Safran Seats Gb Limited

Julian Guy

Rachel James

Huang-Yu Teh

An aircraft passenger suite is provided. The suite comprises an aircraft seat for use by a passenger. The suite also comprises a controller for controlling a number of output states of the suite, the controller comprising a logic condition receiver operable to receive a logic condition input. The suite also comprises sensor equipment operable to provide a sensor input to the controller, the sensor input providing an indication of at least one attribute of a passenger of the suite. The sensor equipment comprises one or more of: an image sensor a pressure sensor and a physiological sensor. The controller is configured to control at least one of the output states of the suite based on both the logic condition input and the sensor input.

Intelligent settings of an aircraft passenger suite

A method of configuring an aircraft electrical system. The aircraft electrical system comprises a wiring harness and a plurality of electronic modules. The wiring harness comprises a plurality of connection points. The method comprises: connecting a first electronic module in the plurality to the wiring harness via a first connection point in the plurality; transmitting by the first electronic module, a connection point identification request; in response to the transmitting, receiving at the first electronic module from the wiring harness, an identifier of the first connection point; on the basis of the received identifier, determining configuration data for the first electronic module, the configuration data being associated with the first connection point; and configuring the first electronic module to operate in accordance with the determined configuration data.

Aircraft electrical system

Described is an aircraft suite having an aircraft seat for use by a passenger, the aircraft suite also having a controller, for controlling a number of output states of the aircraft suite, the controller having a logic condition receiver for receiving a logic condition input, and distance measurement equipment for measuring a distance between a first location within the suite and a second location within the suite, and providing a distance input to a distance receiver of the controller, wherein, in use, the controller controls at least one of the output states of the aircraft suite based upon both the logic condition input and the distance input. The invention also provides a method of controlling an environment within an aircraft suite.

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Cwmbran, United Kingdom

Julian Guy