Patent ID: 6682015
Filing Date: 2004-01-27
Classification: B64D,F02C,Y02T

Abstract:
A device for attaching an engine to a pylon of an aircraft, said device including:a first and s second assemblies forming lateral rods; first connecting means adapted to connect the first assembly forming a lateral rod to a first female yoke secured to said pylon; second connecting means adapted to connect the first assembly forming a lateral rod to a second female yoke secured to said engine; third connecting means adapted to connect the second assembly forming a lateral rod to a third female yoke secured to said pylon; and fourth connecting means adapted to connect the second assembly forming a lateral rod to a fourth female yoke secured to said engine; wherein each of said first, second, third, and fourth female yokes comprises a central web and two lateral webs, said lateral rods being received in said yokes on both sides of said central web, and wherein each of said connecting means includes a pin passing without clearance through said lateral rods and said central web and a passing with clearance through said lateral webs.