Active noise control system for aircraft, and method for enhancing pilot situational awareness

• US 7,383,106 B1
• Filed: 05/31/2005
• Issued: 06/03/2008
• Est. Priority Date: 05/31/2005
• Status: Expired due to Fees

• Current Assignee: Lester C. Coonse Jr
• Original Assignee: Lester C. Coonse Jr
• Inventors: Coonse, Lester C. Jr.
• Primary Examiner(s): Tran; Dalena
• Application Number:
  US11/141,279
• Time in Patent Office: 1,099 Days
• Field of Search: 701/10, 381/71.2, 381/73.1, 381/322, 381/328, 381/317, 381/367, 381/354, 381/353, 381/26, 381/94.1, 381/74.1
• US Class Current: 701/10
• CPC Class Codes: G10K 11/17857 Geometric disposition, e.g. placement of microphones
• CPC Class Codes: G10K 11/17873 using a reference signal without an error signal, e.g. pure feedforward
• CPC Class Codes: G10K 2210/1281 Aircraft, e.g. spacecraft, airplane or helicopter

Abstract

An active noise control system for aircraft includes a headset for use by a pilot of the aircraft. A plurality of sensors are mounted on the aircraft at predetermined locations to sense aircraft noise. The aircraft noise at each of the sensors has a first sound waveform in a first phase. A plurality of actuators are operatively connected to respective sensors and communicate with the headset. Each actuator generates a second sound waveform in a second phase. A controller commands each of the plurality of actuators, and dictates the second phase of the second sound waveform, such that the first and second sound waveforms interact out of phase in a manner sufficient to control the aircraft noise. The controlled aircraft noise enables auditory detection of remote environmental disturbances outside of the aircraft thereby enhancing pilot sensory awareness.

Claims

1. An active noise control system for aircraft, comprising:

a headset for use by a pilot of the aircraft;

a plurality of exterior aircraft sensor pairs for mounting on an exterior of the aircraft at predetermined locations, each sensor pair comprising a first sensor for facing inwardly towards the aircraft to sense aircraft noise and a second sensor for facing outwardly away from the aircraft to sense outside environmental noise other than aircraft noise, the aircraft noise at each of said first sensors comprising a first sound waveform in a first phase;

a plurality of actuators operatively connected to respective sensor pairs and communicating with said headset, each of said actuators generating a second sound waveform in a second phase;

a controller commanding said plurality of actuators and dictating the second phase of said second sound waveform, such that the first and second sound waveforms interact out of phase in a manner sufficient to control the aircraft noise generated by the aircraft, whereby the controlled aircraft noise enables auditory detection of the outside environmental noise sensed by the second sensors of said plurality of sensor pairs thereby enhancing pilot sensory awareness.

2. An active noise control system according to claim 1, wherein said first sensors of said plurality of sensor pairs comprise respective microphones for converting the first sound waveform into electrical signals.

3. An active noise control system according to claim 2, wherein said plurality of actuators comprise respective loudspeakers receiving the electrical signal from said microphones, and cooperating with said controller to generate the second sound waveform.

4. An active noise control system according to claim 1, wherein said controller comprises a digital signal processor.

5. An active noise control system according to claim 1, wherein said controller comprises an analog controller.

6. In an aircraft comprising a cockpit, opposing wings, and a fuselage, the improvement comprising an active noise control system, said noise control system comprising:

a headset for use by a pilot in the cockpit of said aircraft;

a plurality of exterior aircraft sensor pairs mounted on an exterior of the aircraft at predetermined locations, each sensor pair comprising a first sensor facing inwardly towards the aircraft to sense aircraft noise and a second sensor facing outwardly away from the aircraft to sense outside environmental noise other than aircraft noise, the aircraft noise at each of said first sensors comprising a first sound waveform in a first phase;

a plurality of actuators operatively connected to respective sensor pairs and communicating with said headset, each of said actuators generating a second sound waveform in a second phase;

a controller commanding said plurality of actuators and dictating the second phase of said second sound waveform, such that the first and second sound waveforms interact out of phase in a manner sufficient to control aircraft noise communicated through the headset to the pilot, whereby the controlled aircraft noise enables auditory detection of the outside environmental noise sensed by the second sensors of said plurality of sensor pairs thereby enhancing pilot sensory awareness.

7. An aircraft according to claim 6, wherein said first sensors of said plurality of sensor pairs comprise respective microphones for converting the first sound waveform into electrical signals.

8. An aircraft according to claim 7, wherein said plurality of actuators comprise respective loudspeakers receiving the electrical signal from said microphones, and cooperating with said controller to generate the second sound waveform.

9. An aircraft according to claim 6, wherein said controller comprises a digital signal processor.

10. An aircraft according to claim 6, wherein said controller comprises an analog controller.

11. An aircraft according to claim 6, wherein said plurality of sensor pairs comprise first and second wing sensor pairs fixedly attached outside of said aircraft on respective wings.

12. An aircraft according to claim 6, wherein said plurality of sensor pairs comprises at least one fuselage sensor pair fixedly attached outside of said aircraft in an area of the fuselage.

13. An aircraft according to claim 6, wherein said plurality of sensor pairs comprises top and bottom fuselage sensor pairs fixedly attached outside of said aircraft on a top and bottom side of the fuselage.

14. A method for enhancing pilot situational awareness in an aircraft, comprising the steps of:

providing a remote disturbance indicator inside a cockpit of the aircraft;

mounting a plurality of exterior aircraft sensor pairs on an exterior of the aircraft at predetermined locations, each sensor pair comprising a first sensor facing inwardly towards the aircraft to sense aircraft noise and a second sensor facing outwardly away from the aircraft to sense outside environmental noise other than aircraft noise, the aircraft noise at each of the first sensors comprising a first sound waveform in a first phase;

operatively connecting a plurality of actuators to respective sensor pairs, each of the actuators generating a second sound waveform in a second phase;

dictating the second phase of the second sound waveform, such that the first and second sound waveforms interact out of phase in a manner sufficient to control the aircraft noise;

when the aircraft noise is controlled, detecting the outside environmental noise sensed by the second sensors of the plurality of sensor pairs; and

transmitting a signal to the remote disturbance indicator inside the cockpit to alert the pilot of the detected outside environmental noise.

15. A method for enhancing pilot situational awareness according to claim 14, wherein the remote disturbance indicator comprises an auditory indicator.

16. A method for enhancing pilot situational awareness according to claim 14, wherein the remote disturbance indicator comprises a visual indicator.

17. A method for enhancing pilot situational awareness according to claim 14, wherein the step of mounting a plurality of sensor pairs comprises locating microphones outside of the aircraft on opposing wings and a fuselage of the aircraft.

18. A method for enhancing pilot situational awareness according to claim 14, wherein the step of dictating the second phase of the second sound waveform comprises utilizing a digital signal controller for commanding the actuators.

19. A method for enhancing pilot situational awareness according to claim 14, wherein the step of dictating the second phase of the second sound waveform comprises utilizing an analog controller for commanding the actuators.

20. A method for enhancing pilot situational awareness according to claim 14, wherein the plurality of actuators comprise loudspeakers.