Runway light
Latest Honeywell International Inc. Patents:
- Turbine blade tip geometry system and method for gas turbine engine
- ECAE processing for high strength and high hardness aluminum alloys
- BUTTON ASSEMBLY
- Systems and methods for simulating worst-case contention to determine worst-case execution time of applications executed on a processor
- One step process for manufacturing trifluoroiodomethane from trifluoroacetyl halide, hydrogen, and iodine
Description
FIG. 1 is a right side perspective view of an embodiment of the present invention;
FIG. 2 is a front plan view of the embodiment shown in FIG. 1;
FIG. 3 is a rear plan view of the embodiment shown in FIG. 1;
FIG. 4 is a top plan view of the embodiment shown in FIG. 1;
FIG. 5 is a bottom plan view of the embodiment shown in FIG. 1;
FIG. 6 is a right side plan view of the embodiment shown in FIG. 1; and,
FIG. 7 is a left side plan view of the embodiment shown in FIG. 1.
Claims
I claim the ornamental design for a runway light, as shown and described.
Referenced Cited
Patent History
Patent number: D475646
Type: Grant
Filed: Sep 18, 2001
Date of Patent: Jun 10, 2003
Assignee: Honeywell International Inc. (Morristown, NJ)
Inventor: Eduard Mashevsky (Redondo Beach, CA)
Primary Examiner: Marcus A. Jackson
Application Number: 29/148,279
Type: Grant
Filed: Sep 18, 2001
Date of Patent: Jun 10, 2003
Assignee: Honeywell International Inc. (Morristown, NJ)
Inventor: Eduard Mashevsky (Redondo Beach, CA)
Primary Examiner: Marcus A. Jackson
Application Number: 29/148,279
Classifications
Current U.S. Class:
D10/114
International Classification: 1005;
International Classification: 1005;