A beam for suspending a turboshaft engine from an aircraft structure, including a first attachment mechanism configured to be secured to the aircraft structure and at least one second attachment mechanism configured to be secured to the engine. The beam is at least partially made from a metal-matrix composite material including reinforcing fibers. In one embodiment, the beam takes a form of a circle arc.
Beam for suspending a turboshaft engine from an aircraft structure
2016-04-26
Patent
Elektronische Ressource
Englisch
Turboshaft Engine Development for Commercial Tiltrotor Aircraft
SAE Technical Papers | 1991
|Online Contents | 1995
Online Contents | 2001