Patent ID: 8382031
Filing Date: 2013-02-26
Classification: B64D

Abstract:
1. An engine unit for an aircraft comprising: an engine; a device for hooking the engine to said aircraft; a nacelle surrounding the engine and including fan cowls and an air inlet, the device for hooking comprising a rigid structure and a front aerodynamic structure, the front aerodynamic structure including a cradle covered with an aerodynamic fairing, the cradle including rear means of hooking mounted on the rigid structure of the device for hooking, and the cradle including front means of hooking mounted on the air inlet and configured to fasten said air inlet of said nacelle to said cradle of said device for hooking, wherein the air inlet is flush against the fan cowls, and is located frontward in relation to the fan cowls, and wherein the fan cowls are articulated around the cradle, the cradle carrying the front and rear means of hooking.