Method for cooling a tilter motor including a tilt-actuated nacelle door
A VTOL aircraft includes a plurality of tilt propellers configured to be rotated between a forward cruise configuration and a vertical lift configuration. A nacelle or other structure may be configured to form a low pressure zone from the wake of the tilt propellers when operating in the lift configuration. The low pressure zone may include an outlet side of a cooling path. Due to the low pressure, airflow may be induced through the cooling path even in the absence of strong air pressure at the inlet side. During a cruise operation when the VTOL aircraft is in forward motion, the nacelle or other structure may be aligned with a baffle to form an exhaust channel for the cooling airflow.
1. A method of operating a tilt apparatus of a vertical takeoff and landing (VTOL) craft, comprising:
tilting a motor assembly, a nacelle, and a propeller with respect to a body into a lift configuration by a tilt actuator, the motor assembly being coupled to the propeller and to the nacelle, the nacelle comprising a door;
actuating the door to a first position with the tilting of the nacelle and the propeller into the lift configuration;
directing propwash from the propeller to an air inlet of the nacelle and further to a thermal transfer device that is thermally coupled to the motor assembly when the propeller is in the lift configuration;
tilting the motor assembly, the nacelle, and the propeller from the lift configuration to a cruise configuration; and
actuating the door to a second position with the tilting of the nacelle and the propeller into the cruise configuration,
wherein actuating the door to the first position or the second position causes an opening size of the air inlet of the nacelle to be larger in the first position than in the second position.
2. The method of claim 1 , further comprising:
actuating the door between the first position and the second position by a mechanical coupling between the door and the tilt actuator.
3. The method of claim 1 , wherein the door is closed in the second position.
4. The method of claim 1 , wherein the door is located at a top portion of the nacelle as viewed in the cruise configuration.
5. The method of claim 1 , wherein the thermal transfer device comprises a heat exchanger that is thermally coupled to the motor assembly by an oil flow path.
6. The method of claim 1 , further comprising:
directing propwash from the propeller to the thermal transfer device via a baffle.
7. The method of claim 1 , further comprising:
directing propwash from the propeller to an additional air inlet of the nacelle and further to the thermal transfer device when the propeller is operated in the cruise configuration.
8. The method of claim 1 , wherein the door and the air inlet are each located at a side portion of the nacelle as viewed in the cruise configuration.
9. The method of claim 8 , further comprising:
directing propwash from the propeller to the thermal transfer device via a baffle.
10. The method of claim 1 , wherein the thermal transfer device comprises cooling fins.
11. The method of claim 1 , wherein the thermal transfer device comprises a heat exchanger.
12. The method of claim 11 , wherein the heat exchanger is thermally coupled to the motor assembly by an oil flow path.
13. The method of claim 1 , wherein the nacelle comprises a plurality of clamshell segments and actuating the door comprises actuating one of the clamshell segments.
14. The method of claim 1 , further comprising: actuating a plurality of clamshell segments with the tilting of the nacelle and the propeller into the lift configuration.