Patent ID: 9272775
Filing Date: 2016-03-01
CPC Classification: B64C

Claim Text:
1. A breaker strut for an aircraft landing gear, the breaker strut comprising: two portions; wherein a lower one of the two portions includes an eye for articulated connection to a landing gear undercarriage about a first hinge axis; wherein an upper one of the two portions includes a first hinge for articulated connection to at least one structural aircraft element about a second hinge axis; wherein the two portions are connected to one another by a second respective hinge about a third hinge axis parallel to the first and second hinge axes, such that the lower and upper portions are moved relative to one another between: wherein at least one of the lower and upper portions of the breaker strut includes a mechanism of mutual attachment of the eye and the second hinge and the first and second hinges, respectively, which allows a distance separating the eye and second hinge and the first and second hinges, respectively, to be modified.