Claims
- 1. A means for lighting an underside of an airplane comprising:
- a light source positioned at a substantial distance from said airplane, said light source having a primary reflector positioned adjacent thereto; and
- a secondary reflector positioned to receive at least a portion of light from said light source and oriented to reflect at least a portion of said light from said light source onto said underside of said airplane.
- 2. The means of claim 1 wherein said light source is elevated relative to the secondary reflector.
- 3. The means of claim 1 wherein a single light source is used in combination with a single secondary reflector.
- 4. Means of claim 1 wherein the secondary reflector comprises a base, a reflecting surface, and mounting components to detachably mount the reflecting surface to the base.
- 5. The means of claim 4 wherein the base further comprises positioning components to allow the base to be moved across the surface.
- 6. The means of claim 5 wherein the positioning components consist of skids attached to the base.
- 7. The means of claim 5 wherein the positioning components comprise wheels.
- 8. The means of claim 4 wherein the reflecting surface consists of a surface which issues a defuse light pattern.
- 9. The device of claim 4 wherein the reflecting surface consists of a plurality of side-by-side elongated segments.
- 10. The means of claim 9 wherein each segment is V-shaped.
- 11. The means of claim 9 wherein several of the sections have a convex shaped surface.
- 12. A means for lighting an underside of an airplane comprising:
- a light source positioned at a substantial distance from said airplane, said light source having a primary reflector positioned adjacent thereto; and
- a first secondary reflector; and
- a second secondary reflector, said first secondary reflector positioned to receive at least a portion of light from said light source and reflect at least a portion of light onto said second secondary reflector, said second secondary reflector positioned to receive at least a portion of light from said first secondary reflector and reflect at least a portion of light onto said underside of said airplane.
- 13. A method of lighting the underside of an airplane comprising:
- directing a relatively controlled light source at a substantial distance from an airplane wing towards the plane;
- positioning and orienting a secondary reflector so that at least a portion of light from the light source is reflected from the secondary reflector to at least a portion of the underside of the airplane.
- 14. A method of claim 13 further comprising the step of configuring the secondary reflector to reflect light in a direction away from pilots and workmen.
- 15. A method of claim 13 further comprising the step of placing the secondary reflector means on a scaffold underneath the airplane.
- 16. The method of claim 13 comprising placing a plurality of light sources a substantial distance from an airplane and utilizing a plurality of secondary reflectors positioned nearer the airplane.
- 17. The method of claim 13 wherein the secondary reflector issues a diffuse beam.
- 18. The method of claim 13 wherein the secondary reflector consists of a plurality of elongated side-by-side segments.
- 19. The method of claim 17 wherein segments have a reflecting surface configured so that compositely a diffused beam pattern is issued with the perimeter of the beam pattern being sharply controlled and defined.
- 20. A method of lighting the underside of an airplane comprising:
- placing a light source a substantial distance away from and above an airplane, the light source directing a relatively controlled light beam towards the underside of the plane;
- reflecting the light beam from the light source at a location near the underside of the plane in a controlled and defined reflected pattern.
CROSS REFERENCE TO RELATED APPLICATIONS
This is a continuation-in-part of co-owned and Ser. No. 07/855,606, filed Mar. 20, 1992, now U.S. Pat. No. 5,337,221; which is a continuation-in-part of commonly owned and U.S. Ser. No. 07/820,486, filed Jan. 14, 1992, now U.S. Pat. No. 5,402,327; and a continuation-in-part application from co-owned and U.S. Ser. No. 08/004,693, filed Jan. 14, 1993, now U.S. Pat. No. 5,343,374; which was a divisional of U.S. Ser. No. 07/820,486, filed Jan. 14, 1992, now U.S. Pat. No. 5,402,327.
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Divisions (1)
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Date |
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Parent |
820486 |
Jan 1992 |
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Continuation in Parts (2)
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Number |
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855606 |
Mar 1992 |
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Parent |
820486 |
Jan 1992 |
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