Abstract: The present disclosure makes use of the fact that passengers have ways of adjusting the temperature in their immediate environment or indicating their level of comfort or discomfort and uses information about the passengers' use of the temperature control capabilities in their immediate environment and/or indications of their level of comfort/discomfort as an input to a controller of an environmental control system (ECS) to automatically adjust the ECS supply air temperature set point.
Type:
Grant
Filed:
December 1, 2021
Date of Patent:
May 21, 2024
Assignee:
Collins Aerospace Ireland, Limited
Inventors:
Mathieu Le Cam, Giovanni Franzini, Tejaswinee Darure
Abstract: An architecture that provides automatic monitoring of brake conditions making use of a wear pin on a brake. The disclosure makes use of the fact that a wear pin is required to be provided on an aircraft brake, by integrating monitoring functions such as displacement sensors and/or temperature sensors, into the pin. This means that the automatic monitoring components are not taking up more space on the brake than is already taken up by the compulsory wear pin.
Abstract: A series resonant power converter, comprising: a first plurality, m, of resonant power converter modules, each comprising a switching stage, a resonant tank, a transformer, a rectifier stage and an output capacitor, the plurality of resonant power converter modules connected in series across a power supply, the resonant power converter further comprising a common output stage (500) connected across the series-connected plurality of resonant power converter modules, whereby a second plurality, n, of output levels at the common output stage.
Abstract: An architecture that provides automatic monitoring of brake conditions making use of a wear pin on a brake. The disclosure makes use of the fact that a wear pin is required to be provided on an aircraft brake, by integrating monitoring functions such as displacement sensors and/or temperature sensors, into the pin. This means that the automatic monitoring components are not taking up more space on the brake than is already taken up by the compulsory wear pin.