AFT inlet duct mounted door actuator
An inlet door system including an aft inlet duct mounted door actuator providing RAM air to an auxiliary power unit (APU) contained within an aircraft is provided. The inlet door system includes an inlet duct, the aft inlet duct mounted door actuator, and a door. The inlet duct is configured to extend from the auxiliary power unit to the aircraft housing and has a sidewall that defines a flow passage. The door actuator is mounted to an exterior surface of the aft portion of the inlet duct. The door is coupled to the actuator. The actuator is configured to selectively rotate the door between at least a first position and a second position.
1. An inlet door system providing RAM air to an auxiliary power unit (APU) and APU compartment contained within an aircraft, the inlet door system comprising:
a duct configured to extend from the auxiliary power unit (APU) to an intake opening formed in an outer surface of the aircraft, the duct having an inlet port, an outlet port, and a duct sidewall extending from the inlet port to the outlet port, the duct sidewall defining an air flow passage therebetween the inlet port and the outlet port;
a door having a first end and a second end, the door rotationally coupled at the first end to the duct sidewall and positioned to sealingly engage with the inlet port and configured to selectively rotate between at least a first position and a second position; and
an actuator mounted to an exterior surface of an aft portion of the duct and including an extension rod, the extension rod coupled to the first side of the door, the actuator configured to push and pull on the extension rod to thereby rotate the door to at least the first position and the second position, respectively, without the actuator, the extension rod, nor any other structure connected to both the actuator and the door, extending into the air flow passage.
2. The inlet door system of claim 1 , further comprising a forked component coupled between the extension rod and the first side of the door, the forked component configured to provide symmetrical door loading.
3. The inlet door system of claim 1 , further including a mounting bracket to mount the actuator to the aft portion of the duct.
4. The inlet door system of claim 1 , wherein the actuator is a linear actuator.
5. The inlet door system of claim 1 , wherein the actuator is located to provide maintenance access thereto via the APU compartment.
6. The inlet door system of claim 1 , wherein the actuator is configured to selectively raise and lower the door to deflect APU noise within the air flow passage.