Abstract: An aircraft landing gear assembly including a structural load bearing beam arranged, in use, to react torsional loads applied to it. The beam has a tubular box section main body having four straight sidewall portions, adjacent sidewall portions being orthogonal to one another and connected by rounded corner portions. Each corner portion has a radius of between 10% and 40% of the width and/or height of the tubular box section main body.

Abstract: An aircraft landing gear assembly having a shock strut with an outer cylinder and a sliding tube, a bogie beam pivotally coupled to a first one of the outer cylinder and the sliding tube via a bogie pivot pin, and a set of torque links arranged to inhibit rotation of the sliding tube relative to the outer cylinder about the shock absorber travel axis. The torque links include a first torque link and a second torque link movably coupled to the first torque link. The first torque link is movably coupled to a second one of the outer cylinder and the sliding tube, which is distinct from the first one of the outer cylinder and the sliding tube, and the second torque link is pivotally coupled to the bogie pivot pin to pivot about the bogie pivot pin.

Abstract: An aircraft landing gear assembly including a structural load bearing beam arranged, in use, to react torsional loads applied to it. The beam has a tubular box section main body having four straight sidewall portions, adjacent sidewall portions being orthogonal to one another and connected by rounded corner portions. Each corner portion has a radius of between 10% and 40% of the width and/or height of the tubular box section main body.