IP Library Granted Patent US 10,654,555
Granted Patent B2
US 10,654,555 · App. 15/596,748 · Granted May 19, 2020

Window assembly for an aircraft

Inventors: Claus Hanske (Hamburg, DE); Hans-Jürgen Weber (Hamburg, DE); Bernd Kruse (Hamburg, DE); Christoph Cordes (Hamburg, DE)
Assignee: Airbus Operations GmbH
B64C1/1492B64C1/1484
View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 10,654,555
App. No.
15/596,748
Granted
May 19, 2020
Kind
B2
Abstract

A window assembly for an aircraft includes a window frame being arranged bordering a window opening in a hull of the aircraft, a window seal being attached to the window frame, a window being supported by the window frame and sealed to the window frame by the window seal, a window retainer covering the window seal and the window frame from the inside of the aircraft, and a transparent vapor barrier being supported by the window retainer and covering the window from the inside of the aircraft such that an air gap is formed between the window and the transparent vapor barrier.

Claims (19)

1. A window assembly for an aircraft, comprising:

a window frame arranged bordering a window opening in a hull of the aircraft;

a window seal attached to the window frame;

a window supported by the window frame and sealed to the window frame by the window seal;

a window retainer covering the window seal and the window frame from an inside of the aircraft; and

a transparent vapor barrier supported by the window retainer and covering the window from the inside of the aircraft such that an air gap is formed between the window and the transparent vapor barrier;

wherein the transparent vapor barrier is configured as a transparent airtight foil.

2. The window assembly of claim 1 , wherein the window is configured as a single-pane window.

3. The window assembly of claim 1 , wherein the transparent vapor barrier is detachably mounted to the window retainer.

4. The window assembly of claim 3 , wherein the transparent vapor barrier is mounted to the window retainer with a snap-fit connection.

5. The window assembly of claim 1 , wherein the transparent vapor barrier is integrally formed with the window retainer.

6. The window assembly of claim 1 , wherein the transparent vapor barrier is sealed to the window frame by the window seal.

7. An aircraft comprising a window assembly, the window assembly including:

a window frame arranged bordering a window opening in a hull of the aircraft;

a window seal attached to the window frame;

a window supported by the window frame and sealed to the window frame by the window seal;

a window retainer covering the window seal and the window frame from an inside of the aircraft; and

a transparent vapor barrier supported by the window retainer and covering the window from the inside of the aircraft such that an air gap is formed between the window and the transparent vapor barrier;

wherein the transparent vapor barrier is configured as a transparent airtight foil.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded May 17, 2017
From: HANSKE, CLAUS; WEBER, HANS-JÜRGEN; KRUSE, BERND; CORDES, CHRISTOPH
To: AIRBUS OPERATIONS GMBH
Reel/Frame 042416/0054 →
Priority Claims (1)
EP 16170361 · May 19, 2016 · regional
Continuity (1)
Related Publication 20170334540A1 · Nov 23, 2017