System and method for adjusting the volume of an audible indication

• US 20070273556A1
• Filed: 05/26/2006
• Published: 11/29/2007
• Est. Priority Date: 05/26/2006
• Status: Abandoned Application

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: Gyde, Mike G., Howell, John A.
• Application Number:
  US11/441,840
• Publication Number:
  US 20070273556A1
• Time in Patent Office: Days
• US Class Current: 340/945
• CPC Class Codes: G01C 23/00 Combined instruments indicating more than one navigational value, e.g. for aircraft; Combined measuring devices for measuring two or more variables of movement, e.g. distance, speed or acceleration

Abstract

A system and method for a vehicle adjusts the volume of an audible indication. An operational state of the vehicle is determined. The audible volume at which the audible indication is provided to the operator is varied based at least in part on said determined operational state of the vehicle.

Claims

1. A method for providing an audible indication to an operator of a vehicle at an audible volume comprising the steps of:

determining an operational state of the vehicle; and

varying the audible volume at which the audible indication is provided to the operator based at least in part on said determined operational state of the vehicle.

2. The method of claim 1, wherein the vehicle is an aircraft and said determination of the operational state is based on at least one of a configuration of the aircraft and an atmospheric condition.

3. The method of claim 2, wherein the configuration of the vehicle comprises at least one of an airspeed, an elevator position, an aileron position, a rudder position, a trim, a flap position, a slat position, an airbrake position, a landing gear position, and an engine power level.

4. The method of claim 3, wherein the atmospheric condition comprises at least one of aircraft altitude, aircraft airspeed, dynamic pressure, turbulence, barometric pressure, temperature, and humidity.

5. The method of claim 3, wherein the audible indication is an aural warning.

6. The method of claim 5, wherein the audible indication is provided by a speaker mounted on a flight deck of the aircraft.

7. The method of claim 6, further comprising:

providing the audible indication to the operator at a first volume if said determined operational state is a first state;

providing the audible indication to the operator at a second volume if said determined operational state is a second state; and

providing the audible indication to the operator at a third volume if said determined state is a third state.

8. The method of claim 7, wherein the first state is indicative of a predicted first ambient noise level on the flight deck of the aircraft, the second state is indicative of a predicted second ambient noise level on the flight deck of the aircraft, and the third state is indicative of a predicted third ambient noise level on the flight deck of the aircraft.

9. The method of claim 8, wherein the first, second, and third volumes are provided by applying first, second, and third predetermined gains to an audio signal provided to the speaker.

10. The method of claim 9, wherein said determination of the state of the aircraft is not based on a detection of an existing ambient noise level on the flight deck of the aircraft.

11. A method for providing an aural warning to an operator of an aircraft comprising:

predicting an ambient noise level on a flight deck of an aircraft based on at least one of an airspeed, an elevator position, an aileron position, a rudder position, a trim, a flap position, a slat position, an airbrake position, a landing gear position, engine throttle, an altitude of the aircraft, barometric pressure, airspeed, turbulence, temperature, and humidity;

detecting an aural warning condition of the aircraft;

providing an aural warning signal to an audio device mounted within the flight deck of the aircraft;

applying a first predetermined gain to the aural warning signal such that the aural warning is emitted from the speaker and provided to the operator at a first volume if said predicted ambient noise level is a first ambient noise level; and

applying a second predetermined gain to the aural warning signal such that the aural warning is emitted from the audio device speaker and provided to the operator at a second volume if said predicted ambient noise level is a second ambient noise level.

12. The method of claim 11, further comprising applying the second predetermined gain to the aural warning signal such that the aural warning is emitted from the audio device and provided to the operator at the second volume if said determined ambient noise level is greater than the first ambient noise level and less than the second ambient noise level.

13. The method of claim 12, further comprising applying a third predetermined gain to the aural warning signal such that the aural warning is emitted from the audio device and provided to the operator at a third volume if said predicted ambient noise level is a third ambient noise level.

14. The method of claim 13, further comprising applying the third predetermined gain to the aural warning signal such that the aural warning is emitted from the audio device and provided to the operator at the third volume if said predicted ambient noise level is greater than the second ambient noise level and less than the third ambient noise level.

15. The method of claim 14, wherein said prediction of the ambient noise level on the flight deck of the aircraft is not based on a detection of an existing ambient noise level on the flight deck.

16. An avionics system comprising:

an audio device mounted on a flight deck of an aircraft to provide an audible indication to an operator of the aircraft;

a gain amplifier coupled to the audio device to provide a gain to an audio signal provided to the speaker; and

a processor in operable communication with the audio device and the gain amplifier, the processor being configured to;

determine an operational state of the aircraft based on at least one of a configuration of the aircraft and an atmospheric condition; and

vary the audible volume at which the audible indication is provided to the operator based at least in part on said determined operational state of the aircraft.

17. The avionics system of claim 16, wherein the configuration of the aircraft comprises at least one of an airspeed, an elevator position, an aileron position, a rudder position, a trim, a flap position, a slat position, an airbrake position, a landing gear position, and engine throttle and the atmospheric condition comprises at least one an altitude of the aircraft, dynamic pressure, turbulence, barometric pressure, temperature, and humidity.

18. The avionics system of claim 17, wherein the processor is further configured to:

apply a first predetermined gain to the audio signal such that the audible indication is emitted from the audio device and provided to the operator at a first volume if said determined operational state is a first state;

apply a second predetermined gain to the audio signal such that the audible indication is emitted from the audio device and provided to the operator at a second volume if said determined operational state is a second state; and

apply a third predetermined gain to the audio signal such that the audible indication is emitted from the audio device and provided to the operator at a third volume if said determined operational state is a third state.

19. The avionics system of claim 18, wherein the first state is indicative of a first predicted ambient noise level on the flight deck of the aircraft, the second state is indicative of a second predicted ambient noise level on the flight deck of the aircraft, and the third state is indicative of a third predicted ambient noise level on the flight deck of the aircraft.

20. The avionics system of claim 19, wherein the processor is further configured to:

apply the second predetermined gain to the audio signal such that the audio indication is emitted from the audio device and provided to the operator at the second volume if said determined operational state is indicative of an ambient noise level that is greater than the first predicted ambient noise level and less than the second predicted ambient noise level; and

apply the third predetermined gain to the audio signal such that the audio indication is emitted from the audio device and provided to the operator at the third volume if said determined operational state is indicative of an ambient noise level that is greater than the second predicted ambient noise level and less than the third predicted ambient noise level.