Electric fan
AssigneePratt & Whitney Canada Corp.
InventorDavid H. Menheere
Life of this patent
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Abstract
An electric fan for producing thrust to propel an aircraft is disclosed. The electric fan comprises a stator, a fan rotor rotatably mounted relative to the stator and an electric motor mounted to the stator and drivingly engaged with the fan rotor to cause rotation of the fan rotor relative to the stator. The fan rotor comprises an annular body defining a flow passage therethrough and a plurality of fan blades disposed in the flow passage and mounted for common rotation with the annular body about a fan rotation axis. The electric motor has a motor rotation axis that differs from the fan rotation axis.
Claims6
A method of operating an electric fan mounted to an aircraft, the method comprising:
- electrically driving a bladed rotor of the electric fan to rotate in a first direction to generate forward thrust to propel the aircraft;
- electrically driving the bladed rotor of the electric fan to rotate in a second direction opposite the first direction to generate reverse thrust;
- during a descent phase of the aircraft:
- ceasing to electrically drive the bladed rotor to rotate in the first direction:
- allowing windmilling of the bladed rotor;
- and
- generating electricity from the windmilling of the bladed rotor.
A method of operating an electric fan mounted to an aircraft, the method comprising:
- electrically driving a bladed rotor of the electric fan to rotate in a first direction to generate forward thrust to propel the aircraft;
- and
- electrically driving the bladed rotor of the electric fan to rotate in a second direction opposite the first direction to generate reverse thrust, wherein:
- the bladed rotor is a first bladed rotor disposed in a fluid passage;
- the electric fan comprises a second bladed rotor disposed in the fluid passage;
- and
- the method comprises driving the first and second bladed rotors at different rotational speeds when generating forward thrust.
Dependencies are inferred from the claim text.