CUSTOMIZED AURAL METHOD AND SYSTEM FOR MANAGING THREATS IN AN AIRCRAFT COCKPIT

• US 20150097706A1
• Filed: 10/09/2013
• Published: 04/09/2015
• Est. Priority Date: 10/09/2013
• Status: Abandoned Application

• Current Assignee: CMX Avionics, LLC
• Original Assignee: CMX Avionics, LLC
• Inventors: Perger, Warren F., Abbatt, William G.
• Application Number:
  US14/049,593
• Publication Number:
  US 20150097706A1
• Time in Patent Office: Days
• US Class Current: 340/977
• CPC Class Codes: B64D 2045/0075 Adaptations for use of electronic flight bags in aircraft; Supports therefor in the cockpit
• CPC Class Codes: B64D 45/00 Aircraft indicators or protectors not otherwise provided for camouflage F41H3/00
• 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
• CPC Class Codes: G01C 5/005 altimeters for aircraft G01C5/02, G01C5/06 take precedence
• CPC Class Codes: G01D 2207/10 Displays which are primarily used in aircraft or display aircraft-specific information
• CPC Class Codes: G01D 7/12 Audible indication of meter readings, e.g. for the blind
• CPC Class Codes: G08B 3/10 using electric transmission; using electromagnetic transmission
• CPC Class Codes: G10L 13/00 Speech synthesis; Text to speech systems
• CPC Class Codes: G10L 15/00 Speech recognition G10L17/00 takes precedence

Abstract

A micro-computer based aircraft system that creates aural messages based upon system-detected threats (e.g., low oil pressure). The messages are unique to the make and model of aircraft. Speech recognition allows the pilot to request aircraft-specific, customized aurally-delivered checklists and to respond via a challenge and response protocol. This permits a hands-free, timely, complete and prudent response to the threat or hazardous situation, while allowing the pilot the relative freedom to do what is paramount: first, fly the airplane (with minimum distraction).

Claims

1. A system that provides audio feedback to the pilot of an aircraft, the system comprising:

a) a plurality of sensory interfaces to instruments mounted in the aircraft, the sensory interfaces monitoring an operating condition of an aircraft subsystem and generating signals (S_i) indicative of the operating condition;

b) a microprocessor for

processing the signals (S_i) from the plurality of sensory interfaces,

comparing the signals (S_i) with ranges (V_min-V_max) of acceptable values thereof indicative of a normal operating range, and

generating one or more diagnostic advisory signals (S_d) in response thereto;

c) an audio interface to the microprocessor to enable the pilot to provide commands to the microprocessor; and

d) an audio interface from the microprocessor to the pilot that provides the audio feedback to the pilot depending on the advisory signals (S_d) and pilot commands.

2. The system of claim 1 wherein the microprocessor generates an audio announcement to the pilot when a sensed signal (S_i) lies outside the normal operating range (V_min-V_max), the audio announcement to the pilot including a status indicator and a checklist appropriate to the subsystem condition sensed to assist the pilot in diagnosing and reacting to the sensed condition.

3. The system of claim 2 wherein when a sensor'"'"'s input (Si) is outside a normal operating range (Vmin-Vmax) for an oil pressure subsystem, the global positioning subsystem receiver is interrogated to obtain the identifier of the nearest airport, which is presented as an aural message to the pilot that includes information including distance, time, and bearing to the nearest airport.

4. The system of claim 1 wherein the audio interface between the microprocessor and the pilot includes a software speech recognizer.

5. The system of claim 1 wherein the audio interface between the microprocessor and the pilot includes a software speech synthesizer.

6. The system of claim 4 wherein the audio interface communicates with a microphone associated with the pilot'"'"'s headset.

7. The system of claim 5 wherein the audio interface includes a speaker line associated with the pilot'"'"'s headset.

8. The system of claim 1 further including a global positioning subsystem for monitoring aircraft speed and location with respect to two or three dimensional frames of reference.

9. The system of claim 1 wherein checklists customized to the make and model of the aircraft may be summoned by a voice command.

10. The system of claim 1 wherein the subsystems being monitored include one or more of

an oil pressure sensor;

a electrical subsystem charging sensor;

a manifold pressure sensor;

a landing gear position sensor; and

a vacuum sensor.

11. The system of claim 9 wherein the checklists are presented by a speech synthesizer.

12. The system of claim 1, wherein the sensory interfaces include electrical contacts with transducers and sensors.

13. The system of claim 2 further including means for communicating a signal to the microprocessor that is indicative of aircraft altitude so that the microprocessor may calculate a power-off glide distance based on altitude, weight and best glide speed.

14. The system of claim 1 further including means for creating at start-up an ad hoc network for WiFi connection to one or more authenticated devices selected from the group consisting of an iPad, a tablet computer, an iPhone, a Blackberry, another smartphone and like devices for creating flight log entries.

15. The system of claim 14 wherein the flight log entries are communicated to a remote device via a WiFi connection, using a Bluetooth-connected GPS receiver, the remote device being capable of running a browser such as but not limited to Safari, Explorer and Firefox.

16. The system of claim 15 wherein the log book entries include one or more mechanic'"'"'s flight log entries with additional information as to the threat or abnormal condition recorded for a mechanic or investigator to interpret.

17. The system of claim 1 further including either a 12 or 24 volt bus without requiring a switch to be set by an installer and means for detecting the bus voltage.

18. A method for providing audio feedback to the pilot of an aircraft, comprising the steps of:

a) mounting a plurality of sensory interfaces upon instruments in the aircraft, the sensory interfaces monitoring an operating condition of an aircraft subsystem and generating signals (S_i) indicative of the operating condition;

b) connecting a microprocessor to the sensory interfaces for

processing the signals (S_i) from the plurality of sensory interfaces,

comparing the signals (S_i) with ranges (V_min-V_max) of acceptable values thereof indicative of a normal operating range, and

generating one or more diagnostic advisory signals (S_d) in response thereto;

c) communicating an audio interface with the microprocessor to enable the pilot to provide commands to the microprocessor; and

d) providing an audio interface from the microprocessor to the pilot that generates the audio feedback to the pilot depending on the advisory signals (S_d) and pilot commands.

19. The method of claim 18 further including the step of

(e) initializing the system by setting startup parameters selected from the group consisting of aircraft make and model, initial weight of fuel on board, fuel burn rate and ranges (V_min-V_max) of acceptable values for aircraft subsystems to be monitored.

20. The method of claim 19 further including the step of

(f) computing the actual weight of the aircraft (W_a) as it changes during the flight based on the initial weight of fuel on board, the elapsed time and fuel burn rate;

(g) entering (W_a) into an algorithm that calculates glide distance based in part thereon and communicating that glide distance to the pilot.