Front installation joint integrated with airplane hang

Disclosed is a front installation node integrated with an aircraft pylon. The front installation node is suitable for integral forming with a front end frame (100) of an aircraft pylon and comprises: a first lug (10) and a second lug (20), both respectively protruding outwardly from two sides of the front end frame; and a first connecting rod (70) and a second connecting rod (80), one end thereof being respectively connected to the first lug and the second lug, and the other end thereof being respectively suitable for connecting to an aircraft engine, wherein the first connecting rod can pivotally connect to the first lug at a first connection point (1), the second connecting rod and the second lug are respectively connected at a second connecting point (2) and a third connecting point (3). The front installation node for engine is integrated with the pylon frame, saving on weight; and using the front installation node to transmit torque is beneficial in reducing the external width of a rear installation node, reducing engine fuel consumption.