Bonded aluminum window frame on fibre metal laminate fuselage skin
A window system and a method for manufacturing a window system, wherein a window frame is mounted on a fibre metal laminate skin of for example an aircraft. The window system comprise a fibre metal laminate skin including a mounting surface portion, e.g., the surrounding of a window opening, and a window frame having a first flange. A first side of the first flange being mounted to at least a part of a surface, e.g., the surrounding of a window opening. The first side is form-fitted to the mounting surface portion of the fibre metal laminate skin. The least a part of the surface of the first side of the first flange and the mounting surface portion of the fibre metal laminate skin are bonded.
1 . A window system comprising:
a fibre metal laminate skin; and
a window frame;
wherein the fibre metal laminate skin has a mounting surface portion;
wherein the window frame has a first flange;
wherein the first flange comprises a first side;
wherein at least a part of a surface of the first side is form-fitted to the mounting surface portion of the fibre metal laminate skin; and
wherein at least a part of the surface of the first side of the first flange and the mounting surface portion of the fibre metal laminate skin are bonded.
2 . The window system of claim 1 , wherein the first side of the first flange and the mounting surface of the fibre metal laminate skin sandwich a doubler, and the doubler is bonded to the first side of the first flange and the mounting surface of the fibre metal laminate skin.
3 . The window system of claim 1 , wherein the first side of the first flange and the mounting surface of the fibre metal laminate skin are adhesively mounted.
4 . The window system of claim 1 , wherein the first flange further comprises a second side, and a surface of the second side is inclined to the surface of the first side, so that the strength of the first flange substantially, continuously declines towards the edge of the first flange.
5 . The window system of claim 4 , wherein the surface of the second side smoothly transits to the surface to which the second side is bonded.
6 . The window system of claim 1 , wherein the mounting surface of the fibre metal laminate skin corresponds to a surface facing the interior of an aircraft.
7 . The window system of claim 1 , wherein the first flange is an outer flange extending away from a window opening.
8 . The window system of claim 1 , wherein the window frame and the fibre metal laminate skin are conductively connected.
9 . The window system of claim 8 , wherein the window frame and the fibre metal laminate skin are conductively connected by at least one of the group of a rivet, a fastener and a screw.
10 . The window system of claim 1 , wherein the window frame further comprises a surface portion which substantially aligns with a surface portion of the fibre metal laminate skin.
11 . The window system of claim 1 , wherein the fibre metal laminate skin is a fibre metal laminate fuselage skin of an aircraft.
12 . An aircraft having one or a plurality of window systems, each of the window systems comprising:
a fibre metal laminate skin; and
a window frame;
wherein the fibre metal laminate skin has a mounting surface portion;
wherein the window frame has a first flange;
wherein the first flange comprises a first side;
wherein at least a part of a surface of the first side is form-fitted to the mounting surface portion of the fibre metal laminate skin; and
wherein at least a part of the surface of the first side of the first flange and the mounting surface portion of the fibre metal laminate skin are bonded.
13 . A method for mounting a window frame and a fibre metal laminate skin, comprising:
providing a fibre metal laminate skin having a mounting surface portion;
providing a window frame with a first flange, which first flange comprises a first side, wherein at least a part of a surface of the first side is form-fitted to the mounting surface portion of the fibre metal laminate skin; and
bonding at least a part of the surface of the first side of the first flange of the window frame with the mounting surface portion of the fibre metal laminate skin.
14 . A computer readable medium having stored thereon instructions for causing a processor to direct the automated mounting of a window frame and a fibre metal laminate skin by:
providing a fibre metal laminate skin having a mounting surface portion;
providing a window frame with a first flange, which first flange comprises a first side, wherein at least a part of a surface of the first side is form-fitted to the mounting surface portion of the fibre metal laminate skin; and
bonding at least a part of the surface of the first side of the first flange of the window frame with the mounting surface portion of the fibre metal laminate skin.