Strobe light unit and aircraft comprising the same

Patent metadata

Field	Value
Publication number	US-9327843-B2
Application number	US-201414249934-A
Country	US
Kind code	B2
Filing date	Apr 10, 2014
Priority date	May 6, 2013
Publication date	May 3, 2016
Grant date	May 3, 2016

Abstract

A strobe light unit, particularly wing anti-collision strobe light unit for an aircraft, comprises at least one light source, particularly at least one LED; a reflector element, the at least one light source and the reflector element being configured for projecting light into a desired range of directions; and a stray light blocking element for blocking stray light from being projected into undesired directions, the stray light blocking element attached to the reflector element or to a base portion of the strobe light unit.

First claim

What is claimed is:

1. A wing anti-collision strobe light unit for an aircraft, comprising:
at least one light source, particularly at least one LED;
a reflector element,
the at least one light source and the reflector element being configured for projecting light into a desired range of directions; and
a stray light blocking element for blocking stray light from being projected into undesired directions, the stray light blocking element attached to the reflector element or to a base portion of the strobe light unit;

wherein the stray light blocking element comprises a substantially planar main portion, which substantially planar main portion extends into a radial direction from the at least one light source, such that at least one of parallel and radial light beams projected into the desired range of directions are substantially unaffected by the stray light blocking element and such that stray light beams of an undesired range of directions, particularly stray light beams reflected by an additional transparent cover or an additional cover lens, are blocked; and
wherein the substantially planar main portion of the stray light blocking element includes an angle of 30 to 60° with respect to an axis of symmetry of the reflector element.

2. Strobe light unit of claim 1 , wherein the at least one light source and the reflector element are configured for projecting light beams into a desired range of directions.

3. Strobe light unit of claim 1 , having at least one of the following features:
the substantially planar main portion of the stray light blocking element is oriented at an angle with respect to a vertical plane such that the forward face shows in a direction obliquely upwards, and
the substantially planar main portion of the stray light blocking element is oriented at an angle with respect to a horizontal plane such that the forward face shows in a direction to the inner side of the airplane, and particularly roughly into the direction of the cockpit.

4. Strobe light unit of claim 1 , having at least one of the following features:
the reflector element comprises a substantially arcuate shape and a reflecting inner surface, and
the at least one light source is arranged in front of the reflecting inner surface.

5. Strobe light unit of claim 4 , wherein the at least one light source is arranged within a space spanned by the inner surface of the reflector element and a straight line connecting the end portions of the inner surface.

6. Strobe light unit of claim 5 , wherein at least a rear end of the stray light blocking element is arranged in front of one end portion of the reflector element and/or in front of a lateral portion of said space.

7. Strobe light unit of claim 1 , having at least one of the following features:
at least the main portion of the stray light blocking element is made of a material that is at least one of flexible and non-transparent, particularly of a plastics material that is at least one of flexible and non-transparent, and
at least the main portion of the stray light blocking element is mounted to the reflector element or to the base portion of the strobe light unit in a flexible manner.

8. Strobe light unit of claim 1 , wherein two or more light heads, each comprising at least one light source, particularly at least one LED, and a reflector element, are provided; and wherein one joint stray light blocking element is provided for the two or more light heads or wherein separate stray light blocking elements are provided for each of the light heads.

9. Strobe light unit of claim 1 , further comprising a cover lens, particularly a substantially arcuate shaped cover lens, positioned, in optical direction, in front of the at least one light source and of the reflector element.

10. Strobe light unit of claim 9 , wherein the main portion of the stray light blocking element has a rear end and a front end, seen in optical direction, the rear end being arranged in vicinity to one end portion of the reflector element, and the front end arranged close to or at the inner surface of the cover lens.

11. Aircraft comprising a cockpit and at least one strobe light unit arranged as a wing anti-collision strobe light unit, the strobe light including:
at least one light source, particularly at least one LED;
a reflector element,
the at least one light source and the reflector element being configured for projecting light into a desired range of directions; and
a stray light blocking element for blocking stray light from being projected into undesired directions, the stray light blocking element attached to the reflector element or to a base portion of the strobe light unit;
wherein the stray light blocking element is arranged at the side of the strobe light unit oriented towards the cockpit, such that those stray light beams that are projected by the at least one light source and reflected by the cover lens into a direction towards the cockpit are blocked from reaching the cockpit.

12. Aircraft of claim 11 , wherein the substantially planar main portion of the stray light blocking element is oriented at an angle of +20° to −10° with respect to the flight direction.

13. Aircraft of claim 12 , wherein the at least one light source is arranged at an angle with respect to a horizontal plane.

14. Aircraft of any of claim 11 , wherein the at least one light source and the reflector element are oriented vertically or horizontally.

15. A wing anti-collision strobe light unit for an aircraft, comprising:
at least one light source, particularly at least one LED;
a reflector element,
the at least one light source and the reflector element being configured for projecting light into a desired range of directions; and
a stray light blocking element for blocking stray light from being projected into undesired directions, the stray light blocking element attached to the reflector element or to a base portion of the strobe light unit;
wherein the stray light blocking element comprises a substantially planar main portion, which substantially planar main portion extends into a radial direction from the at least one light source, such that at least one of parallel and radial light beams projected into the desired range of directions are substantially unaffected by the stray light blocking element and such that stray light beams of an undesired range of directions, particularly stray light beams reflected by an additional transparent cover or an additional cover lens, are blocked; and
wherein the wing anti-collision strobe light unit has at least one of the following features:
the substantially planar main portion of the stray light blocking element is oriented at an angle with respect to a vertical plane such that the forward face shows in a direction obliquely upwards, and
the substantially planar main portion of the stray light blocking element is oriented at an angle with respect to a horizontal plane such that the forward face shows in a direction to the inner side of the airplane, and particularly roughly into the direction of the cockpit.

16. Strobe light unit of claim 15 , wherein the at least one light source and the reflector element are configured for projecting light beams into a desired range of directions.

17. Strobe light unit of claim 15 , having at least one of the following features:
the reflector element comprises a substantially arcuate shape and a reflecting inner surface, and
the at least one light source is arranged in front of the reflecting inner surface.

18. Strobe light unit of claim 17 , wherein the a

Assignees

• Goodrich Lighting Systems Gmbh

Inventors

• Jha Anil Kumar
• Schoen Christian
• Hessling Andre

Classifications

• B64D2203/00

  Aircraft or airfield lights using LEDs · CPC title

• B64D47/06 Primary

  for indicating aircraft presence · CPC title