Patent ID: 8950702
Filing Date: 2015-02-10
Classification: B64D,Y02T

Abstract:
1. A mounting arrangement for a gas turbine engine comprising: a pylon mount structure having a first mount portion and a second mount portion positioned aft of said first mount portion, said first and said second mount portions comprising separate components to be independently attached to a pylon; a first engine mount beam integrally formed with said first mount portion as a single-piece component, said first engine mount beam being attachable to an engine case structure at a fore attachment interface, and wherein said first engine mount beam includes attachment structure to support at least one thrust link; and a second engine mount beam integrally formed with said second mount portion as a single-piece component, said second engine mount beam being attachable to the engine case structure at an aft attachment interface, and wherein said second engine mount beam includes attachment structure to pivotally support a linkage assembly.