Steerable landing gear
AssigneeThe Boeing Company
InventorJohn Watts
Life of this patent
Estimating the term…
Abstract
A six wheel, three axle, bogie type main landing gear for an airplane is retractable as a unit and is provided with a rearward set of wheels or a forward set of wheels that is steerable with respect to the non-rotatable bogie beam. The set of wheels turns in response to steering of the nose wheel past a given angle. A wheel assembly is mounted for rotation with respect to a vertical shaft supported by a fork extending longitudinally of the beam, and a pair of hydraulic cylinders turns the wheel axles with respect to the beam.
Claims14
In a landing gear system for large aircraft provided with a steerable nose wheel landing gear and a main landing gear including plural trucks mounted on retractable struts positioned rearwardly of said nose wheel landing gear, at least one of said trucks comprising:
- an elongated retractable beam extending in a direction longitudinal of said aircraft and positionable in substantial supporting relation to said aircraft below the body of said aircraft on one of said struts, said beam being provided with a plurality of support wheels mounted on said beam including a first pair coaxial with one another and located forwardly on said beam and a second pair coaxial with one another and located rearwardly on said beam,
- wherein said beam is provided with means for mounting at least one pair of said wheels for rotation with respect to said beam as a unit about a vertical axis fixed with respect to said beam, and
- means for steering the last mentioned pair of wheels with respect to said beam about said vertical axis in coordination with the steering of said nose landing gear for reducing tire scrubbing of the wheels of said main landing gear.
In a landing gear system for large aircraft provided with a steerable nose wheel landing gear and a main landing gear including plural trucks mounted on retractable struts positioned rearwardly of said nose wheel landing gear, at least one of said trucks comprising:
- an elongated retractable beam extending in a direction longitudinal of said aircraft and positionable below the body of said aircraft on one of said struts, said beam being non-rotatable about the axis of its mounting strut and provided with a plurality of support wheels mounted on said beam including a first pair coaxial with one another and located forwardly on said beam and a second pair coaxial with one another and located rearwardly on said beam,
- wherein said beam is provided with means for mounting at least one pair of said wheels for rotation as a unit about a vertical axis fixed with respect to said beam, and
- means for steering the last mentioned pair of wheels with respect to said beam about said vertical axis in coordination with the steering of said nose landing gear for reducing tire scrubbing of the wheels of said main landing gear.
In a landing gear system for large aircraft provided with a steerable nose wheel landing gear and a main landing gear including plural trucks mounted on retractable struts positioned rearwardly of said nose wheel landing gear, at least one of said trucks comprising:
- an elongated retractable beam extending in a direction longitudinal of said aircraft and positionable below the body of said aircraft on one of said struts, said beam being provided with a plurality of support wheels mounted on said beam including a first pair coaxial with one another and located forwardly on said beam and a second pair coaxial with one another and located rearwardly on said beam,
- wherein said beam is provided with means for mounting at least one pair of said wheels for rotation as a unit about a vertical axis fixed with respect to said beam,
- said mounting means for the last mentioned pair of wheels comprising a forked portion at one end of said beam including an upper member and a lower member supporting a vertical post therebetween defining said vertical axis, and a hub rotatable about said vertical post for carrying the last mentioned pair of wheels in coaxial relation with one another on either side of said hub, and
- means for steering the last mentioned pair of wheels with respect to said beam about said vertical axis in coordination with the steering of said nose landing gear for reducing tire scrubbing of the wheels of said main landing gear,
- said means for steering comprising a pair of hydraulic actuators attached to said forked portion and having a driving relation with respect to said hub for exerting a turning moment on said hub.
In a landing gear system for large aircraft provided with a steerable nose wheel landing gear and a main landing gear including plural trucks mounted on retractable struts positioned rearwardly of said nose wheel landing gear, at least one of said trucks comprising:
- an elongated retractable beam extending in a direction longitudinal of said aircraft and positionable below the body of said aircraft on a said strut, said beam being provided with a plurality of support wheels mounted on said beam including a first pair coaxial with one another and located forwardly on said beam and a second pair coaxial with one another and located rearwardly on said beam,
- wherein said beam is provided with means for mounting at least one pair of said wheels for rotation as a unit about a vertical axis fixed with respect to said beam, said mounting means for the last mentioned pair of wheels comprising a forked portion at one end of said beam including an upper member and a lower member supporting a vertical post therebetween defining said vertical axis, and a hub rotatable about said vertical post for carrying the last mentioned pair of wheels in coaxial relation with one another on either side of said hub, and
- means for steering the last mentioned pair of wheels with respect to said beam about said vertical axis in coordination with the steering of said nose landing gear for reducing tire scrubbing of the wheels of said main landing gear,
- said means for steering comprising a pair of hydraulic actuators attached to said forked portion and having a driving relation with respect to said hub for exerting a turning moment on said hub, and including a yoke attached to said upper and lower members and extending longitudinally outward from the end of said beam for pivotally engaging cylinders of said hydraulic actuators at positions spaced from the end of said beam, said actuators having piston rods disposed to provide said driving relation to said hub, said rods driving said hub at either side thereof.
Dependencies are inferred from the claim text.