Abstract: An electro-thermal ice protection system includes a controller for managing and controlling electrical power generated to heat and de-ice surfaces, such as aircraft wings. The system is comprised of a number of power control modules (PCMs) and at least one master control unit (MCU). These elements can be stacked together and mounted into rack systems in order to provide scalable organized power distribution for a de-icing and ice protection system. The electro-thermal system can be used with a load leveling system and method capable of controlling switches such that it appears to a generator that the load is constant. Switches can be scheduled such that, ideally, the power load seen by the power source has emissions of no more than one PWM load superpositioned with zero or more constant, non-modulated loads.

Abstract: An electro-thermal ice protection system includes a controller for managing and controlling electrical power generated to heat and de-ice surfaces, such as aircraft wings. The system is comprised of a number of power control modules (PCMs) and at least one master control unit (MCU). These elements can be stacked together and mounted into rack systems in order to provide scalable organized power distribution for a de-icing and ice protection system. The electro-thermal system can be used with a load leveling system and method capable of controlling switches such that it appears to a generator that the load is constant. Switches can be scheduled such that, ideally, the power load seen by the power source has emissions of no more than one PWM load superpositioned with zero or more constant, non-modulated loads.

Abstract: An electro-thermal wing ice protection solution controller for managing and controlling electrical power generated to heat and de-ice the wing of an aircraft. The system is comprised of a number of power control modules (PCMs) and at least one master control unit (MCU). These elements can be stacked together and mounted into rack systems in order to provide scalable organized power distribution for a wing de-icing and ice protection system.

Abstract: An electro-thermal wing ice protection solution controller for managing and controlling electrical power generated to heat and de-ice the wing of an aircraft. The system is comprised of a number of power control modules (PCMs) and at least one master control unit (MCU). These elements can be stacked together and mounted into rack systems in order to provide scalable organized power distribution for a wing de-icing and ice protection system.

Abstract: Embodiments of the present invention provide a system (10) operable to provide power and control through a rotating interface. The system (10) generally includes a control unit (12) and a distributor unit (14). The control unit (12) is operable to generate a power signal having a plurality of power transitions. The distributor unit (14) is operable to rotatably couple with the control unit (12), receive the power signal from the control unit (12), identify power transitions within the power signal, and generate a plurality of output signals corresponding to the identified power transitions. The distributor unit (14) is also at least substantially powered by the power signal to enable generation of the output signals.

Abstract: Embodiments of the present invention provide a system (10) operable to provide power and control through a rotating interface. The system (10) generally includes a control unit (12) and a distributor unit (14). The control unit (12) is operable to generate a power signal having a plurality of power transitions. The distributor unit (14) is operable to rotatably couple with the control unit (12), receive the power signal from the control unit (12), identify power transitions within the power signal, and generate a plurality of output signals corresponding to the identified power transitions. The distributor unit (14) is also at least substantially powered by the power signal to enable generation of the output signals.

Abstract: Embodiments of the present invention provide a system (10) operable to provide power and control through a rotating interface. The system (10) generally includes a control unit (12) and a distributor unit (14). The control unit (12) is operable to generate a power signal having a plurality of power transitions. The distributor unit (14) is operable to rotatably couple with the control unit (12), receive the power signal from the control unit (12), identify power transitions within the power signal, and generate a plurality of output signals corresponding to the identified power transitions. The distributor unit (14) is also at least substantially powered by the power signal to enable generation of the output signals.