METHOD OF MANAGING AIRCRAFT WARNINGS, AND A DEVICE FOR IMPLEMENTING SAID METHOD

• US 20100250034A1
• Filed: 03/18/2010
• Published: 09/30/2010
• Est. Priority Date: 03/31/2009
• Status: Abandoned Application

• Current Assignee: Eurocopter
• Original Assignee: Eurocopter
• Inventors: REICH, Alexander, BOUCHARD, Pierre, JUPPET, Valérie
• Application Number:
  US12/726,588
• Publication Number:
  US 20100250034A1
• Time in Patent Office: Days
• US Class Current: 701/14
• CPC Class Codes: G07C 5/0825 using optical means
• CPC Class Codes: G07C 5/0833 using audio means
• CPC Class Codes: G08B 7/06 using electric transmission , e.g. involving audible and visible signalling through the use of sound and light sources
• CPC Class Codes: G08G 5/0021 located in the aircraft

Abstract

A method of managing warnings in an aircraft, includes:

• • receiving information signals associated with a malfunction or with conditions requiring the pilot to be informed;
  • preparing warning instructions as a function of the context and forwarding the warning instructions to visual and/or audible indicator elements;
  • allocating a visual and/or audible warning to each of the warning instructions; and
  • using visual indicator elements to display the visual warnings and using audible indicator elements to emit the audible warnings.

Claims

1. A method of managing warnings in an aircraft, the method consisting:

in a step (10), in detecting information signals, e.g. coming from sensors (C1, C2, C3) and associated with malfunctions or conditions requiring the pilot to be informed;

in a step (15), in preparing warning instructions as a function of the context and forwarding said warning instructions to visual and/or audible indicator means (3, 4);

in a step (20), in allocating at least one visual and/or audible warning (V, S) to at least some of the warning instructions;

in a step (30), in allocating a priority class to at least the visual warnings (V);

in a step (40a, 40b, 40c), in allocating a priority rank to each visual warning (V) and to each audible warning (S), said priority rank depending for example on the system to which the warning instruction relates or on the importance of the system in the aircraft;

in a step (50), in recording a maximum number T of visual and/or audible warnings (V, S) in a warning list by priority rank;

in a step (60), in selecting a maximum N of visual warnings (V) consistent with the operation of the aircraft, presenting the highest priority classes or by default the highest priority ranks, where N is less than or equal to T, and in displaying the N corresponding warnings using the visual indicator means (3); and

in a step (90a, 90b), in selecting at least one audible warning (S) firstly presenting the highest priority rank and secondly consistent with the operating context of the aircraft, and in emitting the corresponding audible warning using the audible indicator means (4).

2. A method according to claim 1, consisting in transmitting the information signals to a processor module of the computer kind, which module processes said information signals with the help of an algorithm.

3. A method according to claim 1, consisting in displaying the visual warning (V) and/or in emitting at least one audible warning (S), while waiting for an acknowledgment or processing by the pilot.

4. A method according to claim 3, consisting, in a step (25), in allocating e.g. a lower priority rank to those warnings (S, V) that are acknowledged by the pilot.

5. A method according to claim 3, consisting in ensuring that an acknowledgment consists in step (25) in ensuring that an acknowledgment is consistent with the visual and audible warnings (V, S) by inhibiting the acknowledgment of visual warnings (V) while an audible warning (S) having no visual equivalent is activated.

6. A method according to claim 3, consisting in eliminating from the list of warnings, visual and/or audible warnings (S, V) that have been processed by the pilot.

7. A method according to claim 1, consisting in verifying consistency between the visual and audible warnings before activating them.

8. A method according to claim 1, consisting in defining subsets of malfunctions or conditions for which warning instructions associated with distinct events give rise to visual and/or audible warnings (V, S) that are identical.

9. A method according to claim 1, consisting in emitting audible warnings (S) successively one after another, or in alternation, or by adapting sound levels, as a function of the priority ranks allocated to said warnings.

10. A method according to claim 1, consisting in emitting audible warnings (S) simultaneously, providing said audible warnings (S) are of different kinds, such as for example a sound warning and a voice warning, providing their priority ranks make that possible.

11. A method according to claim 1, consisting in updating the list of warnings periodically, e.g. every 50 milliseconds.

12. An on-board device for processing warnings to implement the method in accordance with claim 1, the device comprising:

a concentrator (5) for concentrating data (D), the concentrator being constituted by a piece of equipment or a module incorporated in a piece of equipment, serving to acquire information signals from various systems and pieces of equipment of the aircraft;

a warning manager (2) constituted by a module incorporated in or separate from the data concentrator (5), for processing information signals and for generating warning instructions, while taking account of the context of the aircraft;

visual indicators (3) for displaying the visual warnings (V); and

audible indicators (4) for emitting the audible warnings (S).

13. An aircraft of the helicopter kind including an on-board device in accordance with claim 12.