Apparatus, system, and method for controlling landing gear
AssigneeAIRman Products, LLC
InventorsShane R. LaHousse, Christopher Domanski, Robert L. Allen
Life of this patent
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Abstract
A landing gear system and method of actuating the landing gear system, the system including a first leg assembly, a second leg assembly, a cross-shaft arranged between the two leg assemblies, and a landing gear actuator. The landing gear actuator includes a motor and a coupling shaft which is arranged to couple and decouple the landing gear actuator from the cross-shaft.
Claims20
A landing gear actuator assembly comprising:
- a housing having a cavity, the cavity comprising;
- a worm hub operatively arranged to rotate about a first imaginary rotational axis and within the cavity of the housing, the worm hub having a first outer circumferential surface having a first plurality of gear teeth arranged thereon and a first through-bore substantially parallel with the first imaginary rotational axis;
- a worm gear having a second outer circumferential surface having at least one gear tooth arranged to engage with the first plurality of gear teeth of the worm hub;
- and,
- a coupling shaft arranged through the housing and within the first through-bore of the worm hub and substantially parallel to the first imaginary rotational axis;
- a motor arranged to provide a first rotational force to the worm gear;
- and,
- wherein, the first rotational force of the motor induces a rotation of the worm gear within the housing and transfers the first rotational force to the worm hub.
A landing gear system, the system comprising:
- a first leg assembly, the first leg assembly comprising:
- a first leg housing;
- a first leg arranged to telescopingly engage with the first leg housing;
- and,
- a first leg gear arranged to transfer a rotational motion to the first leg;
- and,
- a second leg assembly, the second leg assembly comprising:
- a second leg housing;
- a second leg arranged to telescopingly engage with the second leg housing;
- and,
- a second leg gear arranged to transfer the rotational motion to the second leg;
- and,
- a cross-shaft arranged between the first leg assembly and the second leg assembly;
- and,
- a landing gear actuator assembly secured to the first leg assembly, the second leg assembly, or the cross-shaft, the landing gear actuator assembly comprising:
- a motor;
- and,
- a coupling shaft, wherein the coupling shaft is arranged to couple and decouple the motor from the cross-shaft.
The landing gear system of claim 13, wherein the landing gear actuator assembly further comprises:
- a housing having a cavity, the cavity comprising:
- a worm hub operatively arranged to rotate about a first imaginary rotational axis within the cavity of the housing, the worm hub having a first outer circumferential surface having a first plurality of gear-teeth arranged thereon and a first through-bore substantially parallel with the first imaginary rotational axis and the cross-shaft;
- and,
- a worm gear having a second outer circumferential surface having at least one gear tooth arranged to engage with the first plurality of gear teeth of the worm hub;
- wherein the motor is arranged to produce a first rotational force wherein the first rotational force induces a rotation of the worm gear within the housing and transfers the first rotational force to the worm hub.
A method of actuating a landing gear system, the method comprising:
- applying a first rotational force via a motor to a landing gear actuator assembly having a worm gear and a clutch assembly;
- converting the first rotational force into rotational motion via at least the worm gear;
- applying a first input to the landing gear actuator assembly, where the first input is arranged to engage the clutch assembly to transfer the first rotational force to a first leg assembly;
- and,
- raising or lowering a first leg of the first leg assembly.
Dependencies are inferred from the claim text.