Removable passive airflow oscillation device and system
A removable passive airflow oscillation device can be disposed within a pressurized wing structure utilized as a plenum. The passive airflow oscillation device can be a removable insert disposed into exterior vehicle surfaces with pressurization of a sealed chamber to provide the airflow. The device can include a cavity configured to receive the airflow from an ingress opening, direct the airflow therethrough to generate a predetermined oscillating airflow, and expel the oscillatory airflow from the egress opening. The removable passive airflow oscillation devices can provide quick and simple replacement and maintenance of damaged or clogged devices. The aft chamber of the flap seal can be sealed and pressurized to serve as a plenum providing the airflow to the actuators. The device can receive airflow, such as compressor air, and expel an oscillating airflow. Because each device is self-contained the number of devices and location thereof can vary by application.
1. A removable airflow oscillation device, comprising:
a body having an ingress opening and an egress opening;
a cavity disposed within the body and configured to receive an airflow from the ingress opening and expel an oscillatory airflow from the egress opening, wherein the body is configured to be inserted into an externally-accessible device slot on an exterior of a vehicle, wherein the body is individually removable from the externally-accessible device slot without removal of another removable airflow oscillation device; and
a protrusion extending from a first side of the body and configured to:
engage in sealing contact with an exterior surface of an external wall of the vehicle to create an airtight seal against the exterior surface of the external wall of the vehicle;
essentially continue a sweep angle of the external wall of the vehicle; and
prevent the body from passing entirely through the externally-accessible device slot on the exterior surface of the external wall of the vehicle while the body is being inserted into the externally-accessible device slot.
2. The removable airflow oscillation device of claim 1 , wherein the vehicle is an aircraft.
3. The removable airflow oscillation device of claim 2 , wherein the aircraft is a rotorcraft.
4. The removable airflow oscillation device of claim 1 , wherein the device slot is disposed in a flap seal of an aircraft.
5. The removable airflow oscillation device of claim 1 , wherein the oscillation device is 3-D printed.
6. The removable airflow oscillation device of claim 5 , wherein the oscillation device is 3-D printed using Polyetherimide (PEI) or polyaryletherketone (PAEK) material.
7. The removable airflow oscillation device of claim 1 , wherein the oscillation device is made of metal.
8. The removable airflow oscillation device of claim 1 , wherein the body is configured to be slidably insertable into the externally-accessible device slot of the exterior of the vehicle.
9. A removable airflow oscillation system, comprising:
an oscillation device, including:
a body having an ingress opening and an egress opening;
a cavity disposed within the body and configured to receive an airflow from the ingress opening, oscillate the airflow, and expel the oscillatory airflow from the egress opening; and
a protrusion extending from a first side of the body and configured to:
engage in sealing contact with an exterior surface of an external wall of an aircraft to create an airtight seal against the exterior surface of the external wall of the aircraft;
essentially continue a sweep angle of the external wall of the aircraft; and
prevent the body from passing entirely through one or more externally-accessible device slots on the exterior surface of the external wall of the aircraft while the body is being inserted into the one or more externally-accessible device slots; and
the aircraft having the one or more externally-accessible device slots on its exterior, the one or more externally-accessible device slots configured to removably receive the oscillation device, wherein the oscillation device is individually removable from the one or more externally-accessible device slots without removal of another removable airflow oscillation device from the one or more externally-accessible device slots.
10. The removable airflow oscillation system of claim 9 , wherein the device slot is disposed in a wall of a chamber.
11. The removable airflow oscillation system of claim 10 , wherein the chamber is configured to removably receive the oscillation device.
12. The removable airflow oscillation system of claim 10 , wherein the chamber is sealed and pressurized to serve as a plenum providing the airflow to the egress opening of the oscillation device.
13. The removable airflow oscillation system of claim 10 , wherein the egress opening is configured to essentially continue a shape of the external wall of the aircraft.
14. The removable airflow oscillation system of claim 3 , wherein the external wall continues the shape of the egress opening to maintain the sweep angle.
15. The removable airflow oscillation system of claim 10 , wherein the chamber is disposed within a flap seal of the aircraft.
16. The removable airflow oscillation system of claim 9 , wherein the oscillation device is 3-D printed.
17. The removable airflow oscillation system of claim 16 , wherein the oscillation device is 3-D printed using Polyetherimide (PEI) or polyaryletherketone (PAEK) material.
18. The removable airflow oscillation system of claim 9 , wherein the oscillation device is made of metal.
19. The removable airflow oscillation system of claim 9 , wherein the oscillation device is configured to be slidably insertable into the one or more externally-accessible device slots.