CPC B64D 13/08 (2013.01) [B64D 2013/0614 (2013.01); B64D 2013/0618 (2013.01); B64D 2013/0644 (2013.01)] | 20 Claims |
1. An environmental control system for an aircraft, the environmental control system comprising:
an air cycle machine to produce cabin air for a cabin of the aircraft, the air cycle machine including a turbine and a heat exchanger;
a ram circuit, the heat exchanger disposed in the ram circuit;
a fan in the ram circuit to control air flow through the ram circuit and across the heat exchanger;
an electric motor; and
an overrunning clutch operatively coupled between the turbine and the electric motor to couple the turbine to the fan to enable the turbine to drive the fan during a first mode of operation and to decouple the turbine from the fan to enable the electric motor to drive the fan independent of the turbine during a second mode of operation.
|