Summary:
The Ohio State University has developed a new technology that could reduce jet engine noise during takeoff and landing while not affecting the jet exhaust flow and thrust during cruising and thus improving fuel efficiency. Jet noise has been a major issue in commercial subsonic aircraft and in the development of supersonic aircraft for decades. Recently, encroachment of neighboring communities on military airports and landing strips has also created growing pressure to reduce community noise from the military aircraft. Noise radiation from the exhaust jet in an aircraft is the dominant component of noise during takeoff and a major component during landing. While chevrons and tabs have been researched for noise reduction for decades, they were very recently put in use in jet aircraft engines for noise reduction. Since these devices are simple geometric modifications at the nozzle exit, their pattern and strength cannot be changed, and they remain active during the entire flight even when they are not needed. As a result, they decrease the fuel efficiency during most of the fight. This technology utilizes localized arc filament plasma (LAFP) actuators that can be turned on and off as needed, and their pattern and strength can be changed to further reduce jet engine noise and improve fuel efficiency. In addition, LAFP actuators could manipulate instabilities in the jet to maximize their effectiveness.
Potential Applications:
LAFP actuators could be used in jet aircraft engines, large or small, commercial or military, for jet noise reduction.
Advantages:
LAFP actuators can modify the flow field on command and can be turned “on” and “off” to minimize required power and potential losses when actuation is necessary.
This results in:
- Noise reduction during takeoff and landing
- Improved fuel efficiency during cruising altitude
- Manipulation of the jet’s instabilities
In addition:
- LAFP actuators do not involve any moving parts.
- LAFP actuators do not change the geometry of the system/vehicle.
- LAFP actuators can control mixing and noise in the jet by either excitation of the flow instabilities, by generating stream-wise vortices of desired frequency and strength, or by a combination of the two techniques.
