Patent ID: 9238510
Filing Date: 2016-01-19
CPC Classification: B64D

Claim Text:
1. A boomerang link for aircraft engine mounts, including: a first orifice and a second orifice, both intended to connect said boomerang link to an aircraft pylon, and a third orifice, intended to connect said boomerang link to an aircraft engine, wherein: said third orifice is offset relative to a plane passing simultaneously through an axis of said first orifice and through an axis of said second orifice, and when said boomerang link is seen in section in any plane orthogonal to the axes of said first and second orifices, a first straight line segment extending from the axis of said first orifice to an axis of said third orifice crosses a region external to said boomerang link, wherein said boomerang link is conformed so that, when said boomerang link is seen in section in any plane orthogonal to said axes of said first and second orifices, a second straight line segment extending from the axis of said second orifice to the axis of said third orifice crosses said region external to the boomerang link.