Anti-bird-collision light

Patent metadata

Field	Value
Publication number	US-11021264-B2
Application number	US-201715648521-A
Country	US
Kind code	B2
Filing date	Jul 13, 2017
Priority date	Jul 15, 2016
Publication date	Jun 1, 2021
Grant date	Jun 1, 2021

Abstract

A helicopter anti-bird-collision system including a search light (2) and a control unit (35) which is configured for operating the search light (2) in a flash light mode by switching the search light periodically on and off.

First claim

The invention claimed is:

1. A method of operating a helicopter search light, which may be operated in a flood light mode and a spot light mode, as an anti-bird-collision light wherein the method includes: operating the helicopter search light in a flash light mode by periodically switching the helicopter search light, operating in the spot light mode, on and off; and moving a direction of light emission of the helicopter search light along an elliptic pathway such that a combination of light cones emitted by the helicopter search light when switched on covers the elliptic pathway substantially completely; wherein said moving of the direction of light emission over a full cycle along the elliptic pathway takes at most one second, and wherein the helicopter search light is operated to flash between 2 and 14 times during the moving of the direction of light emission over the full cycle.

2. The method according to claim 1 , wherein the elliptic cross section has a major axis and a minor axis and wherein the major axis is oriented horizontally.

3. The method according to claim 1 , wherein the major axis of the of the elliptic cross section corresponds to an angle of 40°.

4. The method according to claim 1 , wherein the helicopter search light is switched on and off while the direction of light emission of the helicopter search light moves along an elliptic pathway, wherein the helicopter search light in particular is switched on and off with a frequency such that the combination of light cones emitted by the helicopter search light covers the elliptic pathway substantially completely.

5. The method according to claim 2 , wherein the major axis is at least five times larger than the minor axis.

6. A helicopter anti-bird-collision system including: a helicopter search light, which may be operated in a flood light mode and a spot light mode; and a control unit which is configured for operating the helicopter search light as an anti-bird-collision light in a flash light mode by periodically switching the helicopter search light, operating in the spot light mode, on and off; wherein the helicopter search light has an adjustable direction of light emission and wherein the helicopter anti-bird collision system further comprises a drive unit which is configured for moving the direction of light emission of the helicopter search light; wherein the drive unit is configured for moving the direction of light emission of the helicopter search light along an elliptic pathway so that said moving of the direction of light emission of a combination of light cones over a full cycle along the elliptic pathway takes at most one second; and wherein the control unit is configured for operating the helicopter search light to flash between 2 and 14 times during the moving of the direction of light emission over the full cycle.

7. The helicopter anti-bird-collision system according to claim 6 , wherein the helicopter search light comprises at least one LED light source.

8. The helicopter anti-bird-collision system according to claim 6 , wherein the helicopter search light is configured to provide a light intensity of at least 300,000 cd, in particular a light intensity of at least 300,000 cd in a peak intensity direction and a light cone having a half beam angle of about 3°.

9. The helicopter anti-bird-collision system according to claim 6 , wherein the major axis of the elliptic cross section is oriented horizontally.

10. The helicopter anti-bird-collision system according to claim 6 , wherein the control unit is configured to switch the helicopter search light on and off while the direction of light emission of the helicopter search light moves along an elliptic pathway, wherein the control unit in particular is configured for switching the helicopter search light on and off with a frequency such that the light cones emitted by the helicopter search light in combination cover the elliptic pathway substantially completely.

Assignees

• Goodrich Lighting Systems Gmbh

Inventors

• Hessling-Von Heimendahl Andre

Classifications

• B64D2045/0095

  Devices specially adapted to avoid bird strike · CPC title

• B60Q1/46

  for giving flashing caution signals during drive, other than signalling change of direction, e.g. flashing the headlights {or hazard lights} · CPC title

• A01M29/10

  using light sources, e.g. lasers or flashing lights · CPC title

• B64D2203/00

  Aircraft or airfield lights using LEDs · CPC title

• B64D47/02 Primary

  Arrangements or adaptations of signal or lighting devices · CPC title