Patent ID: 8371531
Filing Date: 2013-02-12
Classification: B64C,Y10T

Abstract:
1. A method for assembling a window on an opening provided in a side wall of the fuselage of an aircraft, said window including an external transparent member and at least one internal transparent member, the method comprising: a) providing a blind recess on a portion of said side wall along a perimeter of said opening, b) positioning said external transparent member from outside of the fuselage in said opening, said external transparent member having a first part a diameter of which is greater than a diameter of said opening, with said first part having a shape cooperating with the portion of said side wall so as to laterally and longitudinally lock said external transparent member in said opening, c) said external transparent member including a second part having a groove protruding inside said fuselage, wherein the external transparent member is made integral with said at least one internal transparent member and with said fuselage through a band strip, said band strip applying a joint against at least the fuselage and an internal wall of said groove.