| 摘要 |
#CMT# #/CMT# The method involves forming a recess, which does not emerge on a portion of a side wall (12) along perimeter of an opening. An outer transparent element (10) is positioned in the opening from exterior of a fuselage, where the element includes a part (13) whose diameter is higher than that of the opening, and shape cooperates with the wall portion to block the element. The element and an inner transparent element (11) are integrated to the fuselage by a strap (22), where the strap flattens a continuous joint (21) against the fuselage and an inner wall of a groove (17) of the outer element. #CMT# : #/CMT# An independent claim is also included for an outer transparent element mounted on an opening defined in a side wall of a fuselage of an aircraft. #CMT#USE : #/CMT# Method for assembling a window on an opening defined in a side wall of a fuselage of an aircraft (claimed) e.g. commercial aircraft. #CMT#ADVANTAGE : #/CMT# The method assembles the window on the opening without requiring additional drilling in a skin of the fuselage, in a simple and rapid manner, and ensures simple and easy maintenance of the window at reduced cost. The outer transparent element is inexpensive and light in weight, and ensures better mechanical resistance. The method assembles the outer transparent element without requiring drilling of the side wall of the fuselage and mechanical fixations for connecting the wall of the fuselage with liners, thus reducing paraffin consumption in the aircraft. The method enables the window to ensure the thermal insulation of the inner space of the fuselage, thus assuring comfort of the passengers. #CMT#DESCRIPTION OF DRAWINGS : #/CMT# The drawing shows a schematic partial sectional view of a window of an aircraft. 10 : Outer transparent element 11 : Inner transparent element 12 : Side wall 13 : Outer transparent element 's part 17 : Groove 21 : Continuous joint 22 : Strap. |
