Sound reduction method and system for jet engines

Electrical audio signal processing systems and devices – Acoustical noise or sound cancellation – Counterwave generation control path

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

381 718, A61F 1106, H03B 2900

Patent

active

059664525

ABSTRACT:
A method and apparatus for reducing acoustic noise waves in the vicinity of an electrically conductive plasma, such as in the exhaust of a gas turbine engine, having a sensor to detect the noise wave and generate a representative electrical noise signal; a signal analyzer to analyze the noise signal, a wave form generator to generate a phase inverted, electrical interference signal based on the noise signal, an amplifier, a time delay, an error corrector; and an applying means to conduct the electrical interference signal to the plasma causing the plasma to generate a pulsating interference wave to cancel the acoustic noise wave.

REFERENCES:
patent: 3792584 (1974-02-01), Klees
patent: 3936606 (1976-02-01), Wanke
patent: 5127602 (1992-07-01), Batey et al.
patent: 5363450 (1994-11-01), Moody
patent: 5386689 (1995-02-01), Bozich et al.
patent: 5402963 (1995-04-01), Carey et al.
patent: 5410607 (1995-04-01), Mason et al.
patent: 5414230 (1995-05-01), Nieuwendijk et al.
patent: 5440875 (1995-08-01), Torkelson et al.
patent: 5466899 (1995-11-01), Geisenberger
Shirley, Gerald "The Corona Wind Loudspeake" Journal of the Audio Engineering Society, D.M. Tombs, Nature, 176, 923 (1955) pp. 29-37.

LandOfFree

Say what you really think

Search LandOfFree.com for the USA inventors and patents. Rate them and share your experience with other people.

Rating

Sound reduction method and system for jet engines does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Sound reduction method and system for jet engines, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Sound reduction method and system for jet engines will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFUS-PAI-O-659881

  Search
All data on this website is collected from public sources. Our data reflects the most accurate information available at the time of publication.