B/e Aerospace, Inc.

Simon Robert Lee

R Klaus Brauer

Ian L Frost

John Warren

Steven Mark Hanley

Graham Nigel Hildyard

A system for light source calibration and aging compensation is disclosed. In one or more embodiments, the system includes a light source driver, a sensor, and a controller. The light source driver is configured to generate one or more power signals for a plurality of light sources. The sensor is configured to detect an illumination power output by at least one light source of the plurality of light sources. The controller is communicatively coupled to the sensor and the light source driver. The controller is configured to compare the illumination power detected by the sensor to a target illumination power. The controller is further configured to generate one or more control signals to adjust an electrical power output of the light source driver based on the comparison of the illumination power detected by the sensor to the target illumination power.

Light source calibration and aging compensation system

A system. The system may include a glare shield positioned between an exterior pane of an aircraft window and an interior portion of an aircraft. The glare shield may include at least one anti-reflective mask and at least one viewing aperture. Each of the at least one anti-reflective mask may be positioned adjacent one of the at least one viewing aperture.

Apparatus and method for providing attitude reference for vehicle passengers

A system. The system may include at least one monitor mounted on a wall panel. The wall panel may be within an interior of an aircraft. Each of the at least one monitor may be configured to mimic an aircraft window. Each of the at least one monitor may include a shade feature.

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Southampton, United Kingdom

Simon Robert Lee