatus for braking and maneuvering
First Claim
1. An integrated wheel/hub motor generator and electromagnetic braking system for aircraft landing gear, comprising:
- a nose gear and a main landing gear, at least one of the nose gear or the main landing gear comprising;
a nonrotational base portion configured to connect to an airframe of the aircraft;
a wheel connected to and rotatable with respect to the base portion about a rotational axis;
a plurality of stators connected to the base portion;
a plurality of rotors connected to the wheel and configured to rotate with respect to said stators;
wherein each of said pluralities of stators and rotors is configured to generate a magnetic flux; and
wherein said pluralities of stators and rotors are configured so that interaction of their magnetic fluxes causes at least one of;
converting electrical energy to rotational torque energy of the wheel, and converting rotational torque energy of the wheel to electrical energy of a magnitude suitable for use to decrease the rotational velocity of said wheel.
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Accused Products
Abstract
Aircraft landing gear comprised of a wheel hub motor/generator disks stack, includes alternating rotor and stator disks mounted with respect to the wheel support and wheel. The wheel hub motor/generator can provide motive force to the wheel when electrical power is applied, which may be applied prior to touch-down thus decreasing the difference in relative velocities of the tire radial velocity with that of the relative velocity of the runway thus greatly reducing the sliding friction wear of said tire. After touchdown the wheel hub motor/generator may be used as a generator thus applying a regenerative braking force and/or a motorized braking action to the wheel. The energy generated upon landing maybe dissipated through a resistor and/or stored for later use in providing a source for motive power to the aircraft wheels for the purpose of taxiing and ground maneuvers of said aircraft.
96 Citations
21 Claims
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1. An integrated wheel/hub motor generator and electromagnetic braking system for aircraft landing gear, comprising:
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a nose gear and a main landing gear, at least one of the nose gear or the main landing gear comprising; a nonrotational base portion configured to connect to an airframe of the aircraft; a wheel connected to and rotatable with respect to the base portion about a rotational axis; a plurality of stators connected to the base portion; a plurality of rotors connected to the wheel and configured to rotate with respect to said stators; wherein each of said pluralities of stators and rotors is configured to generate a magnetic flux; and wherein said pluralities of stators and rotors are configured so that interaction of their magnetic fluxes causes at least one of;
converting electrical energy to rotational torque energy of the wheel, and converting rotational torque energy of the wheel to electrical energy of a magnitude suitable for use to decrease the rotational velocity of said wheel. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 15, 16, 17, 18, 19, 20, 21)
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Specification