Dual mode aircraft light assembly

1. A dual mode light assembly for a position light of an aircraft, the dual mode light assembly comprising:

a base;

a visible light source mounted to the base and configured to emit visible light;

a covert light source mounted to the base and configured to emit covert light; and

at least one light shield mounted to the base and configured to restrict transmission of the visible light to a visible light pattern and to restrict transmission of the covert light to a covert light pattern;

wherein:

the position light is a forward position light

the at least one light shield is a single light shield; and

the visible light source is outboard and laterally offset relative to the single light shield such that inboard transmission of the visible light is blocked by the single light shield.

2. The dual mode light assembly of claim 1 , wherein the visible light pattern is bounded by a blocking element of at least one of the dual mode light assembly and the aircraft, wherein a horizontal angle of the visible light pattern between the single light shield and the blocking element is at least 110 degrees but less than 120 degrees.

3. The dual mode light assembly of claim 2 , wherein the blocking element comprises a blocking surface of the base.

4. The dual mode light assembly of claim 3 , wherein the base is angled in an aft direction.

5. The dual mode light assembly of claim 1 , wherein the single light shield is disposed below the covert light source on the base to block downward transmission of the covert light.

6. The dual mode light assembly of claim 5 , wherein a vertical angle of the covert light pattern between a horizontal plane and the single light shield is at most 45 degrees downwards.

7. The dual mode light assembly of claim 1 , further comprising a reflector mounted to the base configured to reflect the covert light in an aft direction such that a horizontal angle of the covert light pattern from a line of flight of the aircraft is at least 120 degrees.

8. The dual mode light assembly of claim 7 , wherein the reflector is laterally offset relative to the covert light source on the base to block inboard transmission of the covert light.

9. The dual mode light assembly of claim 1 , wherein the visible light source comprises multiple light emitting diodes vertically aligned across the base.

10. The dual mode light assembly of claim 1 , wherein the covert light source comprises an infrared emitter.

11. The dual mode light assembly of claim 1 , wherein the visible light source is both vertically and horizontally offset from the covert light source.

12. The dual mode light assembly of claim 1 , wherein the visible light source is laterally offset relative to the covert light source.

13. The dual mode light assembly of claim 1 , wherein the single light shield comprises an arch structure extending outward and across the base, wherein components of the base are mounted to the base in a span of the arch structure.

14. The dual mode light assembly of claim 1 , wherein the single light shield is separate from a housing of the dual mode light assembly.

15. A dual mode light assembly for a position light of an aircraft, the dual mode light assembly comprising:

a base;

a visible light source mounted to the base and configured to emit visible light

a covert light source mounted to the base and configured to emit covert light and

at least one light shield mounted to the base and configured to restrict transmission of the visible light to a visible light pattern and to restrict transmission of the covert light to a covert light pattern;

wherein:

the position light is an aft position light;

the at least one light shield comprises a first light shield and a second light shield;

the first light shield is configured to restrict transmission of the visible light such that a horizontal angle of the visible light pattern is 120 degrees; and

the second light shield is configured to restrict transmission of the covert light such that a vertical angle of the covert light pattern between a horizontal plane and the second light shield is at most 45 degrees downwards.

16. The dual mode light assembly of claim 15 , wherein the first light shield extends in an aft direction from peripheral edges of an aft facing surface of the base.

17. The dual mode light assembly of claim 15 , wherein the visible light source comprises multiple light emitting diodes disposed around the covert light source.

18. A dual mode light assembly for a position light of an aircraft, the dual mode light assembly comprising:

a base;

a visible light source mounted to the base and configured to emit visible light;

a covert light source mounted to the base and configured to emit covert light; and

at least one light shield mounted to the base and configured to restrict transmission of the visible light to a visible light pattern and to restrict transmission of the covert light to a covert light pattern;

wherein the visible light pattern is bounded by a blocking element of at least one of the dual mode light assembly and the aircraft, wherein a horizontal angle of the visible light pattern between the at least one light shield and the blocking element is at least 110 degrees but less than 120 degrees.

19. The dual mode light assembly of claim 18 , wherein the position light is a forward position light and wherein the at least one light shield is a single light shield that is laterally offset relative to the visible light source on the base to block inboard transmission of the visible light.

20. The dual mode light assembly of claim 18 , further comprising a reflector mounted to the base configured to reflect the covert light in an aft direction such that a horizontal angle of the covert light pattern from a line of flight of the aircraft is at least 120 degrees.