Surveillance window

• US 7,286,289 B2
• Filed: 03/05/2007
• Issued: 10/23/2007
• Est. Priority Date: 11/21/2001
• Status: Expired due to Term

• Current Assignee: Thales Avionics Incorporated (Thales SA)
• Original Assignee: Thales Avionics Incorporated (Thales SA)
• Inventors: Grich, Richard, Bengoechea, Xavier, Finizio, Francesco
• Primary Examiner(s): LAVARIAS, ARNEL C
• Application Number:
  US11/713,967
• Publication Number:
  US 20070159695A1
• Time in Patent Office: 232 Days
• Field of Search: None
• US Class Current: 359/485.04
• CPC Class Codes: G02B 27/28 for polarising used in stereoscopes G02B30/25
• CPC Class Codes: G08B 13/19626 optical details, e.g. lenses, mirrors or multiple lenses

Abstract

A surveillance window including at least one set of linear polarizer and quarter-waveplate and a reflecting surface. The surveillance window appears dull and opaque to a subject, while allowing a relatively high percentage of light to be transmitted to an observer. Various enhancements including an illuminator and detector, camouflaging, fire resistance, and improvements to the opacity are also described.

Claims

1. A camera system for aircraft, the system comprising:

a sign that disguises the camera system, the sign comprising a plate, and lettering disposed on the plate;

an aircraft interior surface on which the sign is disposed;

a first circular polarizer having a linear polarizer side and a quarter-waveplate side, the linear polarizer side being attached to the plate of the sign;

a second circular polarizer having a linear polarizer side and a quarter-waveplate side, the linear polarizer side disposed such that it is coextent with, proximate to, and substantially parallel to the first circular polarizer, with its linear polarizer side facing the quarter-waveplate side of the first circular polarizer;

a structural supporting plate disposed behind the second circular polarizer, the structural supporting plate having an aperture; and

a surveillance camera extending at least partly through the aperture.

2. The camera system of claim 1, wherein the system is mounted proximate to the entrance of an aircraft.

3. The camera system of claim 1, wherein the lettering on the sign comprises the letters of the word EXIT.

4. The camera system of claim 1, wherein the plate of the sign is a first flame retardant plate, the system further comprising a second flame retardant plate disposed on the quarter-waveplate side of the second circular polarizer, and wherein the structural supporting plate is attached to the second flame retardant plate.

5. A camera system for an aircraft, the camera system comprising:

a front plate having lettering applied thereon;

a front circular polarizer having a linear polarizer side and a quarter-waveplate side, the linear polarizer side being disposed behind and bonded to the plate;

a rear circular polarizer having a linear polarizer side and a quarter-waveplate side, the linear polarizer side of the rear circular polarizer being adjacent to the quarter-waveplate side of the front circular polarizer, and the slow axes of the quarter-waveplate sides of the front circular polarizer and the rear circular polarizer being substantially parallel;

a rear plate disposed behind, and bonded to the rear circular polarizer, the rear plate being attached to an interior surface of the aircraft; and

a camera positioned to receive light that passes through the front and rear circular polarizers.

6. The camera system of claim 5, wherein the system is mounted proximate to the entrance of the aircraft.

7. The camera system of claim 5, wherein the front plate and rear plates are flame retardant.

8. The system of claim 5, wherein the front and rear circular polarizers are made of a polymer-based material.

9. The system of claim 5, wherein the front and rear circular polarizers are made of a birefringent material.

10. A camera system for an aircraft, the camera system comprising:

a front polycarbonate plate having a front surface and a back surface, lettering being applied to the back surface;

a front circular polarizer having a linear polarizer side and a quarter-waveplate side, the linear polarizer side being disposed behind and bonded to the back surface of the front polycarbonate plate with clear adhesive;

a rear circular polarizer having a linear polarizer side and a quarter-waveplate side, the linear polarizer side of the rear circular polarizer being adjacent to the quarter-waveplate side of the front circular polarizer, and the slow axes of the quarter-waveplate sides of the front circular polarizer and the rear circular polarizer being substantially parallel;

an aluminum plate disposed behind, and bonded to the rear circular polarizer, the aluminum plate having an aperture, the aluminum plate being mounted to a surface of the aircraft; and

a camera that receives light through the aperture.

11. The system of claim 10, wherein the front and rear circular polarizers are made of a polymer-based material.

12. The system of claim 10, wherein the front and rear circular polarizers are made of a birefringent material.

13. The system of claim 10, wherein the lettering is silk-screened onto the front polycarbonate plate.

14. The system of claim 10, wherein the lettering is positioned so that it does not obstruct the view of the camera.

15. The system of claim 10, wherein the aluminum plate is mounted to the aircraft surface with double-sided tape.