Goodrich Corporation

Charles J Spink

Dennis Wayne Martin

William E Luce

Ian Kopp

Dennis W Martin

A landing gear arrangement may comprise a lever configured to be coupled between an axle and a strut piston of a shock strut, a load damper configured to be externally coupled between the shock strut and the lever, wherein the load damper is configured to increase a length of the landing gear arrangement in response to an extension force of the load damper increasing above a ground force reacted through the landing gear arrangement. The load damper may be located externally from the strut piston.

Semi cantilevered landing gear actuated by an external articulating load damper for improved take-off

A landing gear support arrangement may comprise a cylinder, a pin pivotally coupled to the cylinder, a head attached to the pin having a portion extending radially from the pin, and a bracket coupled to the portion of the head configured to axially support the pin.

Landing gear with structural load path diverter bracket

A shock strut includes a first cylinder defining a first volume. The shock strut includes a first piston head moveably positioned within the first volume and defining a first fluid chamber and a third fluid chamber within the first volume. The shock strut includes a second cylinder defining a second volume. The shock strut includes a second piston head moveably positioned within the second volume and defining a second fluid chamber and a fourth fluid chamber within the second volume. The fourth fluid chamber is in fluid communication with the third fluid chamber. The shock strut also includes a bleed port. The shock strut also includes a tube extending from the fourth fluid chamber through the second piston head and the second fluid chamber to the bleed port.

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Seattle, WA, United States of America

Charles J Spink