The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Aug. 06, 2024

Filed:

Sep. 07, 2023
Applicant:

Honeywell International Inc., Charlotte, NC (US);

Inventors:

Raghavendra Nagappa, Bangalore, IN;

Gokul Murugesan, Bangalore, IN;

Jyotismita Sahoo, Bangalore, IN;

Senthil Kumar S, Bangalore, IN;

Assignee:

HONEYWELL INTERNATIONAL INC., Charlotte, NC (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64D 45/00 (2006.01); B64C 27/32 (2006.01); F21V 7/00 (2006.01); F21V 23/02 (2006.01);
U.S. Cl.
CPC ...
B64D 45/00 (2013.01); B64C 27/32 (2013.01); F21V 7/0008 (2013.01); F21V 7/0091 (2013.01); F21V 23/02 (2013.01); B64D 2045/0095 (2013.01);
Abstract

A lighting system for an aircraft having at least one rotationally mounted propeller assembly that includes hub and a plurality of rotor blades extending radially away from the hub includes a light source and an optical element. The light source is mounted within the hub and is configured, upon being energized, to emit light in a first direction. The optical element is mounted within the hub and is disposed to receive the light emitted by the light source and is configured, upon receipt of the light, to redirect the light radially outward from the hub so that the light reflects off the rotor blades.


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