Patent ID: 8561940

Claim:
An arrangement for suspending a jet engine, comprising: a suspension beam attachable to a supporting structure attached to an aircraft fuselage; a first suspension for connecting one of a forward portion of an engine casing to a forward portion of the suspension beam and a rearward portion of the engine casing to a rearward portion of the suspension beam; a framework for connecting to an other of the forward portion of the engine casing and the rearward portion of the engine casing; a second suspension connecting the framework to an other of the forward portion of the suspension beam and the rearward portion of the suspension beam; at least one thrust rod additionally connecting the framework to the suspension beam, the thrust rod arranged at an acute angle relative to the suspension beam: wherein the framework is arranged circumferentially around the engine casing; a plurality of struts extending around the engine casing and connecting the engine casing to the framework.