Goodrich Corporation

Korey Michael Reber

James Acks

Derek C Milsom

Ronald Kucera

James P Acks

A steering apparatus may comprise a steering collar, a first linear actuator, a first drive gear, a crankshaft, and a sun gear, wherein the sun gear is disposed within the collar, wherein the first drive gear is fixed to the crankshaft and coupled to the sun gear such that the collar rotates about the sun gear in response to rotation of the crankshaft, wherein the first linear actuator is coupled between the crankshaft and the collar.

Integral steering motor and collar for landing gear

A nose-wheel steering system is disclosed. In various embodiments, the system includes an actuator; a strut; and a gearing mechanism operably coupling the actuator to the strut, the gearing mechanism including a steering collar attached to the strut, and idler gear engaged with the actuator and a pinion having a first gear engaged with the idler gear and a second gear engaged with the steering collar.

Nose wheel steering system

A steering system may include a gear assembly and a collar. The gear assembly may include a planet carrier, a planet gear, an internal ring gear, and a sun gear. The planet gear may be disposed between the internal ring gear and the sun gear. The gear assembly may provide a mechanical advantage to the steering system, which may result in a greater powered steering range, a shorter rack assembly, and/or increased design space relative to typical steering systems.

Nose wheel steering systems and methods

A locking actuator arrangement may comprise an actuator housing defining a retaining cavity, an actuator piston comprising a piston head and a piston rod extending from the piston head, a receptacle body defining a receiving cavity, wherein the receiving cavity is configured to receive at least a portion of the piston rod, and the piston rod is configured to be received by the receiving cavity in response to alignment of at least two coupled links.

Landing gear folding brace with locking actuator

An articulated landing gear may include electrical lines and/or hydraulic lines located within the articulated landing gear. The articulated landing gear may have a hollow structural post and a hollow trailing arm coupled by a pivot joint. The electrical lines and/or hydraulic lines may be routed through an interior of the hollow structural post and through an interior of the hollow trailing arm. A bulkhead within the hollow structural post or the hollow trailing arms may include guide holes. The electrical lines and/or hydraulic lines may be supported by the bulkhead by passing through the guide holes. The electrical lines and/or hydraulic lines may be flexible around the pivot joint.

Growing community of inventors

Strongsville, OH, United States of America

Korey Michael Reber