ENGINE MOUNTING STRUCTURE INTERPOSED BETWEEN AN AIRCRAFT WING SYSTEM AND SAID ENGINE

摘要

The invention concerns an engine mounting structure designed to be interposed between an aircraft wing system and said engine, the structure comprising a rigid structure (8) as well as front aerodynamic structure (24) mounted fixedly on said structure (8) via mounting means, the front aerodynamic structure being designed to support fan cowlings and to be interposed between the rigid structure and the wing system. The invention is characterized in that the mounting means comprise at least one connecting rod with adjustable length (32) one end of which is mounted on the structure (8), and the other end of which is mounted on the front aerodynamic structure (24).