Window frame assembly for aircraft

Patent metadata

Field	Value
Publication number	US-10183735-B2
Application number	US-201615012325-A
Country	US
Kind code	B2
Filing date	Feb 1, 2016
Priority date	Feb 1, 2016
Publication date	Jan 22, 2019
Grant date	Jan 22, 2019

Abstract

A window frame assembly for an aircraft, includes a window frame of composite material, adapted for attachment in a window opening of an aircraft, having an outer flange with an exterior surface and an interior surface, a metal erosion shield attached to the exterior surface of the outer flange, and a polymer adapter ring, attached to the interior surface of the outer flange. The window frame has a substantially constant thickness, and the erosion shield has a substantially constant cross-sectional shape. The adapter ring has a sloped engagement surface configured for supporting a window pane assembly.

First claim

What is claimed is:

1. A window frame assembly for an aircraft, comprising:
a window frame of composite material, having a substantially uniform thickness, adapted for attachment in a window opening of an aircraft, the window frame including an outer flange having an exterior surface and an interior surface;
a metal erosion shield, of substantially constant cross-sectional shape, attached to the exterior surface of the outer flange; and
a polymer adapter ring, attached to the interior surface of the outer flange, having a sloped engagement surface configured for supporting a window pane assembly.

2. The window frame assembly of claim 1 , wherein the window frame comprises stamp-formed polyetherketoneketone (PEKK) material.

3. The window frame assembly of claim 1 , wherein the window frame has a substantially uniform thickness in a range of 0.04″ to 0.33″.

4. The window frame assembly of claim 1 , wherein the window frame further comprises:
an inner flange, having an exterior surface adapted for attachment to an inner surface of a fuselage of the aircraft at the window opening; and
an annular rim, integrally disposed between the inner flange and the outer flange, defining a window pane opening.

5. The window frame assembly of claim 1 , wherein adapter ring comprises an injection-molded ring of carbon-filled polyetheretherketone (PEEK) material.

6. The window frame assembly of claim 1 , wherein the adapter ring is bonded to the interior surface of the outer flange with a polysulfide sealant.

7. The window frame assembly of claim 6 , further comprising a cured primer layer, disposed upon the interior surface of the outer flange, the polysulfide sealant being disposed between the cured primer layer and the adapter ring.

8. The window frame assembly of claim 1 , further comprising an inner beveled surface at a distal end of the outer flange, the inner beveled surface being substantially contiguous and coplanar with the sloped engagement surface of the adapter ring.

9. The window frame assembly of claim 1 , wherein the erosion shield comprises a die-cut titanium alloy ring.

10. The window frame assembly of claim 1 , wherein the erosion shield includes an outer face, an inner lip and an outer curved edge, each of the inner lip and the outer curved edge having an arc of not more than 90° relative to the outer face, the inner lip adapted to mate with a distal end of the outer flange.

11. A window frame assembly for an aircraft, comprising:
a window frame of composite material, having a substantially uniform thickness and cross-sectional shape, including
an inner flange, having an exterior surface adapted for attachment to an inner surface of an aircraft fuselage at a window opening;
an outer flange, having an exterior surface, an interior surface and a distal end with an inner beveled edge;
a metal erosion shield, having a substantially symmetrical shape relative to a vertical axis, attached to the exterior surface of the outer flange; and
an annular rim, integrally disposed between the inner flange and the outer flange, defining a window pane opening; and

a polymer adapter ring, attached to the interior surface of the outer flange, having a sloped inner surface that is substantially aligned with the inner beveled edge of the outer flange, the sloped inner surface configured for supporting a window pane assembly within the window pane opening.

12. The window frame assembly of claim 11 , wherein the window frame comprises stamp-formed polyetherketoneketone (PEKK) material.

13. The window frame assembly of claim 11 , wherein adapter ring comprises an injection-molded ring of carbon-filled polyetheretherketone (PEEK) material.

14. The window frame assembly of claim 11 , wherein the adapter ring is bonded to the interior surface of the outer flange with a polysulfide sealant.

15. The window frame assembly of claim 11 , wherein the erosion shield comprises a die-cut titanium alloy ring, having an inner lip with an arc of not more than 90°.

16. An outer window assembly for an aircraft, comprising:
a window frame of thermoplastic material, defining an outer window pane opening, having a substantially uniform thickness and cross-sectional shape, adapted for attachment in a window opening of an aircraft fuselage, including an outer flange having an exterior surface and an interior surface;
a metal erosion shield, of substantially constant cross-sectional shape, attached to the exterior surface of the outer flange;
a polymer adapter ring, bonded to the interior surface of the outer flange, having a sloped inner surface; and
an outer window pane assembly, mounted upon the sloped inner surface of the adapter ring within the outer window pane opening.

17. The outer window assembly of claim 16 , wherein the window frame comprises stamp-formed polyetherketoneketone (PEKK) material.

18. The outer window assembly of claim 16 , wherein adapter ring comprises an injection-molded ring of 30% carbon-filled polyetheretherketone (PEEK) material.

19. The outer window assembly of claim 16 , further comprising a cured primer layer, disposed upon the interior surface of the outer flange, and a polysulfide sealant, disposed between the primer layer and the adapter ring, the sealant bonding the adapter ring to the outer flange.

20. The outer window assembly of claim 16 , wherein the erosion shield comprises a die-cut titanium alloy ring, having an outer face, an inner lip, and an outer curved edge, each of the inner lip and the outer curved edge having an arc of not more than 90° relative to the outer face.

21. The window frame assembly of claim 1 , wherein the adapter ring has a triangular cross-section.

22. The window frame assembly of claim 4 , further comprising a fillet seal between the adapter ring and the annular rim.

Assignees

• Boeing Co

Inventors

• Gideon David E
• Schroeder Ian E
• Hall Kristin L
• Ng Kin M
• Kinney Megan C
• Reyneke Greg M
• Wilkerson Randall D
• Rosman Richard R
• Bartel Aaron W

Classifications

• B64C1/1492 Primary

  Structure and mounting of the transparent elements in the window or windscreen · CPC title