Assembly for mounting a turbine engine to a pylon

An assembly for mounting a turbine engine to an airframe, the turbine engine comprising a first engine attachment arranged circumferentially between a plurality of second engine attachments, the assembly comprising:

• a pylon extending axially between a forward pylon end and an aft pylon end;
• a mounting beam comprising a mount beam fitting that extends axially between a first mount beam end and a second mount beam end, and a mount beam flange that extends radially out from the mount beam fitting at the first mount beam end;
• a plurality of fasteners that connect the mounting beam to the forward pylon end, wherein a first of the fasteners extends radially through the mount beam fitting and into the pylon, and a second of the fasteners extends axially through the mount beam flange and into the pylon;
• a first mounting linkage adapted to connect the first mount beam end to the first engine attachment;
• and
• a second mounting linkage adapted to connect the second mount beam end to the second engine attachments.

A turbine engine assembly for mounting to a pylon that extends axially between a forward pylon end and an aft pylon end, comprising:

• a turbine engine comprising a first engine attachment arranged circumferentially between a plurality of second engine attachments;
• a mounting beam comprising a mount beam fitting that extends axially between a first mount beam end and a second mount beam end, and a mount beam flange that extends radially out from the mount beam fitting at the first mount beam end, wherein a first fastener aperture extends radially through the mount beam fitting, and a second fastener aperture extends axially through the mount beam flange;
• a plurality of fasteners adapted to connect the mounting beam to the forward pylon end, wherein a first of the fasteners is mated with the first fastener aperture, and a second of the fasteners is mated with the second fastener aperture;
• a first mounting linkage that connects the first mount beam end to the first engine attachment;
• and
• a second mounting linkage that connects the second mount beam end to the second engine attachments.