Turbo air compressor

摘要

A method for operating an air-conditioning system for an aircraft including receiving an available power level from a control system of the aircraft, forwarding air from a first compressed air source to an aircraft cabin and forwarding air from a second compressed air source to the aircraft cabin if the available power level exceeds a threshold value.

主权项

1. A method for operating an air-conditioning system for an aircraft comprising:
receiving an available power level from a control system of the aircraft; forwarding air from a first compressed air source to an aircraft cabin; and based on determining that the available power level exceeds a threshold value, forwarding air from a second compressed air source to the aircraft cabin, wherein a portion of air from the second compressed air source that is forwarded to the aircraft cabin is based upon the available power level; the air-conditioning system of the aircraft cabin also includes a discharge device controller, the controller is configured to instruct the discharge device to forward the circulated air from the aircraft cabin to the turbine if the difference in the ambient air pressure and the cabin air pressure exceeds a threshold value and to forward the circulated air from the aircraft cabin out of the aircraft if the difference in the ambient air pressure and the cabin air pressure is below a threshold value.